Title of Invention	SLING WITH PREDICTABLE PRE-FAILURE WARNING INDICATOR
Abstract	The pre-failure warning indicator (11) is provided for use with a sling (10). The pre-failure warning indicator (11) triggers at a point that is predictable within a relatively narrow range, thereby increasing the possibility that a damaged sling (10) is removed from use. The pre-failure warning indicator (11) includes a dedicated strand of material (20) that is placed in close proximity to the load- bearing core yarns (17) of the sling (10) but remains separate and independent from the core yarns (17); the ends (22,24) of the dedicated strand are connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is visible to operators/riggers work in conjunction with the sacrificial strand (20) and the ring (26) is designed to fail when the sling (10) is subjected to a specifically chosen condition (e.g. excessive weight). The failure of the ring (26) causes the warning fiber (20) to withdraw from the rigger's view thereby warning he rigger that the sling (10) was subjected to the specifically chosen condition and may be damaged.

Title of Invention

SLING WITH PREDICTABLE PRE-FAILURE WARNING INDICATOR

Abstract

The pre-failure warning indicator (11) is provided for use with a sling (10). The pre-failure warning indicator (11) triggers at a point that is predictable within a relatively narrow range, thereby increasing the possibility that a damaged sling (10) is removed from use. The pre-failure warning indicator (11) includes a dedicated strand of material (20) that is placed in close proximity to the load- bearing core yarns (17) of the sling (10) but remains separate and independent from the core yarns (17); the ends (22,24) of the dedicated strand are connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is visible to operators/riggers work in conjunction with the sacrificial strand (20) and the ring (26) is designed to fail when the sling (10) is subjected to a specifically chosen condition (e.g. excessive weight). The failure of the ring (26) causes the warning fiber (20) to withdraw from the rigger's view thereby warning he rigger that the sling (10) was subjected to the specifically chosen condition and may be damaged.

