Title of Invention | A GAS COMPRESSION SYSTEM AND A METHOD OF OPERATING A REFRIGERANT COMPRESSOR DRIVEN BY A SINGLE-SHAFT GAS TURBINE |
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Abstract | A driver, of the kind that slows down when the power requirement exceeds the maximum driver power, driving a gas compressor (104; 204; 304) is regulated by recycling, via a pressure relief device (102; 202; 302), compressed gas to the compressor inlet when the discharge pressure reaches a designated pressure thereby increasing the mass flow rate through the compressor. The method has particular application to reducing flare loading in a baseload LNG plant. |
Full Text | The production of liquefied natural gas (LNG) may be achieved by cooling and condensing a feed gas stream against multiple refrigerant streams provided by recirculating refrigerant systems. Cooling of the natural gas feed may be accomplished by various cooling process cycles, such as the well-known cascade cycle in which refrigeration is provided by three different refrigerant loops. One such cascade cycle uses methane, ethylene, and propane cycles in sequence to produce refrigeration at three different temperature levels. Another well-known refrigeration cycle uses a propane pre-cooled, mixed refrigerant (C3MR) cycle in which a multicomponent refrigerant mixture generates refrigeration over a selected temperature range. The mixed refrigerant may contain hydrocarbons such as methane, ethane, propane, and other light hydrocarbons, and also may contain nitrogen. Versions of this refrigeration system are used in many operating LNG plants around the world. These and other types of refrigeration processes for natural gas liquefaction involve the use of refrigerant compressors driven by gas turbines. In recent years, single-shaft gas turbines have been used for this purpose. During a blocked compressor discharge event, the compressed refrigerant typically is discharged to a flare system, which must be sized to handle anticipated relief flows during such an event. There also are other systems in the prior art, some of which are discussed below. The term “baseload LNG plant” as used herein is intended to mean a facility that continuously produces liquefied natural gas via refrigeration from at least one of the many cooling process cycles known in the art. The facility may be a land-based site, a floating production, storage, and offloading (FPSO) facility to recover natural gas from the sea/ocean floor, or a gravity-based system (GBS), a FPSO site that is anchored to the sea floor in a particular location. Persons skilled in the art will understand that the net power available from a gas turbine used to drive a refrigerant compressor in a baseload LNG plant is a function of several variables, including but not limited to ambient temperature (the most power is available at cold temperatures), inlet/outlet duct losses, frictional losses, and compressor fouling over time. US-A-4,799,359 (Nicoll) discloses a cryogenic refrigeration compressor containing an externally adjustable relief valve between the compressor discharge and the suction lines. This allows cryogenic fluid to flow from the compressor discharge to the suction line when the discharge pressure exceeds a set value. US-A-4,566,885 (Haak) discloses a liquefaction process with two closed loop refrigeration cycles. In each loop, the compressors are driven by a gas turbine. At times of low power consumption by the compressors at the first loop, turbine power is diverted to a generator. The generator supplements the power generated by the turbine of the second loop, WO-A-88/06674 discloses a process, applicable to FPSO and stationary platforms, to relieve high pressure gas discharge to the sea floor. Any low and/or medium pressure gas is discharged through a conventional flare. This reduces the necessary diameter and length of the flare extending from the platform. WO-A-97/33131 discloses a liquefied natural gas process characterized by coolant loop compressors being mechanically interconnected and driven by a single-shaft gas turbine. Also disclosed is a bypass valve between the inlet and outlet of each compressor for use during process start-up. US-A-5,408,840 (Talley) discloses a refrigerant recovery process. In the event of refrigeration circuit overpressure, the refrigerant, after passing through the pressure relief valve, is collected in a vessel rather than being vented to the atmosphere. US-A-5,319,945 (Bartlett) discloses a process where, in the event of overpressure, refrigerant is diverted from the refrigeration loop to a holding vessel. The volume of the holding vessel must be large enough to reduce the overpressure before a relief vent set pressure is reached. US-A-3,855,810 (Simon et at.) discloses the insertion of a sufficient buffer volume on the low-pressure side of a refrigeration circuit to accommodate the build-up in pressure when the compressor is cut-off. This eliminates the need to flare refrigerant through pressure relief valves. As described above, most refrigerant