Full Text	WO 2006/127489 PCT/US2006/019518 SLING WITH PREDICTABLE PRE-FAILURE WARNING INDICATOR CROSS-REFERENCE TO RELATED APPLICATION The present application claims the benefit under any applicable U.S. statute, including 35 U.S.C. § 120, to U.S. Application No. 11/418,597 filed 05 May 2006, in the name of Dennis St. Germain and titled Sling With Predictable Pre-Failure Warning Indicator, and claims the benefit under any applicable U.S. statute, including 35 U.S.C. § 119(e), to U.S. Provisional Application No. 60/683,987 filed 23 May 2005, in the name of Dennis St. Germain and titled Sling Having Predictable Pre-Failure Warning Indicator and Associated Method. This application incorporates by reference U.S. Application No. 11/418,597 and U.S. Provisional Application No. 60/683,987 as if both are fully set forth herein. FIELD OF THE INVENTION This invention relates generally to industrial slings used to lift, move and transport heavy loads and, more particularly, an apparatus for notifying operators/riggers who use synthetic slings of an overload or damage situation that may lead to sling failure. BACKGROUND OF THE INVENTION Wire rope slings made of a plurality of metal strands twisted together and secured by large metal sleeves or collars are common in the industry. During the past thirty years, industrial metal slings have seen improvements in flexibility and strength. However, compared to non-metal or synthetic fiber slings, metal slings are relatively stiff and inflexible. WO 2006/127489 PCT/US2006/019518 2 Synthetic fiber slings have gained popularity over the last fifteen years and are replacing metal slings in many circumstances. Synthetic slings are usually comprised of a lifting core made of twisted strands of synthetic fiber and an outer cover that protects the core. The most popular design of synthetic slings is a roundsling in which the lifting core forms a continuous loop and the sling has a circular or oval-shaped appearance. An advantage of synthetic slings is that they have a very high load-lifting performance strength-to-weight ratio which provides for a lighter, more flexible and even stronger slings than their heavier and bulkier metal counterparts. Even with such advances in the art of sling making, the riggers who use these improved synthetic slings still suffer and endure some of the age old problems of sudden failure and loss of a load caused by a sling breaking without warning because it was fatigued (or overly stretched) from being subjected previously to overload conditions. After a sling has been fatigued, it does not usually provide any physical indication that it was damaged - even to the trained eye. (One of the few advantages of a metal sling over a non-metal sling is that there is equipment available that can be used to conduct a non-destructive test of the metal. For example, similar equipment is routinely used to determine whether the wings of an airplane have become fatigued.) Standard break tests have been established for determining how large of a load a sling can endure. Slings are attached to a testing machine that applies a steady but increasing force on the sling until it is unable to withstand the stress of the force being applied to it and the sling ultimately breaks. Such break tests have enabled manufacturers of industrial slings to rate the load-bearing capacity of the sling. The load capacity is determined to be a point well below the load used to break the sling and also below the point where the sling is fatigued or damaged. Most sling manufacturers will affix some type of tag notice on the sling which WO 2006/127489 PCT/US2006/019518 3 states the load capacity (rated capacity) of the particular sling. This rated capacity gives the maximum amount of load to which the sling may be subjected and still be considered a safe use of the sling. Unfortunately, even conscientious operators/riggers who do not take unsafe shortcuts and who operate in a safe responsible manner sometimes are surprised by a sling breaking in use even when they believed it was being used within the load limits of its rated capacity. For example, when industrial slings are in continuous heavy use over three shifts around the clock, the operators on a later shift may not be aware that someone on an earlier shift had subjected the sling to a substantial overload which may have caused serious damage to the lifting core strands of the sling. When a synthetic fiber sling is overloaded beyond its tensile strength or weight-lifting capacity at maximum stretch, it is considered to be fatigued and may never return to its normal strength and load bearing capacity. When subjected to an overload condition above its rated capacity, a roundsling can be permanently damaged/deformed if the load stretches the fibers of the load bearing core material beyond their yield point. An over-loaded sling may be susceptible to fracture at a stress point. This condition is similar to the stretching of a rubber band beyond its point of normal elasticity so that when the load or tension is removed or relieved, the rubber band will never regain its normal configuration and its strand dimensions may be permanently stretched which will cause it to fail under a load which is less than its tensile strength load. As stated previously, it is nearly impossible to determine, upon a cursory visual inspection, that a sling has been damaged because of the large size of such slings (on the order of 6 feet or more) and because the load-bearing core is hidden inside the outer cover. Once the load-lifting core of the synthetic sling is stretched beyond its yield point, it WO 2006/127489 PCT/US2006/019518 4 can actually change in its physical structure and be restricted at a stress point. To date, there has been no precise method or apparatus available to an operator or rigger to determine if a sling with a protective cover was subjected to an overload or damage-causing condition. If a roundsling has been fatigued or structurally changed, the sling may no longer lift a load according to its maximum rated load capacity and, most importantly, becomes a serious threat to the operators and riggers using the sling. Thousands of roundslings are being used on a daily basis in a broad variety of heavy load lifting applications which range from ordinary construction (e.g., skyscrapers and bridges), plant and equipment operations, to ship building (e.g., oil rigs), nuclear power plants and the like. The lifting core fibers of such roundslings may be derived from natural or synthetic materials, such as polyester, polyethylene, nylon, and the like. Although the outer covers of synthetic slings are designed to reduce damage, the core fibers are still susceptible to damage from abrasion, cutting by sharp edges, or degradation from exposure to heat, cold, ultraviolet rays, corrosive chemicals or gaseous materials, or other environmental pollutants. In certain instances, the core yarn of a synthetic sling could weaken, melt or disintegrate when subjected to elevated temperatures, or to prolonged exposure to either ultraviolet light or chemicals. Still another safety concern flows from abuse by the user when the core yarn is damaged from abrasive wear when the slings are not rotated and the same wear points are permitted to stay in contact for extended periods of time with a device used for lifting (such as hooks on a crane), or on the edges of the load itself. Such abrasion is accelerated for certain types of synthetic fiber material and especially if the load contact section is under compression or is bunched. Riggers in the field are concerned that the inner lifting core yarn of their roundslings may be damaged on the inside without a means for them WO 2006/127489 PCT/US2006/019518 5 to detect such defects through the sling cover. Even if the cover is removed it may be impossible to tell if the lifting core has been damaged to the point where it cannot lift its rated load. Since there is no reasonable non-destructive testing techniques for synthetic fiber slings, a synthetic sling that is only suspected of being damaged must be removed from service for safety reasons. The structural integrity of the roundsling lifting core material is difficult to determine when it is hidden inside a protective cover of opaque material which renders the lifting core yarn inaccessible for inspection. A stretched or fatigued roundsling could experience a sudden catastrophic failure without warning to the rigger, which may result in the loss of lives and property. Many in the industry have sought to provide safe slings to its riggers to avoid bodily injury, property damage and product liability claims. Several roundsling constructions are known which have a failure indicator. For example, it is known in the art to incorporate a failure indicator synthetic strand as an integral member of the lifting or load-bearing core. The failure indicator strand in prior art constructions was always an extension of the core yarns. A popular design of prior art roundslings was to twist a plurality of yarns together to form a single strand; the strand is then rolled into an endless parallel loops of strands that form the core, which is then encased in a protective cover material. If the sling was designed with a prior art failure indicator, an indicator strand would be incorporated into and twisted with the core yarns. The two ends of the indicator strand (sometimes referred to as tell-tails), extend freely through an opening in the cover material. When the sling is subjected to an overload condition, the tell-tail would partially withdraw within the cover and the freely extending tell-tail ends would be visibly shorter than the tell-tails of an undamaged sling; if WO 2006/127489 PCT/US2006/019518 6 the overload condition exceeded the maximum rated load of the sling, one or both tell-tails would usually withdraw completely within the cover. In either event, the rigger is warned of the occurrence of a potentially damaged sling by either the absence of one or both tell-tails, or a "significant" withdraw of at least one tell-tail inside the cover. However, there usually was no consistency on how the tell-tails would react when triggered, even when the slings were manufactured under identical conditions. A drawback of prior art failure indicators based on an indicator strand is that there is no predictable way of determining when the failure indicator will be triggered. Synthetic slings have a safety factor designed into their construction. For example, if the sling is rated at 6,000 pounds, it typically will not be damaged unless the sling is subjected to a force five times greater (i.e., around 30,000 pounds, a 5-to-1 design factor) than the rated capacity; the tell-tail may be triggered and indicate an overload condition when the sling is subject to a force of between four to five times the rated capacity (i.e., about 24,000 lbs) by retracting into the sling's cover. Therefore, the tell-tail will provide a visual indication that the sling may have been damaged or subjected to a situation that may have been detrimental to the overall condition of the sling before the sling actually is subjected to such a condition. Unfortunately, there was no way of ensuring that the tell-tails would consistently withdraw within the cover at about 24,000 pounds. In other words, two slings having prior art failure indicator strands contemporaneously made under the same conditions would have two different trigger points (for example, one sling may trigger at about 22,050 pounds and the other sling may trigger at about 26,000 pounds). In addition, one sling may react to a trigger event by completely withdrawing one of the tell-tails, while the other sling may react to a trigger event by partially withdrawing both tell-tails. WO 2006/127489 PCT/US2006/019518 7 If the tell-tail is not withdrawn completely within the cover, one rigger's opinion of a "significant withdrawal" towards the opening in the cover may differ from another rigger's opinion. Therefore, a "small" movement of one or both of the tell-tails, which may result from the constant use and handling of the sling, may appear to one rigger as an indication that an overload condition was reached when, in fact, the sling was not subjected to an overload condition. Therefore, the visual inspection of the tell-tails in prior art failure indicators and the eventual determination of a trigger event becomes a subjective test. Another prior art roundsling construction utilizes an optical fiber strand that enables the operator/rigger to test it by shining a light on one end of the optical fiber to determine if the light can be seen at the other end of the optical fiber. In U.S. Patent No. 5,651,572 to Dennis St. Germain, it is taught to incorporate a flexible fiber optic "signal" cable into the lifting core strands of the roundsling. As indicated previously, in a roundsling, the lifting core is configured in endless parallel loops of strands which are then encased within a protective cover material. The cover will have openings or orifice slits out of which the two ends of the fiber optic signal strand emerge. The aforesaid ends of the fiber optic cable are designed to extend freely through a slit in the sling's cover so that they are easily accessible by the rigger. The optical signal strand member conducts light from a light source at one end to an observer looking at the opposite end for testing the integrity and the continuity of the core strands. The inclusion of the fiber optic cable in the lifting core yarn of the roundsling converts the inaccessible inner core area into an observable test check area by means of the passage of light through the fiber optic component of the lifting core. Fiber optic materials are capable of transmitting light into endless parallel relationship WO 2006/127489 PCT/US2006/019518 8 with the fibers of the lifting core yarn. This fiber optic signal strand comprises fiber or rod material which permits the propagation of light that enters the fiber material at one end and is totally reflected back inward repeatedly from the fiber wall through the entire length of the fiber optic strand which enables the light being transmitted within the fiber optic cable to pass from one end of the fiber optic cable to the other end. If the light emerges at the other end of the fiber optic cable, it indicates that the integrity of the fiber optic cable throughout the path of the roundsling lifting core bundle is intact and, by reasoning, the integrity of the lifting core yarns are also intact. Since the fiber optic cable member is incorporated into the lifting core of the roundsling disclosed in U.S. Patent No. 5,651,572, it tends to develop somewhat similar breaking or snapping characteristics as the lifting core fiber materials. If the fibers of lifting core yarn break or fracture, then the fiber optic cable will also be damaged which will prevent the transmission of light from one end to the other end of the emerging fiber optic cable. If the light fails to pass from one end of the signal fiber optic cable to the other end, then the rigger is warned that the lifting core strands may be damaged, and to remove the protective cover from the roundsling for further inspection. If, upon inspection, it is determined that the roundsling was damaged, it will be immediately removed from service, and replaced with a new sling. Although the apparatus disclosed in U.S. Patent No. 5,651,572 is currently the leading product for determining whether the lifting core yarns of a synthetic sling have snapped or been damaged, in the stages where the sling has been subjected to an overload condition, the fiber optic signal strand still does not have the identical stretching properties of the load- bearing core yarns. Accordingly, unless the fiber optic cable breaks completely, some light WO 2006/127489 PCT/US2006/019518 9 may still be able to traverse the entire length of the fiber optic cable such that the degradation in the intensity of the light may be imperceptible to the naked eye. Alternatively, the fiber optic cable, being more brittle than the synthetic core material, may be damaged by normal handling (and dropping) of the sling, or at a force less than the rated capacity of the sling. In such cases, the light transmission through the fiber optic cable may be disrupted causing the fiber optic cable to indicate an overload condition when, in fact, no overload condition was reached. Finally, under other excessive or damage-causing situations (e.g., excessive heat, acidic or chemical exposure, and ultraviolet exposure) it can be expected that the fiber optic cable will be affected differently than the synthetic strands of the lifting core. If, for example, a sling with the fiber optic signal cable is exposed to certain chemicals, the fiber optic signal cable may be relatively unaffected (or only its exterior surface is affected leaving the light path through the center of the cable unscathed), while the lifting core has been degraded to the point where it no longer meets its load rating. Therefore, as stated previously, the need to precisely determine whether the load bearing core of a synthetic sling was subjected to an excessive or damage- causing situation still exists. SUMMARY OF THE INVENTION The present invention discloses a pre-failure warning indicator for use with a sling that is more accurate and predictable than prior art indicators. In the present invention, the failure indicator strand is separate and independent from the load-bearing core yarns. One of the most popular designs of a roundsling is to twist a plurality of yams together to form a single strand; the strand is then rolled into endless parallel loops of strands WO 2006/127489 PCT/US2006/019518 10 that form the core. In accordance with the present invention, a pre-failure warning indicator includes a separate dedicated strand of material, a ring made of a specially chosen material, and a separate warning fiber having an elongated indicator whip end. The dedicated strand is placed proximate and substantially parallel to the loops of core strands of the sling; the ends of the dedicated strand are brought within close proximity (in a preferred embodiment several inches) to each other and are terminated with eyes or another configuration that can secure the ring. The ring is inserted through or secured to both eye terminations, thereby bridging the gap between the ends of the dedicated strand, and usually forms an oval-shaped loop. One end of the warning fiber is attached to one of the eyes of the dedicated strand, and the free end of the warning fiber is placed along the ring and threaded through the opposite eye; the free end of the warning fiber is then double-backed along the length of the ring. A tubular cover material encases the lifting core and the pre-failure warning indicator. The free end of the warning fiber extends through an opening in the cover material and is referred to as the indicator whip. In a specific embodiment, a tag is attached to the strand (and preferably one of the terminating eyes) and is also drawn through the slot so that it extends freely outside the cover. The tag is designed to provide an indicator that the sling has been tampered with or sabotaged. The ring is designed to fail when the sling is subjected to an excessive or damage- causing situation. A common damage-causing situation is when the sling is over-loaded. The ring will break when the sling is placed in an overload situation, thereby causing the termination eyes to separate, resulting in the complete withdrawal of the whip inside of the cover. WO 2006/127489 PCT/US2006/019518 11 By choosing the ring carefully, relatively accurate predictions of the force needed to trigger the warning fiber can be made. In addition, the ring may be chosen to fail and thereby convey a damage situation when the sling is being used under unusual environmental conditions (e.g., excessively hot, acidic, or ultraviolet rays from, for example, sunlight). Previous indicators either of the fiber optic nature or of the tell-tail type could give false indications of an overload or other internal damage. In the case of fiber optics, the ability to transmit light can be impeded by dirt, grease, and other debris that can retard the transmission of light through the fiber optic cable by jamming the ends. In the case of tell- tails, the movement of the sling's outer cover from friction with a load can give a false implication that the tell-tails were pulling under the cover when it was really the cover moving over the tell-tails. In the current invention, these areas of confusion are eliminated by a simple visual identification of the external warning indicator. Also, the dedicated strand can be locked into place by permanent attachment to the cover. If the cover shifts, the entire assembly of this invention moves with it in concert so a false indication of overload is eliminated. Additional objects and advantages will be evident to one skilled in the art after a reading of the detailed description that follows. BRIEF DESCRIPTION OF THE DRAWINGS The accompanying drawings, which are incorporated in and form a part of the specification, illustrate the embodiments of the present invention and, together with the following description, serve to explain the principles of the invention. For the purpose of illustrating the invention, there are shown in the drawings embodiments which are presently WO 2006/127489 PCT/US2006/019518 12 preferred, it being understood, however, that the invention is not limited to the specific instrumentality or the precise arrangement of elements or process steps disclosed. In the drawings: Figure 1 is a perspective view of a single-path roundsling which incorporates a predictable pre-failure warning indicator in accordance with the present invention; Figure 2 is an enlarged cross-sectional view of the roundsling illustrated in Figure 1 taken along line 2-2; Figure 3 is a side view of a pre-failure warning indicator in accordance with the present invention; Figure 4 is a side view of another embodiment of a pre-failure warning indicator in accordance with the present invention, utilizing multiple rings linked together; Figure 5 is a side view of another embodiment of a pre-failure warning indicator in accordance with the present invention for use with a two-path sling; Figure 6 is a perspective view of a two-path sling incorporating the pre-failure indicator of Figure 5; Figure 7 is a side view of a pre-failure warning indicator in accordance with the present invention which also incorporates a sabotage indicator means; and Figure 8 is a perspective view of a single-path roundsling incorporating the predictable pre-failure warning indicator of Figure 3 and the sabotage indicator of Figure 7. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT In describing a preferred embodiment of the invention, specific terminology will be selected for the sake of clarity. However, the invention is not intended to be limited to the WO 2006/127489 PCT/US2006/019518 13 specific terms so selected, and it is to be understood that each specific term includes all technical equivalents that operate in a similar manner to accomplish a similar purpose. The subject invention is an apparatus and method for determining whether a synthetic fiber sling has been damaged (because of an overload or other condition that could weaken the sling's load-bearing core) to a point where the sling should be removed from service and returned to the manufacturer for internal inspection and, if necessary, repair or disposal. Preferred embodiments of the present invention will now be described in detail with reference to the accompanying drawings in which a roundsling having a pre-warning failure indicator in accordance with the present invention is generally indicated at 10. The various preferred embodiments will be described with reference to the drawing figures that form a part of this description where like numerals represent like elements throughout. Figure 1 illustrates a perspective view of a roundsling in accordance with the present invention. Figure 1 specifically shows a single-path roundsling, but the principles disclosed herein may be applied to other slings including multiple-path slings. Figure 2 is a cross- sectional view of the roundsling shown in Figure 1 taken along line 2-2, and illustrates the primary interior components of a typical roundsling. Referring to Figures 1 and 2, the roundsling 10 comprises an inner core 12 encased within an outer protective cover 25. The outer cover 25 shown in Figure 2 is meant to convey that the cover 25 is larger than the load-bearing core 12 and moves relatively freely with respect to the load-bearing core 12 and not necessarily that the cover 25 has a cross-sectional shape of an oval. The core 12 is designed to bear the entire weight of the load to be lifted. The primary purpose of the outer cover 25 is to prevent physical damage to the core from abrasion, sharp edges on the load, etc.; the cover 25 will also help to reduce damage to the WO 2006/127489 PCT/US2006/019518 14 sling when it is used in an environment that will subject it to harsh elements such as heat, ultraviolet light, corrosive chemicals, gaseous materials, or other environmental pollutants. As will be explained hereinafter, the cover 25 can also be designed to notify a user when physical damage has occurred to the cover. The lifting core 12 is preferably made of a single or multiple strands 17 configured in a plurality of endless parallel loops of strands to form a single core or multiple cores, all of which are contained inside the protective cover material 25. The use of a single strand or multiple strands in this configuration is typical in the construction of roundslings. The lifting core 12 of such roundslings may be derived from one or more natural or synthetic materials, such as polyester, polyethylene, nylon, K-Spec® (a proprietary blend of fibers), HMPE, LCP, para-aramid or other types of synthetics. The material chosen for the core primarily depends on the maximum weight the sling is designed to lift and environment in which the sling 10 will be used. Such sling constructions have a high lifting and break strength, lighter weight, high temperature resistance and high durability, compared to wire rope or metal chain slings. Referring now to Figure 3, the pre-failure warning indicator 11 in accordance with the present invention is illustrated in side view and is shown without the cover 25 and without core 12. In a preferred embodiment, the sling 10 may be manufactured with only a pre-failure warning indicator 11, or with both a pre-failure warning indicator 11 and a tamper-evident means 35. Initially, the operation of the pre-failure warning indicator 11 will be disclosed; the tamper-evident means 35 will be described later with respect to Figure 7. A separate (preferably single) strand 20 of yarn is dedicated to the pre-failure warning indicator 11. The dedicated warning strand 20 is located within cover 25; it is preferably WO 2006/127489 PCT/US2006/019518 15 placed proximate the core 12 and may either be twisted around the load-bearing strands of the core 12 or it may just lay next to the core 12, as illustrated in Figure 2. In a different embodiment, it may be desired to permanently affix the dedicated strand 20 to the inside of the cover 25. When a sling is used over a period of time, the cover will develop wear points at specific locations, for example, where the sling hangs from a crane's hook. Accordingly, it is usually advisable to rotate the cover with respect to the load-bearing core 12. By securing the dedicated strand 20 to the inner cover, movement of the cover (either intentionally or non-intentionally) will not affect the operation of the pre-failure warning indicator 11. First end 22 and second end 24 of the dedicated strand 20 are terminated in eyes 32, 34, respectively. The dedicated strand 20 and eyes 32,34 are preferably made of the same material as the core strands 17. The eyes 32,34 are connected by a ring 26, thereby forming an endless loop with the dedicated strand 20. The shape of the separate dedicated strand 20 generally matches the shape of the endless parallel loops formed by the core strand 17 (i.e., generally circular or oval). Although the term "ring" implies a circularly-shaped object, as used herein "ring" is defined as any closed link or band that will connect the ends of a dedicated strand. In one preferred embodiment, the ring 26 is chosen to have a lower tensile strength than the core 12. The sling manufacturer may choose to do this any number of ways, e.g., by making the ring 26 out of a different material than the dedicated strand 20, cutting a notch or notches in the ring to physically weaken it, or by making the ring 26 out of the same material as, but of a smaller diameter than, the core strands 17. When ring 26 is chosen to have a WO 2006/127489 PCT/US2006/019518 16 lower tensile strength, the pre-failure warning indicator 11 is designed to trigger and thereby notify the rigger or other users of the sling that the sling 10 has been subjected to an overload condition (i.e., the sling was subjected to a force that was pre-determined to compromise the integrity of the sling, and is sometimes determined to be about four times greater than the sling's rated capacity). Attached to first termination eye 32 is a warning indicator fiber 29. Warning indicator fiber 29 is an elongated strand that is placed substantially parallel to the ring, is threaded through the second termination eye 34, is then double-backed along the ring 26 towards the first eye 32, and directed out an opening in the sling cover 25. (The external end 40 of the warning indicator fiber 29 that extends through the sling cover 25 is sometimes referred to as a "whip.") Although the sling cover 25 is not shown in Figure 3, the preferred orientation of the warning indicator fiber 29 is illustrated, i.e., it forms a substantially "J" shape within the sling cover 25. Referring again to Figure 1, the whip 40 of the warning indicator 29 extends freely through cover 25. Although not necessary, cover patch 30 may be attached (preferably by sewing), to the cover to protect the opening through which the whip end 40 of the warning indicator 29 extends. The dedicated strand 20 is preferably made of similar material as the strands 17 of the load-bearing core 12; this promotes the relatively equal stretching of all components of the sling 10. In a preferred embodiment, the ring 26 has a pre-selected lower tensile strength than the material used to make the core strands; in this embodiment, the ring 26 will fail before the lifting core 12 is stretched or fatigued. Alternatively - or in addition - the ring 26 may be designed to have a lower resistance to abrasion, heat, cold, and/or chemical exposure. By WO 2006/127489 PCT/US2006/019518 17 carefully choosing the properties of ring 26, a sling manufacturer can control the condition(s) under which the subject pre-failure warning indicator 11 will trigger. In one example, the sling manufacturer may design the ring 26 to fail at 70% of the tensile strength of the inner core. Accordingly, the material from which ring 26 is made and/or its cross-sectional thickness may be chosen to meet the pre-selected tensile strength. When the sling 10 is placed under a load that exceeds its recommended rating, ring 26 will fail before damage can occur to either the load bearing core strands 17 that form the core 12 or the dedicated strand 20. When ring 26 fails, the termination eyes 32, 34 begin moving in opposite directions away from each other, and the physical distance between the eyes 32, 34 and/or ends 22, 24 of the dedicated strand 20 increases. As the eyes 32, 34 move apart, the whip portion 40 of warning indicator fiber 29 (i.e., the end that extends freely outside the cover 25) is drawn back inside the cover 25 until it no longer extends through the cover. If the whip end 40 of the warning indicator 29 is not visible, an inspector or rigger will immediately be able to determine that the sling 10 may have been subjected to a condition that would prevent the lifting core 12 from lifting its maximum rated load and will therefore remove the sling 10 from service for further inspection. The double-back configuration of the indicator fiber 29 ensures that the whip end 40 moves twice the distance compared to the distance the eyes 32, 34 move apart, ensuring that every time a trigger event occurs, the whip end 40 will completely disappear. (It should be noted that the whip end 40 of the warning indicator 29 may be shaded in a high visibility color or otherwise marked, so that its visibility or lack thereof will be more noticeable.) An important feature is that the ring 26 is designed to fail before damage occurs to the lifting core, thereby warning the riggers that they must either stop using the sling 10 in the WO 2006/127489 PCT/US2006/019518 18 manner in which they are using it or, if they continue, the sling 10 will be permanently damaged. If the rigger stops using the sling, the integrity of the lifting core 12 may remain intact. In this case, the sling 10 can be returned to the manufacturer and the pre-failure warning indicator 11 can be replaced or repaired; usually only the ring 26 will have to be replaced. A primary advantage of the pre-failure warning indicator 11 in accordance with this invention is that the ring 26 may be designed to more precisely fail at a controlled point (regardless of whether it is at a specific strength, abrasion, temperature, etc.). The ring 26 can be used as an indicator of an overload condition by making it weaker than the individual core strands 17. In a second embodiment, the ring 26 can be made from a material that would fail from yarn-on-yarn abrasion damage. In a third embodiment, the ring 26 can be made to fail from excessive temperatures (either heat or cold, or both). In a fourth embodiment, the ring 26 could be made from a material that would deteriorate in the presence of chemicals at a concentration lower than would damage the strands 17 of the load-bearing core. In still another embodiment, the ring 26 can be made of a material or combination of materials that would fail when subjected to more than one of the pre-determined conditions (e.g., overload and excessive heat). In all of the above conditions, the ring 26 is preferably designed to fail at the pre- determined or desired condition at a relatively precise point. For example, if the sling is rated to lift 6,000 pounds (with a five-to-one design factor), the ring 26 can be designed to break relatively close to 24,000 pounds every time. Therefore, the ring 26 can be made to fail before the built-in safety factor of 30,000 pounds and well before any damage occurs to the sling 10. The use of the predictable pre-failure warning indicator 11 as disclosed herein, WO 2006/127489 PCT/US2006/019518 19 gives a sling manufacturer a more predictable and accurate way of incorporating a failure notification means into any sling it designs or makes. In other words, the present invention introduces a degree of predictability into the manufacturing of roundslings since the failure point of the ring 26 can be selected and consistently reproduced. In prior art tell-tail indicators, the failure point was unpredictable and was not consistently reproducible. A prototype was made in order to meet the following requirements: Tensile strength of 30,000 lbs.; Vertical Rated Capacity = 6,000 lbs. at a 5 to 1 design factor; Overload Warning Indicator triggers at 20,000 - 25,000 lbs. with a Design Factor between 3 & 4 to 1; Lightweight: 6' prototype weighs 1.7 lbs; Double contrasting color cover: Outer Green and inner Red for easy cut inspection; Low stretch; Impervious to salt water and most chemicals including oil, diluted acids and bases; Made with K-Spec® proprietary blend of high performance core yarn. The above prototype was tested and it was determined that the whip 40 of the pre- failure warning indicator 11 consistently disappeared (meaning that ring 26 consistently broke) at between 23,000 and 24,000 lbs. and the final tensile strength of the sling 10 was 32,860 lbs. WO 2006/127489 PCT/US2006/019518 20 When the whip 40 of the warning indicator 29 is no longer visible, the sling 10 should be returned to the sling manufacturer for inspection and/or repair. The ring 26 consistently broke before damage occurred to either the dedicated strand 20 or the load-bearing core 12. In many cases, the sling manufacturer will only have to replace the ring 26 in order to refurbish the sling and return it service. (In the above example, the ring 26 failed around 24,000 pounds and the sling 10 did not approach its maximum tensile strength of 30,000 pounds.) Under certain conditions, even though the ring 26 may have been designed to fail first, the sling 10 may have degraded to a point where it must be discarded entirely. For example, if the sling 10 was exposed to an acidic environment for an extended period of time, especially after the ring 26 failed, the sling 10 (and, specifically, the strands 17 that make up the load-bearing core) may have been damaged to such an extent that it can no longer meet its rated capacity. (The selection of the material for the core is the primary factor in determining whether the subject sling is impervious to sea water, oil, acids and other chemicals. Also, the cover 25 plays an important factor in protecting the core especially from abrasion or from sharp edges.) It should be noted that a person skilled in the art, after reading the present disclosure could produce equivalent embodiments. For example, even though virtually all synthetic slings have a load-bearing core protected by an outer cover, a sling manufacturer can eliminate the outer cover (or shorten the outer cover) so that the ring 26 is visible. In this embodiment, a dedicated strand is not required and an operator can determine that a sling overload condition (or other failure condition) was met by observing the integrity of the ring 26. WO 2006/127489 PCT/US2006/019518 21 Referring now to Figure 4, another preferred embodiment is disclosed. In this embodiment, pre-failure warning indicator 11a incorporates a plurality of rings 26a, 26b, 26c, etc. connected together (i.e., as links in a chain) between termination eye 32 and termination eye 34. In this manner, a sling 10a can be designed to indicate whether it has been subjected to multiple excessive conditions - any one of which could cause the controlled destruction of one of the linked rings 26a, 26b, 26c, etc. and which would then trigger the warning indicator lla in a similar manner as when there is only one ring 26. (Although this example uses three rings 26a, 26b, and 26c, two rings, four rings or more rings may be used depending on the number of failure conditions the sling manufacturer wishes to incorporate into the sling.) The warning indicator fiber 29 has a secured end and a whip end. The secured end is attached to one termination eye 32; the remainder of the indicator fiber 29 is placed along all of the rings 26a, 26b, 26c; the indicator fiber is then threaded through the other termination eye 34, is double-backed along all the rings, and is finally directed through the slit in the cover 25 where the whip is visible to an operator. For example, as shown in Figure 4, ring 26a could be designed to fail when the sling is subjected to an overload (excessive weight) condition, ring 26b could be designed to fail under an excessive heat condition, and ring 26c could be designed to fail when exposed to a specific concentration of a particular chemical. Therefore, if the sling is subjected to any of the pre-determined failure conditions, one of the rings 26a, 26b, 26c will fail, causing the termination eyes 32, 34 to pull away from one another, thereby causing the whip portion 40 of the warning indicator whip 29 to completely retract inside the cover 25. In this manner, a single predictable pre-failure warning indicator 11c can be used to signal one of a multiple possible failure conditions. By marking the individual rings before assembly of the sling, one WO 2006/127489 PCT/US2006/019518 22 can determine the exact condition which the sling was subjected to that caused the pre-failure warning indicator to trigger. So, for example, if ring 26b failed (and ring 26a and ring 26c remained intact), the sling manufacturer would know that the sling was subjected to a high temperature for an extended period of time. An improved synthetic roundsling having multiple cores is manufactured by Slingmax, Inc. and is disclosed in U.S. Pat. No. 4,850,629 to Dennis St. Germain. An embodiment disclosed in U.S. Pat. No. 4,850,629 is a two-core roundsling (sold under the brand name TWIN-PATH®) which has two-load lifting cores inside a single cover. The cover is also divided into two separate paths. U.S. Pat. No. 4,850,629 is incorporated by reference as if fully set forth herein. Similar to a sling having a single core (and a single pre-failure warning indicator), in a multiple-core or multiple-path roundsling 50, each core incorporates a predictable pre-failure warning indicator 11a, 11b, as taught herein. Referring now to Figure 5, a first dedicated strand 20a is associated with the first core 12a of a two-path sling 50 and a second dedicated strand 20b is associated with the second core of the two-path sling. The dedicated strand 20a is terminated by termination eyes 32a, 34a, and dedicated strand 20b is terminated by termination eyes 32b, 34b, respectively. A ring 26d, 26e, as disclosed previously in a one- path sling 10, is incorporated into each path of the two-path sling 50. Referring now to Figure 6, whip 40a is associated with the predictable pre-warning indicator lla in the first path of the sling 50, and whip 40b is associated with the predictable pre-warning indicator 11b in the second path. (It should be noted that the warning indicator fiber 29a is attached to one termination eye 32a, threaded through the other termination eye 34a, and the whip end 40a is passed through the cover 25a, and operates in a similar manner WO 2006/127489 PCT/US2006/019518 23 as the "basic" single-path sling 10 illustrated in Figures 1 through 3 using only one ring 26. Similarly, warning indicator strand 29b is attached to one termination eye 32b, threaded through the other termination eye 34b, and the respective whip end 40b is passed through the cover, and operates in a similar manner as when there is only one ring 26.) Sling 50 is comprised of a two-path core; as illustrated in Figure 6 the warning indicator whips 40a and 40b are passed through the cover 25a and emerge in free extension apart from the cover 25a. This embodiment provides a pre-failure indicator for each path that can convey sling damage or overload when either core of the TWIN-PATH® sling is subjected to a load which exceeds its tensile strength or rated capacity. When this happens, one or both of the extended warning indicator whips, 40a and/or 40b, which emerge outside of the cover material 25a will retract completely within the cover thereby alerting the operator or rigger to a sling overload condition. In a Twin-Path® sling having exactly two cores, each core is identical to the other. Referring again to Figure 5, an interesting variation for a two-core sling is the ability to design into the sling two distinct and separate damage-indicating parameters into a single sling. For example, in the first path, the ring 26d could be designed to fail only at a lower tensile strength than the core 12; while in the second path, the ring 26e could be designed to fail only when the sling is exposed to a certain chemical in the environment. The whips 40a, 40b of warning indicators 29a and 29b can be marked or coded in order to indicate which whip is associated with which ring so that if a ring breaks, the rigger will know the condition that was exceeded (i.e., if ring 26d breaks it was because the TWIN-PATH® sling was subjected to a load approaching it's maximum load rating; alternatively, if ring 26e breaks if was because the TWIN-PATH® sling was exposed to the chemical for a period of time such WO 2006/127489 PCT/US2006/019518 24 that it deteriorated the integrity of the sling). Therefore, if a three-core sling is made, three separate conditions may be simultaneously and independently tested using the predictable pre-failure indicator 11 taught herein; a four-core sling can be used to simultaneously test for four separate conditions, etc. In this manner, if the two-path sling 50 is subjected to either one of the pre-selected conditions to a point that causes either ring 26d or ring 26e to fail, the rigger will be alerted and will have more information than would otherwise be available to him. Designing the rings 26d, 26e to fail under different situations may also assist the sling manufacturer in analyzing the sling or further improving the sling, if the sling is ever returned for inspection or repair. However, there are situations in which it will be necessary to design the rings 26d and 26e to fail under the same condition (e.g., an overload condition). The pre-failure warning indicator 11 in accordance with the present invention is designed with a trigger mechanism that will generate a magnified force on the whip end 40 of the external warning indicator 29 in order to move the whip end 40 out-of-sight almost instantaneously, if any of the pre-engineered conditions are met and the ring fails. The reason why the force on the whip end 40 of the warning indicator fiber 29 is magnified is because of the double-back design of the warning indicator fiber 29 through the termination eyes 32,34. After the ring 26 breaks, the termination eyes 32 and 34 separate at a certain speed; however, since the warning indicator fiber 29 is tied to one eye 32, threaded through the opposite eye 34, and doubles-back along the ring before emerging through the cover 25, the whip end 40 of the warning indicator is moving twice as fast (and twice the distance) as the speed (and distance) at which the eyes 32, 34 are moving away from each other. Accordingly, the whip WO 2006/127489 PCT/US2006/019518 25 end 40 withdraws inside the cover entirely so that there is no question as to whether a trigger event occurred. Another feature to note, is that because the whip 40 of the warning indicator 29 is moving so fast, it creates a sound that is audible to the operator. Therefore, the present invention not only gives a visual indication that a sling has reached a critical damage point, but also gives an audible warning. The audible warning is especially important when the sling is positioned so that the operator cannot see the whip 40 (e.g., when the sling is hanging thirty feet in the air). Another notable feature of the subject pre-failure warning indicator 11 is the ability to warn the rigger of an overload and other dangerous situations without affecting the overall strength of the roundsling 10. If the rigger stops lifting the load promptly after the pre-failure warning indicator 11 is triggered, the sling 10 retains 100% of its residual strength. The color code safety feature of this invention may be achieved by encasing the load- bearing core in two separate covers, each cover having a different color. For example, the outer cover could be green or blue, and the inner cover could be orange or red; since the inner cover is a different color from the outer cover, it will show through whenever the outer cover is cut or worn through. This double-cover feature provides a visible safety warning for any user of the sling that abrasion or other damage not normally detectable, has occurred. In another embodiment of the present invention, a pre-failure warning indicator 11 can be adapted with a sabotage or tamper-evident means. Referring now to Figure 7, a tamper- evident tag 35 is attached to either the dedicated indicator strand 20 or, preferably, to one of the eyes 32 or 34. The free end of the tamper-evident tag 35 is passed through the cover via a slit. The slit can be the same one through which the whip 40 passes through. WO 2006/127489 PCT/US2006/019518 26 If the pre-failure warning indicator 11 is triggered (by, for example, an overload condition), this means that ring 26 has been broken, the ends 22, 24 of the dedicated strand 20 are free, causing whip 40 to withdraw completely within the cover. Upon inspection, the tamper-evident tag 35 can be easily pulled out from inside the cover 25 along with a portion of the dedicated strand 20, as illustrated in Figure 8, when the pre-failure warning indicator 11 has been triggered. If the whip end 40 of the warning indicator is not visible because of an intentional intervention by a user, the tamper-evident tag 35 will remain secure and cannot be pulled from the cover 25. In this manner, sabotage of the sling 10 can be evidenced by the supervisor on the work site. (In order to avoid work, some users will cut off the whip end 40 of the warning indicator 29 in an attempt to make it appear that the sling was subjected to a damage situation and, therefore, work must be temporarily stopped so that the sling can be removed for inspection and, if necessary, replaced with a new sling.) As part of the inspection process, the inspector may yank on the tamper-evident tag 35. If the tag is secure, the sling 10 is useable; but, if the tamper-evident tag 35 can be pulled out from inside the cover, the sling 10 must be removed from use because the pre-failure warning indicator 11 has been triggered. Of course, if a saboteur cuts both the whip end 40 and the visible portion of the tamper-evident tag 35, the inspector will immediately know that the sling 10 has been tampered with, and should remove the sling from service. It is important to note that no other prior warning indicators have the ability to quickly inspect the condition of a roundsling. Also, prior warning indicators are not as accurate as the subject warning indicator 11. If the whip end 40 of the warning indicator is visible and the cover 25 is intact, the roundsling can be used for the next lift; if the whip end 40 of the warning indicator is not visible, the sling should be removed from service and inspected. WO 2006/127489 PCT/US2006/019518 27 The subject pre-failure warning indicator is the first completely pass/fail inspection system - it is a completely objective test and not subjective. It should also be noted that one skilled in the art, after reading this disclosure, may develop variations that are contemplated as being equivalent in scope to the various embodiments specifically set forth in the present disclosure. For example, the termination loops 32, 34 may be eliminated and the ends of the dedicated strand 20 may be tied directly to the ring 26. (Alternatively, slip-knots or other means may be used to secure the ends of the strand 20 to the ring 26.) Although this invention has been described and illustrated by reference to specific embodiments, it will be apparent to those skilled in the art that various changes, modifications and equivalents may be made which clearly fall within the scope of this invention. The present invention is intended to be protected broadly within the spirit and scope of the appended claims. ***** WO 2006/127489 PCT/US2006/019518 28 CLAIMS I Claim: 1. A roundsling which comprises: a) a load-bearing core; b) a pre-failure warning indicator means including: i) a strand, having a first end terminated by a first eye and a second end terminated by a second eye, said strand placed proximate the lifting core; ii) a ring adapted to join said eyes to form an endless loop of the strand, wherein said ring is designed to fail from one or more predetermined conditions and said failure occurs before said lifting core is damaged; and iii) a warning indicator fiber having a secured end and a whip end, the secured end of said warning indicator being attached to the first eye of the strand, and the whip end of said warning indicator fiber being directed along the ring, threaded through the second eye of said strand and double-backed along the ring; and c) a cover means for covering the lifting core and the pre-failure warning indicator, said cover having at least one slit from which said whip end of the warning indicator fiber emerges and extends so that the whip end is visible upon a cursory inspection. 2. The roundsling of claim 1 wherein said ring has a lower tensile strength than the load-bearing core. WO 2006/127489 PCT/US2006/019518 29 3. The roundsling of claim 2 wherein said ring fails at a pre-determined force well before damage can occur to the load-bearing core, said ring failure causing the first eye and second eye to separate with respect to each other and drawing the whip end of the warning indicator inside the cover so that it is no longer visible. 4. The roundsling of claim 3 wherein said whip end of the warning indicator moves so quickly as it withdraws within the cover that it makes an audible indication. 5. The roundsling of claim 2 wherein when the roundsling is subjected to a force of approximately 70% of its rated maximum load, the ring breaks, causing the whip end to withdraw completely inside the cover, thereby providing a visual indication to any observer that the sling has been subjected to a possible overload condition and may have been damaged. 6. The roundsling of claim 1 wherein said ring is more susceptible to break from yarn-on-yarn abrasion damage than the load-bearing core. 7. The roundsling of claim 1 wherein said ring is more susceptible to break from excessive temperatures than the load-bearing core. 8. The roundsling of claim 1 wherein said ring is more susceptible to break from the deterioration of chemicals than the load-bearing core. WO 2006/127489 PCT/US2006/019518 30 9. The roundsling of claim 1 wherein said strand of the pre-failure warning indicator is twisted around the load-bearing core. 10. The roundsling of claim 1 wherein the load-bearing core is formed by twisting a plurality of yarns together to form a single strand and then wrapping the single strand into endless parallel loops. 11. The roundsling of claim 10 wherein said load-bearing core comprises one of the following materials: a) aramid material strands; b) K-Spec ® strands (a proprietary blend of high performance fibers); c) polyester strands; d) polyethylene strands; e) HMPE strands; or f) LCP strands. 12. The roundsling of claim 11 wherein said strand of the pre-failure warning indicator is made from the same load-bearing material as the load-bearing core. 13. The roundsling of claim 1 comprising a second cover means that encloses said cover means, said second cover means having a different color than the enclosed cover means. WO 2006/127489 PCT/US2006/019518 31 14. The roundsling of claim 1 further comprising a tamper-evident indication means including a tag having a first end and a second end, the first end of said tag attached to the strand of the pre-failure warning indicator, the second end of said tag threaded through the slit in the cover, the tamper-evident indication means designed to remain stationary as long as the ring's integrity remains intact, and if the sling has been subjected to a pre-determined condition such that the ring breaks, the tamper-evident indication means can be pulled out from inside the cover. 15. The roundsling of claim 14 in which said first end of the tag is attached to an eye of the pre-failure warning indicator. 16. A pre-failure warning indicator for use with an industrial sling, the pre-failure warning indicator comprising: a) a strand, having a first end terminated with a first eye loop and a second end terminated with a second eye loop; b) a ring adapted to join said eyes to form an endless loop of the strand, wherein said ring is designed to break from one or more predetermined conditions; and c) a warning indicator fiber having a secured end and a whip end, wherein said secured end is attached to the first eye of the strand and said whip end is threaded through the second eye of the strand. 17. The pre-failure warning indicator of claim 16 wherein said ring is designed to break at a predetermined tensile strength. WO 2006/127489 PCT/US2006/019518 32 18. The pre-failure warning indicator of claim 16 wherein said ring is designed to break when subjected to a predetermined temperature. 19. The pre-failure warning indicator of claim 16 wherein said ring is designed to break when subjected to a predetermined concentration of specific chemicals. 20. The pre-failure warning indicator of claim 16 wherein said pre-failure warning indicator is designed to make an audible indication when the indicator is triggered. 21. The pre-failure warning indicator of claim 16 comprising a tamper indication means including a tag having a first end and a second end, the first end of said tag attached to the strand of the pre-failure warning indicator, said tag designed to remain stationary as long as the ring's integrity remains intact, and if the sling has been subjected to a pre-determined condition such that the ring breaks, the tamper indication means can be pulled out from inside the cover. 22. The roundsling of claim 21 wherein said first end of the tag is attached to an eye of the pre-failure warning indicator. ABSTRACT Title : SLING WITH PREDICTABLE PRE-FAILURE WARNING INDICATOR The pre-failure warning indicator (11) is provided for use with a sling (10). The pre-failure warning indicator (11) triggers at a point that is predictable within a relatively narrow range, thereby increasing the possibility that a damaged sling (10) is removed from use. The pre-failure warning indicator (11) includes a dedicated strand of material (20) that is placed in close proximity to the load- bearing core yarns (17) of the sling (10) but remains separate and independent from the core yarns (17); the ends (22,24) of the dedicated strand are connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is visible to operators/riggers work in conjunction with the sacrificial strand (20) and the ring (26) is designed to fail when the sling (10) is subjected to a specifically chosen condition (e.g. excessive weight). The failure of the ring (26) causes the warning fiber (20) to withdraw from the rigger's view thereby warning he rigger that the sling (10) was subjected to the specifically chosen condition and may be damaged. The pre-failure warning indicator (11) is provided for use with a sling (10). The pre-failure warning indicator (11) triggers at a point that is predictable within a relatively narrow range, thereby increasing the possibility that a damaged sling (10) is removed from use. The pre-failure warning indicator (11) includes a dedicated strand of material (20) that is placed in close proximity to the load- bearing core yarns (17) of the sling (10) but remains separate and independent from the core yarns (17); the ends (22,24) of the dedicated strand are connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is visible to operators/riggers work in conjunction with the sacrificial strand (20) and the ring (26) is designed to fail when the sling (10) is subjected to a specifically chosen condition (e.g. excessive weight). The failure of the ring (26) causes the warning fiber (20) to withdraw from the rigger's view thereby warning he rigger that the sling (10) was subjected to the specifically chosen condition and may be damaged.