compressors used in baseload LNG plants are driven by gas turbines. In many applications, single shaft gas turbines are used wherein the gas turbine .and one or more compressors or compressor stages are mounted on a single shaft. If the compressor discharge is blocked by an unexpected process event, the compressed refrigerant typically is discharged to a piping and flare system, which must be sized to handle anticipated relief flows during such an event. It is desirable to minimize the size of the piping and flare system required to handle such flows. It also may be desirable for economic and environmental reasons to minimize the amount of gas flared during process upsets or compressor discharge blockage events. Embodiments of the present invention address these needs and include an apparatus and method for minimizing relief flows in baseload plants for the production of liquefied natural gas (LNG), relating in particular to an apparatus and method which take advantage of the bogdown characteristics of single-shaft gas turbines used to drive refrigerant compressors in order to minimize flare loading during a blocked compressor discharge event. BRIEF SUMMARY OF THE INVENTION In a first aspect, the present invention provides a gas compression apparatus comprising: a gas compressor having a gas inlet and a gas outlet; a driver driving the gas compressor, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip; a recycle pressure relief device in fluid communication with the gas outlet to receive a stream of a compressed gas and opening when the discharge pressure from the gas outlet reaches a designated pressure and conduit means in fluid communication between the gas inlet and the recycle pressure relief device to supply to the gas inlet compressed gas from the recycle pressure relief device when the discharge pressure reaches the designated pressure, thereby increasing the mass flow rate through the compressor and regulating the driver in another aspect, the present invention provides a method of regulating a driver driving a gas compressor having a gas inlet and a gas outlet, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip, wherein, when the discharge pressure of compressed gas from the gas outlet reaches a designated pressure, at least a portion of the compressed gas is recycled to the gas inlet thereby increasing the mass flow rate through the compressor. In a further aspect, the present invention provides a method of limiting flare loading during a blocked compressor discharge event in a baseload LNG plant comprising a gas compressor having a gas inlet and a gas outlet and a driver driving the gas compressor, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip, wherein, when the discharge pressure of compressed gas from the gas outlet reaches a designated pressure lower than the pressure at which flare-off occurs, at least a portion of the compressed gas is recycled to the gas inlet thereby increasing the mass flow rate through the compressor and slowing the driver. In a first embodiment, the apparatus for regulating a driver driving a gas compressor having a gas inlet and a gas outlet, the driver having a maximum power, includes two elements. The first element is a recycle pressure relief device in fluid communication with the gas outlet, the recycle pressure relief device adapted to receive a stream of a compressed gas having a discharge pressure from the gas outlet. The second element is a conduit in fluid communication with the gas inlet, whereby the gas inlet receives at least a portion of the stream of the compressed gas transmitted to the conduit from the recycle pressure relief device when the discharge pressure reaches a designated pressure. The driver can be a gas turbine and at least a portion of the compressed gas is a refrigerant. Preferably, the driver is a single-shaft gas turbine and the compressor is a refrigerant compressor. Suitably, the recycle pressure relief device is a valve. A second embodiment of the apparatus is similar to the first embodiment but includes a vessel in fluid communication with the conduit and the gas inlet. A third embodiment of the apparatus is similar to the first embodiment but includes at least one additional recycle pressure relief device in fluid communication with the gas outlet, the additional recycle pressure relief device adapted to receive an additional stream of the compressed gas from the gas outlet. The at least a portion of the stream of the compressed gas can be transmitted to the conduit from the recycle pressure relief device when the driver reaches a first designated percentage of the maximum power, and at least a portion of the additional stream of the compressed gas transmitted to the conduit from the additional recycle pressure relief device when the driver reaches a second designated percentage of the maximum power. In a fourth embodiment, an apparatus for regulating at least one driver driving at least one multi-stage gas compressor having a plurality of stages, a gas inlet for each stage, and a gas outlet for each stage, includes