Full Text

WO 2006/127489 PCT/US2006/019518
SLING WITH PREDICTABLE PRE-FAILURE WARNING INDICATOR
CROSS-REFERENCE TO RELATED APPLICATION
The present application claims the benefit under any applicable U.S. statute, including
35 U.S.C. § 120, to U.S. Application No. 11/418,597 filed 05 May 2006, in the name of
Dennis St. Germain and titled Sling With Predictable Pre-Failure Warning Indicator, and
claims the benefit under any applicable U.S. statute, including 35 U.S.C. § 119(e), to U.S.
Provisional Application No. 60/683,987 filed 23 May 2005, in the name of Dennis St.
Germain and titled Sling Having Predictable Pre-Failure Warning Indicator and Associated
Method.
This application incorporates by reference U.S. Application No. 11/418,597 and U.S.
Provisional Application No. 60/683,987 as if both are fully set forth herein.
FIELD OF THE INVENTION
This invention relates generally to industrial slings used to lift, move and transport
heavy loads and, more particularly, an apparatus for notifying operators/riggers who use
synthetic slings of an overload or damage situation that may lead to sling failure.
BACKGROUND OF THE INVENTION
Wire rope slings made of a plurality of metal strands twisted together and secured by
large metal sleeves or collars are common in the industry. During the past thirty years,
industrial metal slings have seen improvements in flexibility and strength. However,
compared to non-metal or synthetic fiber slings, metal slings are relatively stiff and inflexible.

WO 2006/127489 PCT/US2006/019518
2
Synthetic fiber slings have gained popularity over the last fifteen years and are
replacing metal slings in many circumstances. Synthetic slings are usually comprised of a
lifting core made of twisted strands of synthetic fiber and an outer cover that protects the
core. The most popular design of synthetic slings is a roundsling in which the lifting core
forms a continuous loop and the sling has a circular or oval-shaped appearance.
An advantage of synthetic slings is that they have a very high load-lifting performance
strength-to-weight ratio which provides for a lighter, more flexible and even stronger slings
than their heavier and bulkier metal counterparts. Even with such advances in the art of sling
making, the riggers who use these improved synthetic slings still suffer and endure some of
the age old problems of sudden failure and loss of a load caused by a sling breaking without
warning because it was fatigued (or overly stretched) from being subjected previously to
overload conditions. After a sling has been fatigued, it does not usually provide any physical
indication that it was damaged - even to the trained eye. (One of the few advantages of a
metal sling over a non-metal sling is that there is equipment available that can be used to
conduct a non-destructive test of the metal. For example, similar equipment is routinely used
to determine whether the wings of an airplane have become fatigued.)
Standard break tests have been established for determining how large of a load a sling
can endure. Slings are attached to a testing machine that applies a steady but increasing force
on the sling until it is unable to withstand the stress of the force being applied to it and the
sling ultimately breaks. Such break tests have enabled manufacturers of industrial slings to
rate the load-bearing capacity of the sling. The load capacity is determined to be a point well
below the load used to break the sling and also below the point where the sling is fatigued or
damaged. Most sling manufacturers will affix some type of tag notice on the sling which

WO 2006/127489 PCT/US2006/019518
3
states the load capacity (rated capacity) of the particular sling. This rated capacity gives the
maximum amount of load to which the sling may be subjected and still be considered a safe
use of the sling.
Unfortunately, even conscientious operators/riggers who do not take unsafe shortcuts
and who operate in a safe responsible manner sometimes are surprised by a sling breaking in
use even when they believed it was being used within the load limits of its rated capacity. For
example, when industrial slings are in continuous heavy use over three shifts around the
clock, the operators on a later shift may not be aware that someone on an earlier shift had
subjected the sling to a substantial overload which may have caused serious damage to the
lifting core strands of the sling. When a synthetic fiber sling is overloaded beyond its tensile
strength or weight-lifting capacity at maximum stretch, it is considered to be fatigued and
may never return to its normal strength and load bearing capacity.
When subjected to an overload condition above its rated capacity, a roundsling can be
permanently damaged/deformed if the load stretches the fibers of the load bearing core
material beyond their yield point. An over-loaded sling may be susceptible to fracture at a
stress point. This condition is similar to the stretching of a rubber band beyond its point of
normal elasticity so that when the load or tension is removed or relieved, the rubber band will
never regain its normal configuration and its strand dimensions may be permanently stretched
which will cause it to fail under a load which is less than its tensile strength load. As stated
previously, it is nearly impossible to determine, upon a cursory visual inspection, that a sling
has been damaged because of the large size of such slings (on the order of 6 feet or more) and
because the load-bearing core is hidden inside the outer cover.
Once the load-lifting core of the synthetic sling is stretched beyond its yield point, it

WO 2006/127489 PCT/US2006/019518
4
can actually change in its physical structure and be restricted at a stress point. To date, there
has been no precise method or apparatus available to an operator or rigger to determine if a
sling with a protective cover was subjected to an overload or damage-causing condition. If a
roundsling has been fatigued or structurally changed, the sling may no longer lift a load
according to its maximum rated load capacity and, most importantly, becomes a serious threat
to the operators and riggers using the sling.
Thousands of roundslings are being used on a daily basis in a broad variety of heavy
load lifting applications which range from ordinary construction (e.g., skyscrapers and
bridges), plant and equipment operations, to ship building (e.g., oil rigs), nuclear power plants
and the like. The lifting core fibers of such roundslings may be derived from natural or
synthetic materials, such as polyester, polyethylene, nylon, and the like. Although the outer
covers of synthetic slings are designed to reduce damage, the core fibers are still susceptible
to damage from abrasion, cutting by sharp edges, or degradation from exposure to heat, cold,
ultraviolet rays, corrosive chemicals or gaseous materials, or other environmental pollutants.
In certain instances, the core yarn of a synthetic sling could weaken, melt or
disintegrate when subjected to elevated temperatures, or to prolonged exposure to either
ultraviolet light or chemicals. Still another safety concern flows from abuse by the user when
the core yarn is damaged from abrasive wear when the slings are not rotated and the same
wear points are permitted to stay in contact for extended periods of time with a device used
for lifting (such as hooks on a crane), or on the edges of the load itself. Such abrasion is
accelerated for certain types of synthetic fiber material and especially if the load contact
section is under compression or is bunched. Riggers in the field are concerned that the inner
lifting core yarn of their roundslings may be damaged on the inside without a means for them

WO 2006/127489 PCT/US2006/019518
5
to detect such defects through the sling cover. Even if the cover is removed it may be
impossible to tell if the lifting core has been damaged to the point where it cannot lift its rated
load. Since there is no reasonable non-destructive testing techniques for synthetic fiber
slings, a synthetic sling that is only suspected of being damaged must be removed from
service for safety reasons.
The structural integrity of the roundsling lifting core material is difficult to determine
when it is hidden inside a protective cover of opaque material which renders the lifting core
yarn inaccessible for inspection. A stretched or fatigued roundsling could experience a
sudden catastrophic failure without warning to the rigger, which may result in the loss of lives
and property. Many in the industry have sought to provide safe slings to its riggers to avoid
bodily injury, property damage and product liability claims.
Several roundsling constructions are known which have a failure indicator. For
example, it is known in the art to incorporate a failure indicator synthetic strand as an integral
member of the lifting or load-bearing core. The failure indicator strand in prior art
constructions was always an extension of the core yarns.
A popular design of prior art roundslings was to twist a plurality of yarns together to
form a single strand; the strand is then rolled into an endless parallel loops of strands that
form the core, which is then encased in a protective cover material. If the sling was designed
with a prior art failure indicator, an indicator strand would be incorporated into and twisted
with the core yarns. The two ends of the indicator strand (sometimes referred to as tell-tails),
extend freely through an opening in the cover material. When the sling is subjected to an
overload condition, the tell-tail would partially withdraw within the cover and the freely
extending tell-tail ends would be visibly shorter than the tell-tails of an undamaged sling; if

WO 2006/127489 PCT/US2006/019518
6
the overload condition exceeded the maximum rated load of the sling, one or both tell-tails
would usually withdraw completely within the cover. In either event, the rigger is warned of
the occurrence of a potentially damaged sling by either the absence of one or both tell-tails, or
a "significant" withdraw of at least one tell-tail inside the cover. However, there usually was
no consistency on how the tell-tails would react when triggered, even when the slings were
manufactured under identical conditions.
A drawback of prior art failure indicators based on an indicator strand is that there is
no predictable way of determining when the failure indicator will be triggered. Synthetic
slings have a safety factor designed into their construction. For example, if the sling is rated
at 6,000 pounds, it typically will not be damaged unless the sling is subjected to a force five
times greater (i.e., around 30,000 pounds, a 5-to-1 design factor) than the rated capacity; the
tell-tail may be triggered and indicate an overload condition when the sling is subject to a
force of between four to five times the rated capacity (i.e., about 24,000 lbs) by retracting into
the sling's cover. Therefore, the tell-tail will provide a visual indication that the sling may
have been damaged or subjected to a situation that may have been detrimental to the overall
condition of the sling before the sling actually is subjected to such a condition.
Unfortunately, there was no way of ensuring that the tell-tails would consistently withdraw
within the cover at about 24,000 pounds. In other words, two slings having prior art
failure indicator strands contemporaneously made under the same conditions would have two
different trigger points (for example, one sling may trigger at about 22,050 pounds and the
other sling may trigger at about 26,000 pounds). In addition, one sling may react to a trigger
event by completely withdrawing one of the tell-tails, while the other sling may react to a
trigger event by partially withdrawing both tell-tails.

WO 2006/127489 PCT/US2006/019518
7
If the tell-tail is not withdrawn completely within the cover, one rigger's opinion of a
"significant withdrawal" towards the opening in the cover may differ from another rigger's
opinion. Therefore, a "small" movement of one or both of the tell-tails, which may result
from the constant use and handling of the sling, may appear to one rigger as an indication that
an overload condition was reached when, in fact, the sling was not subjected to an overload
condition. Therefore, the visual inspection of the tell-tails in prior art failure indicators and
the eventual determination of a trigger event becomes a subjective test.
Another prior art roundsling construction utilizes an optical fiber strand that enables
the operator/rigger to test it by shining a light on one end of the optical fiber to determine if
the light can be seen at the other end of the optical fiber. In U.S. Patent No. 5,651,572 to
Dennis St. Germain, it is taught to incorporate a flexible fiber optic "signal" cable into the
lifting core strands of the roundsling.
As indicated previously, in a roundsling, the lifting core is configured in endless
parallel loops of strands which are then encased within a protective cover material. The cover
will have openings or orifice slits out of which the two ends of the fiber optic signal strand
emerge. The aforesaid ends of the fiber optic cable are designed to extend freely through a
slit in the sling's cover so that they are easily accessible by the rigger.
The optical signal strand member conducts light from a light source at one end to an
observer looking at the opposite end for testing the integrity and the continuity of the core
strands. The inclusion of the fiber optic cable in the lifting core yarn of the roundsling
converts the inaccessible inner core area into an observable test check area by means of the
passage of light through the fiber optic component of the lifting core.
Fiber optic materials are capable of transmitting light into endless parallel relationship

WO 2006/127489 PCT/US2006/019518
8
with the fibers of the lifting core yarn. This fiber optic signal strand comprises fiber or rod
material which permits the propagation of light that enters the fiber material at one end and is
totally reflected back inward repeatedly from the fiber wall through the entire length of the
fiber optic strand which enables the light being transmitted within the fiber optic cable to pass
from one end of the fiber optic cable to the other end. If the light emerges at the other end of
the fiber optic cable, it indicates that the integrity of the fiber optic cable throughout the path
of the roundsling lifting core bundle is intact and, by reasoning, the integrity of the lifting
core yarns are also intact.
Since the fiber optic cable member is incorporated into the lifting core of the
roundsling disclosed in U.S. Patent No. 5,651,572, it tends to develop somewhat similar
breaking or snapping characteristics as the lifting core fiber materials. If the fibers of lifting
core yarn break or fracture, then the fiber optic cable will also be damaged which will prevent
the transmission of light from one end to the other end of the emerging fiber optic cable. If
the light fails to pass from one end of the signal fiber optic cable to the other end, then the
rigger is warned that the lifting core strands may be damaged, and to remove the protective
cover from the roundsling for further inspection. If, upon inspection, it is determined that the
roundsling was damaged, it will be immediately removed from service, and replaced with a
new sling.
Although the apparatus disclosed in U.S. Patent No. 5,651,572 is currently the leading
product for determining whether the lifting core yarns of a synthetic sling have snapped or
been damaged, in the stages where the sling has been subjected to an overload condition, the
fiber optic signal strand still does not have the identical stretching properties of the load-
bearing core yarns. Accordingly, unless the fiber optic cable breaks completely, some light