two elements. The first element is at least one recycle pressure relief device in fluid communication with each gas outlet, the recycle pressure relief device adapted to receive at least one stream of a compressed gas having a discharge pressure from the gas outlet The second element is at least one conduit in fluid communication with at least one gas inlet, whereby the at least one gas inlet receives at least a portion of the at least one stream of the compressed gas transmitted to the at least one conduit from the recycle relief device when the discharge pressure reaches a designated pressure. In common with the other embodiments, it is preferred that the driver is a single-shaft gas turbine and the compressor is a refrigerant compressor. A fifth embodiment of the apparatus is similar to the fourth embodiment but includes at least one vessel in fluid communication with the at least one conduit and at least one gas inlet. In a sixth embodiment, an apparatus for regulating a single-shaft gas turbine driving a refrigerant compressor having a gas inlet and a gas outlet, the gas inlet optionally being in fluid communication with at least one vessel, includes two elements. The first element is at least one recycle pressure relief valve in fluid communication with the gas outlet of the refrigerant compressor, each recycle pressure relief valve adapted to receive a separate stream of a compressed gas having a discharge pressure from the gas outlet of the refrigerant compressor. The second element is at least one conduit in fluid communication with the gas inlet and optionally with the at least one vessel, whereby the gas inlet, and optionally each vessel, receives at least a portion of the stream of the compressed gas transmitted to the at least one conduit from the recycle pressure relief valve when the discharge pressure reaches a designated pressure. Another aspect of the invention is a baseload LNG plant using an apparatus as in any of the embodiments or variations thereof of the apparatus discussed herein. A first embodiment of a method for regulating a driver driving a gas compressor having a gas inlet and a gas outlet, the driver having a maximum power, includes providing a recycle pressure relief device in fluid communication with the gas outlet, the recycle pressure relief device adapted to receive a stream of a compressed gas having a discharge pressure from the gas outlet. A designated pressure for the discharge pressure is established, a conduit in fluid communication with the gas inlet is provided, and at least a portion of the stream of the compressed gas is transmitted to the conduit from the recycle pressure relief device when the discharge pressure reaches the designated pressure. There are several variations of the first method embodiment. In one variation, the driver is a gas turbine and at least a portion of the compressed gas is a refrigerant. In another variation, the driver is a single-shaft gas turbine and the compressor is a refrigerant compressor. In yet another variation, the recycle pressure relief device is a valve. A second method embodiment is similar to the first method embodiment and further includes providing a vessel in fluid communication with the conduit and the gas inlet and transmitting at least a portion of the at least a portion of the stream of the compressed gas from the conduit to the vessel. A third method embodiment is similar to the first method embodiment and further includes providing at least one additional recycle pressure relief device in fluid communication with the gas outlet, the additional recycle pressure relief device adapted to receive an additional stream of the compressed gas from the gas outlet. At least a portion of the additional stream of the compressed gas is transmitted to the conduit when the discharge pressure reaches the designated pressure. In a variation of the third method embodiment, the at least a portion of the stream of the compressed gas in transmitted to the conduit from the recycle pressure relief device when the driver reaches a first designated percentage of the maximum power, and at least a portion of the another stream of the compressed gas is transmitted to the conduit from the additional recycle pressure relief device when the driver reaches a second designated percentage of the maximum power. A fourth method embodiment for regulating at least one driver driving at least one multi-stage gas compressor having a plurality of stages, a gas inlet for each stage, and a gas outlet for each stage. The method includes providing at least one recycle pressure relief device in fluid communication with each gas outlet, the recycle pressure relief device adapted to receive at least one stream of a compressed gas having a discharge pressure from the gas outlet. A designated pressure is established for the discharge pressure, at least one conduit is provided in fluid communication with at least one gas inlet, and at least a portion of the at least one stream of the compressed gas is transmitted to the at least one conduit from