WO 2006/127489 PCT/US2006/019518
9
may still be able to traverse the entire length of the fiber optic cable such that the degradation
in the intensity of the light may be imperceptible to the naked eye.
Alternatively, the fiber optic cable, being more brittle than the synthetic core material,
may be damaged by normal handling (and dropping) of the sling, or at a force less than the
rated capacity of the sling. In such cases, the light transmission through the fiber optic cable
may be disrupted causing the fiber optic cable to indicate an overload condition when, in fact,
no overload condition was reached.
Finally, under other excessive or damage-causing situations (e.g., excessive heat,
acidic or chemical exposure, and ultraviolet exposure) it can be expected that the fiber optic
cable will be affected differently than the synthetic strands of the lifting core. If, for example,
a sling with the fiber optic signal cable is exposed to certain chemicals, the fiber optic signal
cable may be relatively unaffected (or only its exterior surface is affected leaving the light
path through the center of the cable unscathed), while the lifting core has been degraded to
the point where it no longer meets its load rating. Therefore, as stated previously, the need to
precisely determine whether the load bearing core of a synthetic sling was subjected to an
excessive or damage- causing situation still exists.
SUMMARY OF THE INVENTION
The present invention discloses a pre-failure warning indicator for use with a sling
that is more accurate and predictable than prior art indicators. In the present invention, the
failure indicator strand is separate and independent from the load-bearing core yarns.
One of the most popular designs of a roundsling is to twist a plurality of yams
together to form a single strand; the strand is then rolled into endless parallel loops of strands

WO 2006/127489 PCT/US2006/019518
10
that form the core. In accordance with the present invention, a pre-failure warning indicator
includes a separate dedicated strand of material, a ring made of a specially chosen material,
and a separate warning fiber having an elongated indicator whip end.
The dedicated strand is placed proximate and substantially parallel to the loops of core
strands of the sling; the ends of the dedicated strand are brought within close proximity (in a
preferred embodiment several inches) to each other and are terminated with eyes or another
configuration that can secure the ring. The ring is inserted through or secured to both eye
terminations, thereby bridging the gap between the ends of the dedicated strand, and usually
forms an oval-shaped loop. One end of the warning fiber is attached to one of the eyes of the
dedicated strand, and the free end of the warning fiber is placed along the ring and threaded
through the opposite eye; the free end of the warning fiber is then double-backed along the
length of the ring. A tubular cover material encases the lifting core and the pre-failure
warning indicator. The free end of the warning fiber extends through an opening in the cover
material and is referred to as the indicator whip.
In a specific embodiment, a tag is attached to the strand (and preferably one of the
terminating eyes) and is also drawn through the slot so that it extends freely outside the cover.
The tag is designed to provide an indicator that the sling has been tampered with or
sabotaged.
The ring is designed to fail when the sling is subjected to an excessive or damage-
causing situation. A common damage-causing situation is when the sling is over-loaded. The
ring will break when the sling is placed in an overload situation, thereby causing the
termination eyes to separate, resulting in the complete withdrawal of the whip inside of the
cover.

WO 2006/127489 PCT/US2006/019518
11
By choosing the ring carefully, relatively accurate predictions of the force needed to
trigger the warning fiber can be made. In addition, the ring may be chosen to fail and thereby
convey a damage situation when the sling is being used under unusual environmental
conditions (e.g., excessively hot, acidic, or ultraviolet rays from, for example, sunlight).
Previous indicators either of the fiber optic nature or of the tell-tail type could give
false indications of an overload or other internal damage. In the case of fiber optics, the
ability to transmit light can be impeded by dirt, grease, and other debris that can retard the
transmission of light through the fiber optic cable by jamming the ends. In the case of tell-
tails, the movement of the sling's outer cover from friction with a load can give a false
implication that the tell-tails were pulling under the cover when it was really the cover
moving over the tell-tails. In the current invention, these areas of confusion are eliminated by
a simple visual identification of the external warning indicator. Also, the dedicated strand
can be locked into place by permanent attachment to the cover. If the cover shifts, the entire
assembly of this invention moves with it in concert so a false indication of overload is
eliminated.
Additional objects and advantages will be evident to one skilled in the art after a
reading of the detailed description that follows.
BRIEF DESCRIPTION OF THE DRAWINGS
The accompanying drawings, which are incorporated in and form a part of the
specification, illustrate the embodiments of the present invention and, together with the
following description, serve to explain the principles of the invention. For the purpose of
illustrating the invention, there are shown in the drawings embodiments which are presently

WO 2006/127489 PCT/US2006/019518
12
preferred, it being understood, however, that the invention is not limited to the specific
instrumentality or the precise arrangement of elements or process steps disclosed.
In the drawings:
Figure 1 is a perspective view of a single-path roundsling which incorporates a
predictable pre-failure warning indicator in accordance with the present invention;
Figure 2 is an enlarged cross-sectional view of the roundsling illustrated in Figure 1
taken along line 2-2;
Figure 3 is a side view of a pre-failure warning indicator in accordance with the
present invention;
Figure 4 is a side view of another embodiment of a pre-failure warning indicator in
accordance with the present invention, utilizing multiple rings linked together;
Figure 5 is a side view of another embodiment of a pre-failure warning indicator in
accordance with the present invention for use with a two-path sling;
Figure 6 is a perspective view of a two-path sling incorporating the pre-failure
indicator of Figure 5;
Figure 7 is a side view of a pre-failure warning indicator in accordance with the
present invention which also incorporates a sabotage indicator means; and
Figure 8 is a perspective view of a single-path roundsling incorporating the
predictable pre-failure warning indicator of Figure 3 and the sabotage indicator of Figure 7.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
In describing a preferred embodiment of the invention, specific terminology will be
selected for the sake of clarity. However, the invention is not intended to be limited to the

WO 2006/127489 PCT/US2006/019518
13
specific terms so selected, and it is to be understood that each specific term includes all
technical equivalents that operate in a similar manner to accomplish a similar purpose.
The subject invention is an apparatus and method for determining whether a synthetic
fiber sling has been damaged (because of an overload or other condition that could weaken
the sling's load-bearing core) to a point where the sling should be removed from service and
returned to the manufacturer for internal inspection and, if necessary, repair or disposal.
Preferred embodiments of the present invention will now be described in detail with reference
to the accompanying drawings in which a roundsling having a pre-warning failure indicator in
accordance with the present invention is generally indicated at 10. The various preferred
embodiments will be described with reference to the drawing figures that form a part of this
description where like numerals represent like elements throughout.
Figure 1 illustrates a perspective view of a roundsling in accordance with the present
invention. Figure 1 specifically shows a single-path roundsling, but the principles disclosed
herein may be applied to other slings including multiple-path slings. Figure 2 is a cross-
sectional view of the roundsling shown in Figure 1 taken along line 2-2, and illustrates the
primary interior components of a typical roundsling.
Referring to Figures 1 and 2, the roundsling 10 comprises an inner core 12 encased
within an outer protective cover 25. The outer cover 25 shown in Figure 2 is meant to convey
that the cover 25 is larger than the load-bearing core 12 and moves relatively freely with
respect to the load-bearing core 12 and not necessarily that the cover 25 has a cross-sectional
shape of an oval. The core 12 is designed to bear the entire weight of the load to be lifted.
The primary purpose of the outer cover 25 is to prevent physical damage to the core from
abrasion, sharp edges on the load, etc.; the cover 25 will also help to reduce damage to the

WO 2006/127489 PCT/US2006/019518
14
sling when it is used in an environment that will subject it to harsh elements such as heat,
ultraviolet light, corrosive chemicals, gaseous materials, or other environmental pollutants.
As will be explained hereinafter, the cover 25 can also be designed to notify a user when
physical damage has occurred to the cover.
The lifting core 12 is preferably made of a single or multiple strands 17 configured in
a plurality of endless parallel loops of strands to form a single core or multiple cores, all of
which are contained inside the protective cover material 25. The use of a single strand or
multiple strands in this configuration is typical in the construction of roundslings.
The lifting core 12 of such roundslings may be derived from one or more natural or
synthetic materials, such as polyester, polyethylene, nylon, K-Spec® (a proprietary blend of
fibers), HMPE, LCP, para-aramid or other types of synthetics. The material chosen for the
core primarily depends on the maximum weight the sling is designed to lift and environment
in which the sling 10 will be used. Such sling constructions have a high lifting and break
strength, lighter weight, high temperature resistance and high durability, compared to wire
rope or metal chain slings.
Referring now to Figure 3, the pre-failure warning indicator 11 in accordance with the
present invention is illustrated in side view and is shown without the cover 25 and without
core 12. In a preferred embodiment, the sling 10 may be manufactured with only a pre-failure
warning indicator 11, or with both a pre-failure warning indicator 11 and a tamper-evident
means 35. Initially, the operation of the pre-failure warning indicator 11 will be disclosed;
the tamper-evident means 35 will be described later with respect to Figure 7.
A separate (preferably single) strand 20 of yarn is dedicated to the pre-failure warning
indicator 11. The dedicated warning strand 20 is located within cover 25; it is preferably

WO 2006/127489 PCT/US2006/019518
15
placed proximate the core 12 and may either be twisted around the load-bearing strands of the
core 12 or it may just lay next to the core 12, as illustrated in Figure 2.
In a different embodiment, it may be desired to permanently affix the dedicated strand
20 to the inside of the cover 25. When a sling is used over a period of time, the cover will
develop wear points at specific locations, for example, where the sling hangs from a crane's
hook. Accordingly, it is usually advisable to rotate the cover with respect to the load-bearing
core 12. By securing the dedicated strand 20 to the inner cover, movement of the cover
(either intentionally or non-intentionally) will not affect the operation of the pre-failure
warning indicator 11.
First end 22 and second end 24 of the dedicated strand 20 are terminated in eyes 32,
34, respectively. The dedicated strand 20 and eyes 32,34 are preferably made of the same
material as the core strands 17.
The eyes 32,34 are connected by a ring 26, thereby forming an endless loop with the
dedicated strand 20. The shape of the separate dedicated strand 20 generally matches the
shape of the endless parallel loops formed by the core strand 17 (i.e., generally circular or
oval).
Although the term "ring" implies a circularly-shaped object, as used herein "ring" is
defined as any closed link or band that will connect the ends of a dedicated strand.
In one preferred embodiment, the ring 26 is chosen to have a lower tensile strength
than the core 12. The sling manufacturer may choose to do this any number of ways, e.g., by
making the ring 26 out of a different material than the dedicated strand 20, cutting a notch or
notches in the ring to physically weaken it, or by making the ring 26 out of the same material
as, but of a smaller diameter than, the core strands 17. When ring 26 is chosen to have a

WO 2006/127489 PCT/US2006/019518
16
lower tensile strength, the pre-failure warning indicator 11 is designed to trigger and thereby
notify the rigger or other users of the sling that the sling 10 has been subjected to an overload
condition (i.e., the sling was subjected to a force that was pre-determined to compromise the
integrity of the sling, and is sometimes determined to be about four times greater than the
sling's rated capacity).
Attached to first termination eye 32 is a warning indicator fiber 29. Warning indicator
fiber 29 is an elongated strand that is placed substantially parallel to the ring, is threaded
through the second termination eye 34, is then double-backed along the ring 26 towards the
first eye 32, and directed out an opening in the sling cover 25. (The external end 40 of the
warning indicator fiber 29 that extends through the sling cover 25 is sometimes referred to as
a "whip.") Although the sling cover 25 is not shown in Figure 3, the preferred orientation of
the warning indicator fiber 29 is illustrated, i.e., it forms a substantially "J" shape within the
sling cover 25.
Referring again to Figure 1, the whip 40 of the warning indicator 29 extends freely
through cover 25. Although not necessary, cover patch 30 may be attached (preferably by
sewing), to the cover to protect the opening through which the whip end 40 of the warning
indicator 29 extends.
The dedicated strand 20 is preferably made of similar material as the strands 17 of the
load-bearing core 12; this promotes the relatively equal stretching of all components of the
sling 10. In a preferred embodiment, the ring 26 has a pre-selected lower tensile strength than
the material used to make the core strands; in this embodiment, the ring 26 will fail before the
lifting core 12 is stretched or fatigued. Alternatively - or in addition - the ring 26 may be
designed to have a lower resistance to abrasion, heat, cold, and/or chemical exposure. By