the recycle relief device when the discharge pressure reaches the designated pressure, whereby the at least one gas inlet receives at least part of the at least a portion of the at least one stream of the compressed gas. In common with other method embodiments, it is preferred that the driver is a single-shaft gas turbine and the compressor is a refrigerant compressor. A fifth method embodiment is similar to the fourth method embodiment and includes providing a vessel in fluid communication with the at least one conduit and the gas inlet and transmitting at least a portion of the at least a portion of the stream of the compressed gas from the at least one conduit to the vessel. A sixth method embodiment is a method for regulating a single-shaft gas turbine driving a refrigerant compressor having a gas inlet and a gas outlet, the gas inlet optionally being in fluid communication with at least one vessel. The method includes providing at least one recycle pressure relief valve in fluid communication with the gas outlet of the refrigerant compressor, each recycle pressure relief valve adapted to receive a separate stream of a compressed gas having a discharge pressure from the gas outlet of the refrigerant compressor. A designated pressure is established for the discharge pressure and at least one conduit is provided in fluid communication with the gas inlet and optionally with the at least one vessel. At least a portion of the stream of the compressed gas is transmitted to the conduit from the recycle pressure relief valve when the discharge pressure reaches the designated pressure, whereby the gas inlet, and optionally each vessel, receives at least a portion of the stream of the compressed gas transmitted to the at least one conduit from the recycle pressure relief valve when the discharge pressure reaches the designated pressure. BRIEF DESCRIPTION OF SEVERAL VIEWS OF THE DRAWINGS The following is a description by way of example only and with reference to the accompanying drawings of presently preferred embodiments of the invention. In the drawings: Figure 1 is a schematic flow diagram illustrating one embodiment of the present invention; Figure 2 is a schematic flow diagram illustrating another embodiment of the present invention; Figure 3 is a graph illustrating a simulation result of bogdown of a single-stage gas turbine; and Figure 4 is graph illustrating the discharge pressure from a compressor during a blocked discharge event in a system using the present invention. DETAILED DESCRIPTION OF THE INVENTION Embodiments of the present invention relate to an apparatus and method to purposely cause a refrigerant compressor used in the production of LNG to consume all the available power of a single-shaft gas turbines (SSGT) driving the refrigerant compressor during a blocked discharge event. The goal is to bog down the SSGT and trip it off on a low speed warning before the mechanical design pressure (flare relief setting) is reached. The primary benefit of the invention is reduced capital costs for the LNG plant. For example, the diameter and length of the cryogenic piping used in the flare system of the LNG plant may be reduced, and the height of the flare stack may be shortened. In addition, the amount of gas flared may be reduced, thereby realizing economic and environmental benefits. Single-shaft gas turbines (SSGT) (e.g., GE Frame 7EA) are being used to drive refrigerant compressors in existing baseload LNG plants and are being considered for future plants. A characteristic of the SSGT is that it slows down or bogs down in response to a power imbalance between the available power of the unit and the power required by the process. The bogdown of a SSGT is unique in that it is a positive feedback event. When the machine begins to bog down, the air compressor delivering combustion air to the gas turbine also slows down since it is on the same shaft. Thus, less combustion air is available to the gas turbine, which leads to less delivered power, and the event propagates until the gas turbine trips on low speed. In view of this bogdown characteristic, the recycle relief system of the present invention can eliminate a blocked compressor discharge as the controlling event that traditionally sizes the flare header for a natural gas liquefaction plant. This is often estimated as the maximum refrigerant flow rate in the system or the maximum throughput of the compressor (the stonewall point.) The gas bypass/recycle stream moves the operating point of the compressor to the right, lowering the compression ratio. The suction pressure and mass flow rate can be raised until the compressor is operating near the stonewall point A first embodiment of the invention is illustrated in Figure 1. In each stage, a fixed recycle pressure safety valve (PSV) (102, 202, 302), which may be located at the discharge of the compressor (104, 204, 304) or downstream of the aftercooler (106, 206, 306), pipes compressed gas back to an optional suction drum (108, 208, 308). In Figure 1t a recycle PSV is located downstream of the aftercooler in each stage, and compressed refrigerant is transmitted to the optional suction drum. Each recycle PSV has a lower set point than the relief PSV (110, 210, 310) which is open during a blocked discharge event. Embodiments of the present invention may utilize one or more stages, although it is illustrated in embodiments having three stages in Figures 1 and 2. Also, some of the elements in the embodiments shown in Figures 1 and 2 are optional, including the aftercooler (106, 206, 306), the suction drum (108, 208, 308), the relief PSV (110, 210, 310) in Figure 1 and the second or subsequent recycle pressure relief valves (122, 222, 322) in Figure 2. For example, in one variation wherein there is no suction drum, the recycle PSV (102, 2Q3, 302) pipes material directly back to the inlet of the compressor (104r204r304). During a blocked discharge event, the mass flow rate of refrigerant through the compressor (104, 204, 304) increases, thus consuming more power. When the power required by the refrigeration compressors exceeds the available power of the gas turbine and optional helper motor/steam turbine (not shown), the gas turbine will begin to bog down. The recycle PSV (102, 202,302) in each stage is sized so that the gas turbine bogs down and trips on low speed before the set pressure to the flare system (112, 212, 312) is reached. This eliminates the need to size the flare system in response to a blocked refrigerant compressor event. The recycle PSV in each stage can also serve as back-up to the anti-surge valves (114, 214, 314). There are several ways to arrive at a designated pressure for the discharge pressure at which the recycle PSV (102, 202, 302) opens and compressed gas is transmitted to the gas inlet of the compressor (104, 204, 304). For example, during a blocked discharge event, the recycle PSV may be opened just as the compressor enters surge. At the point of surge, the system will have a certain pressure that is a function of several variables, which will be different in every LNG plant. The key variables are the compressor performance curves, system volume, and safety constraints. Alternatively, the recycle valve may be opened at a pressure that does not correlate with the surge point of the compressor. This may be needed to ensure that the gas turbine trips off on low speed before a selected safety constraint is reached. Such a safety constraint may be, for example, that the maximum pressure attained during the event cannot exceed 92% of the flare relief mechanical design pressure. The selected safety constraint or constraints will differ on a case-by-case basis. For example, in the Example discussed below, there is a safety constraint that the final circuit pressure must be less than 95% of the flare relief pressure, as shown in Figure 4, Existing anti-surge valves may not be suitable for relief recycle applications because the anti-surge valves Bre sized specifically to handle flow rates necessary to keep the compressor away from the surge limit (low flow). Similarly, the anti-surge controllers are often tuned to keep the compressor out of surge, and not necessarily to bog the machine down. In a variation of the first embodiment, each recycle PSV (102, 202, 302) can be replaced with an automatic or manual control valve (CV) sized for the same function as each recycle PSV shown in the first embodiment. Another embodiment of the invention is illustrated in Figure 2. As shown, a series of parallel recycle pressure relief valves (122, 222, 322) (PSV, CV, or a combination thereof) can be used instead of a single valve. This series of valves may be staged to open at set percentages of the maximum available gas turbine power (e.g., design value) and/or at set percentages of the flare relief pressure. For example, the first recycle pressure relief valve may open when the gas turbine reaches 75% of maximum power; the second recycle pressure relief valve may open when the gas turbine reaches 85% of maximum power; and the third recycle pressure relief valve may open when the gas turbine reaches 95% of maximum power. Multiple staged recycle pressure relief valves allow an extra degree of flexibility and safety to ensure that, during a blocked compressor discharge, the gas turbine will indeed bog down and trip off on low speed before the flare relief valve opens. In yet another embodiment of the invention, cooling elements are installed in each recycle line to increase fluid density. This increases the mass flow rate through the compressor, thereby consuming available power more quickly. The present invention also can be beneficial when a LNG plant is running at turndown. If a blocked compressor discharge event occurs at lower production levels, the invention will trigger a less severe relief situation, such as, for example, a shell relief scenario that occurs when the outlet of the main LNG heat exchanger is blocked. The present invention also may be used with a multistage compressor. For a n-stage compressor housed within a single casing (e.g., propane compressor in a C3MR liquefaction