WO 2006/127489 PCT/US2006/019518
17
carefully choosing the properties of ring 26, a sling manufacturer can control the condition(s)
under which the subject pre-failure warning indicator 11 will trigger.
In one example, the sling manufacturer may design the ring 26 to fail at 70% of the
tensile strength of the inner core. Accordingly, the material from which ring 26 is made
and/or its cross-sectional thickness may be chosen to meet the pre-selected tensile strength.
When the sling 10 is placed under a load that exceeds its recommended rating, ring 26
will fail before damage can occur to either the load bearing core strands 17 that form the core
12 or the dedicated strand 20. When ring 26 fails, the termination eyes 32, 34 begin moving
in opposite directions away from each other, and the physical distance between the eyes 32,
34 and/or ends 22, 24 of the dedicated strand 20 increases.
As the eyes 32, 34 move apart, the whip portion 40 of warning indicator fiber 29 (i.e.,
the end that extends freely outside the cover 25) is drawn back inside the cover 25 until it no
longer extends through the cover. If the whip end 40 of the warning indicator 29 is not
visible, an inspector or rigger will immediately be able to determine that the sling 10 may
have been subjected to a condition that would prevent the lifting core 12 from lifting its
maximum rated load and will therefore remove the sling 10 from service for further
inspection. The double-back configuration of the indicator fiber 29 ensures that the whip end
40 moves twice the distance compared to the distance the eyes 32, 34 move apart, ensuring
that every time a trigger event occurs, the whip end 40 will completely disappear. (It should
be noted that the whip end 40 of the warning indicator 29 may be shaded in a high visibility
color or otherwise marked, so that its visibility or lack thereof will be more noticeable.)
An important feature is that the ring 26 is designed to fail before damage occurs to the
lifting core, thereby warning the riggers that they must either stop using the sling 10 in the

WO 2006/127489 PCT/US2006/019518
18
manner in which they are using it or, if they continue, the sling 10 will be permanently
damaged. If the rigger stops using the sling, the integrity of the lifting core 12 may remain
intact. In this case, the sling 10 can be returned to the manufacturer and the pre-failure
warning indicator 11 can be replaced or repaired; usually only the ring 26 will have to be
replaced.
A primary advantage of the pre-failure warning indicator 11 in accordance with this
invention is that the ring 26 may be designed to more precisely fail at a controlled point
(regardless of whether it is at a specific strength, abrasion, temperature, etc.). The ring 26 can
be used as an indicator of an overload condition by making it weaker than the individual core
strands 17. In a second embodiment, the ring 26 can be made from a material that would fail
from yarn-on-yarn abrasion damage. In a third embodiment, the ring 26 can be made to fail
from excessive temperatures (either heat or cold, or both). In a fourth embodiment, the ring
26 could be made from a material that would deteriorate in the presence of chemicals at a
concentration lower than would damage the strands 17 of the load-bearing core. In still
another embodiment, the ring 26 can be made of a material or combination of materials that
would fail when subjected to more than one of the pre-determined conditions (e.g., overload
and excessive heat).
In all of the above conditions, the ring 26 is preferably designed to fail at the pre-
determined or desired condition at a relatively precise point. For example, if the sling is rated
to lift 6,000 pounds (with a five-to-one design factor), the ring 26 can be designed to break
relatively close to 24,000 pounds every time. Therefore, the ring 26 can be made to fail
before the built-in safety factor of 30,000 pounds and well before any damage occurs to the
sling 10. The use of the predictable pre-failure warning indicator 11 as disclosed herein,

WO 2006/127489 PCT/US2006/019518
19
gives a sling manufacturer a more predictable and accurate way of incorporating a failure
notification means into any sling it designs or makes. In other words, the present invention
introduces a degree of predictability into the manufacturing of roundslings since the failure
point of the ring 26 can be selected and consistently reproduced. In prior art tell-tail
indicators, the failure point was unpredictable and was not consistently reproducible.
A prototype was made in order to meet the following requirements:
Tensile strength of 30,000 lbs.;
Vertical Rated Capacity = 6,000 lbs. at a 5 to 1 design factor;
Overload Warning Indicator triggers at 20,000 - 25,000 lbs. with a Design
Factor between 3 & 4 to 1;
Lightweight: 6' prototype weighs 1.7 lbs;
Double contrasting color cover: Outer Green and inner Red for easy cut
inspection;
Low stretch;
Impervious to salt water and most chemicals including oil, diluted acids and
bases;
Made with K-Spec® proprietary blend of high performance core yarn.
The above prototype was tested and it was determined that the whip 40 of the pre-
failure warning indicator 11 consistently disappeared (meaning that ring 26 consistently
broke) at between 23,000 and 24,000 lbs. and the final tensile strength of the sling 10 was
32,860 lbs.

WO 2006/127489 PCT/US2006/019518
20
When the whip 40 of the warning indicator 29 is no longer visible, the sling 10 should
be returned to the sling manufacturer for inspection and/or repair. The ring 26 consistently
broke before damage occurred to either the dedicated strand 20 or the load-bearing core 12.
In many cases, the sling manufacturer will only have to replace the ring 26 in order to
refurbish the sling and return it service. (In the above example, the ring 26 failed around
24,000 pounds and the sling 10 did not approach its maximum tensile strength of 30,000
pounds.)
Under certain conditions, even though the ring 26 may have been designed to fail first,
the sling 10 may have degraded to a point where it must be discarded entirely. For example,
if the sling 10 was exposed to an acidic environment for an extended period of time,
especially after the ring 26 failed, the sling 10 (and, specifically, the strands 17 that make up
the load-bearing core) may have been damaged to such an extent that it can no longer meet its
rated capacity. (The selection of the material for the core is the primary factor in determining
whether the subject sling is impervious to sea water, oil, acids and other chemicals. Also, the
cover 25 plays an important factor in protecting the core especially from abrasion or from
sharp edges.)
It should be noted that a person skilled in the art, after reading the present disclosure
could produce equivalent embodiments. For example, even though virtually all synthetic
slings have a load-bearing core protected by an outer cover, a sling manufacturer can
eliminate the outer cover (or shorten the outer cover) so that the ring 26 is visible. In this
embodiment, a dedicated strand is not required and an operator can determine that a sling
overload condition (or other failure condition) was met by observing the integrity of the ring
26.

WO 2006/127489 PCT/US2006/019518
21
Referring now to Figure 4, another preferred embodiment is disclosed. In this
embodiment, pre-failure warning indicator 11a incorporates a plurality of rings 26a, 26b, 26c,
etc. connected together (i.e., as links in a chain) between termination eye 32 and termination
eye 34. In this manner, a sling 10a can be designed to indicate whether it has been subjected
to multiple excessive conditions - any one of which could cause the controlled destruction of
one of the linked rings 26a, 26b, 26c, etc. and which would then trigger the warning indicator
lla in a similar manner as when there is only one ring 26. (Although this example uses three
rings 26a, 26b, and 26c, two rings, four rings or more rings may be used depending on the
number of failure conditions the sling manufacturer wishes to incorporate into the sling.)
The warning indicator fiber 29 has a secured end and a whip end. The secured end is
attached to one termination eye 32; the remainder of the indicator fiber 29 is placed along all
of the rings 26a, 26b, 26c; the indicator fiber is then threaded through the other termination
eye 34, is double-backed along all the rings, and is finally directed through the slit in the
cover 25 where the whip is visible to an operator.
For example, as shown in Figure 4, ring 26a could be designed to fail when the sling
is subjected to an overload (excessive weight) condition, ring 26b could be designed to fail
under an excessive heat condition, and ring 26c could be designed to fail when exposed to a
specific concentration of a particular chemical. Therefore, if the sling is subjected to any of
the pre-determined failure conditions, one of the rings 26a, 26b, 26c will fail, causing the
termination eyes 32, 34 to pull away from one another, thereby causing the whip portion 40 of
the warning indicator whip 29 to completely retract inside the cover 25. In this manner, a
single predictable pre-failure warning indicator 11c can be used to signal one of a multiple
possible failure conditions. By marking the individual rings before assembly of the sling, one

WO 2006/127489 PCT/US2006/019518
22
can determine the exact condition which the sling was subjected to that caused the pre-failure
warning indicator to trigger. So, for example, if ring 26b failed (and ring 26a and ring 26c
remained intact), the sling manufacturer would know that the sling was subjected to a high
temperature for an extended period of time.
An improved synthetic roundsling having multiple cores is manufactured by
Slingmax, Inc. and is disclosed in U.S. Pat. No. 4,850,629 to Dennis St. Germain. An
embodiment disclosed in U.S. Pat. No. 4,850,629 is a two-core roundsling (sold under the
brand name TWIN-PATH®) which has two-load lifting cores inside a single cover. The
cover is also divided into two separate paths. U.S. Pat. No. 4,850,629 is incorporated by
reference as if fully set forth herein.
Similar to a sling having a single core (and a single pre-failure warning indicator), in a
multiple-core or multiple-path roundsling 50, each core incorporates a predictable pre-failure
warning indicator 11a, 11b, as taught herein. Referring now to Figure 5, a first dedicated
strand 20a is associated with the first core 12a of a two-path sling 50 and a second dedicated
strand 20b is associated with the second core of the two-path sling. The dedicated strand 20a
is terminated by termination eyes 32a, 34a, and dedicated strand 20b is terminated by
termination eyes 32b, 34b, respectively. A ring 26d, 26e, as disclosed previously in a one-
path sling 10, is incorporated into each path of the two-path sling 50.
Referring now to Figure 6, whip 40a is associated with the predictable pre-warning
indicator lla in the first path of the sling 50, and whip 40b is associated with the predictable
pre-warning indicator 11b in the second path. (It should be noted that the warning indicator
fiber 29a is attached to one termination eye 32a, threaded through the other termination eye
34a, and the whip end 40a is passed through the cover 25a, and operates in a similar manner

WO 2006/127489 PCT/US2006/019518
23
as the "basic" single-path sling 10 illustrated in Figures 1 through 3 using only one ring 26.
Similarly, warning indicator strand 29b is attached to one termination eye 32b, threaded
through the other termination eye 34b, and the respective whip end 40b is passed through the
cover, and operates in a similar manner as when there is only one ring 26.)
Sling 50 is comprised of a two-path core; as illustrated in Figure 6 the warning
indicator whips 40a and 40b are passed through the cover 25a and emerge in free extension
apart from the cover 25a. This embodiment provides a pre-failure indicator for each path that
can convey sling damage or overload when either core of the TWIN-PATH® sling is
subjected to a load which exceeds its tensile strength or rated capacity. When this happens,
one or both of the extended warning indicator whips, 40a and/or 40b, which emerge outside
of the cover material 25a will retract completely within the cover thereby alerting the
operator or rigger to a sling overload condition.
In a Twin-Path® sling having exactly two cores, each core is identical to the other.
Referring again to Figure 5, an interesting variation for a two-core sling is the ability to
design into the sling two distinct and separate damage-indicating parameters into a single
sling. For example, in the first path, the ring 26d could be designed to fail only at a lower
tensile strength than the core 12; while in the second path, the ring 26e could be designed to
fail only when the sling is exposed to a certain chemical in the environment. The whips 40a,
40b of warning indicators 29a and 29b can be marked or coded in order to indicate which
whip is associated with which ring so that if a ring breaks, the rigger will know the condition
that was exceeded (i.e., if ring 26d breaks it was because the TWIN-PATH® sling was
subjected to a load approaching it's maximum load rating; alternatively, if ring 26e breaks if
was because the TWIN-PATH® sling was exposed to the chemical for a period of time such

WO 2006/127489 PCT/US2006/019518
24
that it deteriorated the integrity of the sling). Therefore, if a three-core sling is made, three
separate conditions may be simultaneously and independently tested using the predictable
pre-failure indicator 11 taught herein; a four-core sling can be used to simultaneously test for
four separate conditions, etc.
In this manner, if the two-path sling 50 is subjected to either one of the pre-selected
conditions to a point that causes either ring 26d or ring 26e to fail, the rigger will be alerted
and will have more information than would otherwise be available to him. Designing the
rings 26d, 26e to fail under different situations may also assist the sling manufacturer in
analyzing the sling or further improving the sling, if the sling is ever returned for inspection
or repair. However, there are situations in which it will be necessary to design the rings 26d
and 26e to fail under the same condition (e.g., an overload condition).
The pre-failure warning indicator 11 in accordance with the present invention is
designed with a trigger mechanism that will generate a magnified force on the whip end 40 of
the external warning indicator 29 in order to move the whip end 40 out-of-sight almost
instantaneously, if any of the pre-engineered conditions are met and the ring fails. The reason
why the force on the whip end 40 of the warning indicator fiber 29 is magnified is because of
the double-back design of the warning indicator fiber 29 through the termination eyes 32,34.
After the ring 26 breaks, the termination eyes 32 and 34 separate at a certain speed; however,
since the warning indicator fiber 29 is tied to one eye 32, threaded through the opposite eye
34, and doubles-back along the ring before emerging through the cover 25, the whip end 40 of
the warning indicator is moving twice as fast (and twice the distance) as the speed (and
distance) at which the eyes 32, 34 are moving away from each other. Accordingly, the whip

WO 2006/127489 PCT/US2006/019518
25
end 40 withdraws inside the cover entirely so that there is no question as to whether a trigger
event occurred.
Another feature to note, is that because the whip 40 of the warning indicator 29 is
moving so fast, it creates a sound that is audible to the operator. Therefore, the present
invention not only gives a visual indication that a sling has reached a critical damage point,
but also gives an audible warning. The audible warning is especially important when the
sling is positioned so that the operator cannot see the whip 40 (e.g., when the sling is hanging
thirty feet in the air).
Another notable feature of the subject pre-failure warning indicator 11 is the ability to
warn the rigger of an overload and other dangerous situations without affecting the overall
strength of the roundsling 10. If the rigger stops lifting the load promptly after the pre-failure
warning indicator 11 is triggered, the sling 10 retains 100% of its residual strength.
The color code safety feature of this invention may be achieved by encasing the load-
bearing core in two separate covers, each cover having a different color. For example, the
outer cover could be green or blue, and the inner cover could be orange or red; since the inner
cover is a different color from the outer cover, it will show through whenever the outer cover
is cut or worn through. This double-cover feature provides a visible safety warning for any
user of the sling that abrasion or other damage not normally detectable, has occurred.
In another embodiment of the present invention, a pre-failure warning indicator 11 can
be adapted with a sabotage or tamper-evident means. Referring now to Figure 7, a tamper-
evident tag 35 is attached to either the dedicated indicator strand 20 or, preferably, to one of
the eyes 32 or 34. The free end of the tamper-evident tag 35 is passed through the cover via a
slit. The slit can be the same one through which the whip 40 passes through.

WO 2006/127489 PCT/US2006/019518
26
If the pre-failure warning indicator 11 is triggered (by, for example, an overload
condition), this means that ring 26 has been broken, the ends 22, 24 of the dedicated strand 20
are free, causing whip 40 to withdraw completely within the cover. Upon inspection, the
tamper-evident tag 35 can be easily pulled out from inside the cover 25 along with a portion
of the dedicated strand 20, as illustrated in Figure 8, when the pre-failure warning indicator
11 has been triggered. If the whip end 40 of the warning indicator is not visible because of an
intentional intervention by a user, the tamper-evident tag 35 will remain secure and cannot be
pulled from the cover 25. In this manner, sabotage of the sling 10 can be evidenced by the
supervisor on the work site. (In order to avoid work, some users will cut off the whip end 40
of the warning indicator 29 in an attempt to make it appear that the sling was subjected to a
damage situation and, therefore, work must be temporarily stopped so that the sling can be
removed for inspection and, if necessary, replaced with a new sling.)
As part of the inspection process, the inspector may yank on the tamper-evident tag
35. If the tag is secure, the sling 10 is useable; but, if the tamper-evident tag 35 can be pulled
out from inside the cover, the sling 10 must be removed from use because the pre-failure
warning indicator 11 has been triggered. Of course, if a saboteur cuts both the whip end 40
and the visible portion of the tamper-evident tag 35, the inspector will immediately know that
the sling 10 has been tampered with, and should remove the sling from service.
It is important to note that no other prior warning indicators have the ability to quickly
inspect the condition of a roundsling. Also, prior warning indicators are not as accurate as the
subject warning indicator 11. If the whip end 40 of the warning indicator is visible and the
cover 25 is intact, the roundsling can be used for the next lift; if the whip end 40 of the
warning indicator is not visible, the sling should be removed from service and inspected.

WO 2006/127489 PCT/US2006/019518
27
The subject pre-failure warning indicator is the first completely pass/fail inspection system -
it is a completely objective test and not subjective.
It should also be noted that one skilled in the art, after reading this disclosure, may
develop variations that are contemplated as being equivalent in scope to the various
embodiments specifically set forth in the present disclosure. For example, the termination
loops 32, 34 may be eliminated and the ends of the dedicated strand 20 may be tied directly to
the ring 26. (Alternatively, slip-knots or other means may be used to secure the ends of the
strand 20 to the ring 26.)
Although this invention has been described and illustrated by reference to specific
embodiments, it will be apparent to those skilled in the art that various changes,
modifications and equivalents may be made which clearly fall within the scope of this
invention. The present invention is intended to be protected broadly within the spirit and
scope of the appended claims.
*****

WO 2006/127489 PCT/US2006/019518
28
CLAIMS
I Claim:
1. A roundsling which comprises:
a) a load-bearing core;
b) a pre-failure warning indicator means including:
i) a strand, having a first end terminated by a first eye and a second end
terminated by a second eye, said strand placed proximate the lifting core;
ii) a ring adapted to join said eyes to form an endless loop of the strand,
wherein said ring is designed to fail from one or more predetermined conditions and said
failure occurs before said lifting core is damaged; and
iii) a warning indicator fiber having a secured end and a whip end, the
secured end of said warning indicator being attached to the first eye of the strand, and the
whip end of said warning indicator fiber being directed along the ring, threaded through the
second eye of said strand and double-backed along the ring; and
c) a cover means for covering the lifting core and the pre-failure warning
indicator, said cover having at least one slit from which said whip end of the warning
indicator fiber emerges and extends so that the whip end is visible upon a cursory inspection.
2. The roundsling of claim 1 wherein said ring has a lower tensile strength than
the load-bearing core.

WO 2006/127489 PCT/US2006/019518
29
3. The roundsling of claim 2 wherein said ring fails at a pre-determined force
well before damage can occur to the load-bearing core, said ring failure causing the first eye
and second eye to separate with respect to each other and drawing the whip end of the
warning indicator inside the cover so that it is no longer visible.
4. The roundsling of claim 3 wherein said whip end of the warning indicator
moves so quickly as it withdraws within the cover that it makes an audible indication.
5. The roundsling of claim 2 wherein when the roundsling is subjected to a force
of approximately 70% of its rated maximum load, the ring breaks, causing the whip end to
withdraw completely inside the cover, thereby providing a visual indication to any observer
that the sling has been subjected to a possible overload condition and may have been
damaged.
6. The roundsling of claim 1 wherein said ring is more susceptible to break from
yarn-on-yarn abrasion damage than the load-bearing core.
7. The roundsling of claim 1 wherein said ring is more susceptible to break from
excessive temperatures than the load-bearing core.
8. The roundsling of claim 1 wherein said ring is more susceptible to break from
the deterioration of chemicals than the load-bearing core.

WO 2006/127489 PCT/US2006/019518
30
9. The roundsling of claim 1 wherein said strand of the pre-failure warning
indicator is twisted around the load-bearing core.
10. The roundsling of claim 1 wherein the load-bearing core is formed by twisting
a plurality of yarns together to form a single strand and then wrapping the single strand into
endless parallel loops.
11. The roundsling of claim 10 wherein said load-bearing core comprises one of
the following materials:

a) aramid material strands;
b) K-Spec ® strands (a proprietary blend of high performance fibers);
c) polyester strands;
d) polyethylene strands;
e) HMPE strands; or
f) LCP strands.

12. The roundsling of claim 11 wherein said strand of the pre-failure warning
indicator is made from the same load-bearing material as the load-bearing core.
13. The roundsling of claim 1 comprising a second cover means that encloses said
cover means, said second cover means having a different color than the enclosed cover
means.

WO 2006/127489 PCT/US2006/019518
31
14. The roundsling of claim 1 further comprising a tamper-evident indication
means including a tag having a first end and a second end, the first end of said tag attached to
the strand of the pre-failure warning indicator, the second end of said tag threaded through the
slit in the cover, the tamper-evident indication means designed to remain stationary as long as
the ring's integrity remains intact, and if the sling has been subjected to a pre-determined
condition such that the ring breaks, the tamper-evident indication means can be pulled out
from inside the cover.
15. The roundsling of claim 14 in which said first end of the tag is attached to an
eye of the pre-failure warning indicator.
16. A pre-failure warning indicator for use with an industrial sling, the pre-failure
warning indicator comprising:

a) a strand, having a first end terminated with a first eye loop and a second end
terminated with a second eye loop;
b) a ring adapted to join said eyes to form an endless loop of the strand,
wherein said ring is designed to break from one or more predetermined conditions; and
c) a warning indicator fiber having a secured end and a whip end, wherein said
secured end is attached to the first eye of the strand and said whip end is threaded through the
second eye of the strand.
17. The pre-failure warning indicator of claim 16 wherein said ring is designed to
break at a predetermined tensile strength.

WO 2006/127489 PCT/US2006/019518
32
18. The pre-failure warning indicator of claim 16 wherein said ring is designed to
break when subjected to a predetermined temperature.
19. The pre-failure warning indicator of claim 16 wherein said ring is designed to
break when subjected to a predetermined concentration of specific chemicals.
20. The pre-failure warning indicator of claim 16 wherein said pre-failure warning
indicator is designed to make an audible indication when the indicator is triggered.
21. The pre-failure warning indicator of claim 16 comprising a tamper indication
means including a tag having a first end and a second end, the first end of said tag attached to
the strand of the pre-failure warning indicator, said tag designed to remain stationary as long
as the ring's integrity remains intact, and if the sling has been subjected to a pre-determined
condition such that the ring breaks, the tamper indication means can be pulled out from inside
the cover.
22. The roundsling of claim 21 wherein said first end of the tag is attached to an
eye of the pre-failure warning indicator.

ABSTRACT
Title : SLING WITH PREDICTABLE PRE-FAILURE
WARNING INDICATOR
The pre-failure warning indicator (11) is provided for use with a sling (10). The
pre-failure warning indicator (11) triggers at a point that is predictable within a
relatively narrow range, thereby increasing the possibility that a damaged sling
(10) is removed from use. The pre-failure warning indicator (11) includes a
dedicated strand of material (20) that is placed in close proximity to the load-
bearing core yarns (17) of the sling (10) but remains separate and independent
from the core yarns (17); the ends (22,24) of the dedicated strand are
connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is
visible to operators/riggers work in conjunction with the sacrificial strand (20)
and the ring (26) is designed to fail when the sling (10) is subjected to a
specifically chosen condition (e.g. excessive weight). The failure of the ring (26)
causes the warning fiber (20) to withdraw from the rigger's view thereby
warning he rigger that the sling (10) was subjected to the specifically chosen
condition and may be damaged.

The pre-failure warning indicator (11) is provided for use with a sling (10). The
pre-failure warning indicator (11) triggers at a point that is predictable within a
relatively narrow range, thereby increasing the possibility that a damaged sling
(10) is removed from use. The pre-failure warning indicator (11) includes a
dedicated strand of material (20) that is placed in close proximity to the load-
bearing core yarns (17) of the sling (10) but remains separate and independent
from the core yarns (17); the ends (22,24) of the dedicated strand are
connected via a sacrificial "ring" (26). A warning fiber (29) having an end that is
visible to operators/riggers work in conjunction with the sacrificial strand (20)
and the ring (26) is designed to fail when the sling (10) is subjected to a
specifically chosen condition (e.g. excessive weight). The failure of the ring (26)
causes the warning fiber (20) to withdraw from the rigger's view thereby
warning he rigger that the sling (10) was subjected to the specifically chosen
condition and may be damaged.

Documents:

http://ipindiaonline.gov.in/patentsearch/GrantedSearch/viewdoc.aspx?id=Wt5Q5wCN6u5KSAdqs1ewig==&loc=wDBSZCsAt7zoiVrqcFJsRw==

« Previous Patent

Next Patent »

Patent Number

279855

Indian Patent Application Number

4357/KOLNP/2007

PG Journal Number

05/2017

Publication Date

03-Feb-2017

Grant Date

31-Jan-2017

Date of Filing

14-Nov-2007

Name of Patentee

SLINGMAX, INC.

Applicant Address

2626 MARKET STREET, P.O. BOX 2423 ASTON, PA

Inventors:

#	Inventor's Name	Inventor's Address
1	ST. GERMAIN, DENNIS	358 HIGH RIDGE ROAD CHADDS FORD PA 19317

PCT International Classification Number

B66C 1/12

PCT International Application Number

PCT/US2006/019518

PCT International Filing date

2006-05-19

PCT Conventions:

#	PCT Application Number	Date of Convention	Priority Country
1	60/683,987	2005-05-23	U.S.A.
2	11/418,597	2006-05-05	U.S.A.