cycle), the recycle pressure relief valve downstream of the compressor can pipe discharge gas back to any of the suction drums, individually or in combination. It is preferable to recycle the discharge gas to the first stage suction drum so that the gas must travel through the entire n-stage compressor, thereby consuming more power. The present invention also may reduce the severity of the relief scenario when the cooling water is lost to the propane desuperheater in the C3MR liquefaction cycle. EXAMPLE An embodiment of the invention as operated according to Figure 1 is illustrated for a situation in which anti-surge valve 114 fails to operate. The following process steps occur: (1) At time = 0.0005 hours, a blockage of the discharge of compressor 104 is simulated. (2) At time = 0-0041 hours, compressor 104 is about to enter surge. Recycle PSV 102 opens and compressed gas flows back to suction drum 108. (3) At time = 0.0061 hours, recycling refrigerant material flowing back to the suction drum and increasing the throughput of compressor 104 consumes all the available power of the gas turbine. The gas turbine begins to slow (bog) down- (4) At time = 0.0083 hours, the gas turbine reaches its specified low speed trip warning and the simulation stops. The gas turbine trips on low speed before the flare relief pressure is reached, and thus relief PSV 110 does not open. Figure 3, which is a simulation result of bogdown of a SSGT, shows the power consumed by compressors 104 and 204 during the simulation, the power of the gas turbine, and speed of the gas turbine. As shown in Figure 3, the speed drops off very rapidly when all the available power of the gas turbine has been consumed. The data ends at the point the gas turbine reaches its low speed trip, prompting a shutdown of the gas turbine to begin. In order to achieve this result, the dedicated recycle PSV must be sized properly. Figure 4 shows the discharge pressure of compressor 104 during a blocked discharge event. Without using the present invention, the pressure would have continued to rise at 0.0045 hours toward the relief pressure to flare set at a pressure represented by the dashed line in Figure 4, thereby requiring PSV 110 to be opened. In this scenario, the flare system would have to be sized to handle the total compressor discharge flow. Using the present invention, however, it is possible to force the shutdown of the gas turbine before the relief pressure to flare is reached and PSV 110 is opened. Figure 4 shows the pressure initially rises and then decreases as the recycle PSV 102 is opened, and the pressure does build up again over time. However, as the pressure rebuilds in the circuit, bogdown occurs and the gas turbine reaches its low speed setting without the relief PSV 110 opening to flare system 112. Although illustrated and described herein with reference to certain specific embodiments, the present invention is nevertheless not intended to be limited to the details shown. Rather, various modifications may be made in the details within the scope and range of equivalents of the claims and without departing from the scope and spirit of the invention. CLAIMS 1. A gas compression apparatus comprising: a gas compressor (104; 204; 304) having a gas inlet and a gas outlet and a driver driving the gas compressor, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip, characterized in that the apparatus comprises: a recycle pressure relief device (102; 202; 302; 122; 222; 322) in fluid communication with the gas outlet to receive a stream of a compressed gas and opening when the discharge pressure from the gas outlet reaches a designated pressure and conduit means in fluid communication between the gas inlet and the recycle pressure relief device to supply to the gas inlet compressed gas from the recycle pressure relief device when the discharge pressure reaches the designated pressure, thereby increasing the mass flow rate through the compressor and regulating the driver. 2. An apparatus as claimed in Claim 1, wherein the driver is a gas turbine and the compressor is a refrigerant compressor. 3. An apparatus as claimed in Claim 2, wherein the driver is a single-shaft gas turbine. 4. An apparatus as claimed in any one of the preceding claims, wherein the recycle pressure relief device is a valve. 5. An apparatus as claimed in anyone of the preceding claims, wherein said conduit means comprises a vessel in fluid communication with the gas inlet. 6. An apparatus as claimed in any one of the preceding claims, further comprising at least one additional recycle pressure relief device (122; 222; 322) in fluid communication with the gas outlet to receive an additional stream of the compressed gas and opening when the discharge pressure from the gas outlet reaches a respective designated pressure and wherein the conduit means is in fluid communication between the gas inlet and said additional recycle pressure relief device(s) to supply to the gas inlet compressed gas from the additional recycle pressure relief device(s) when the discharge pressure reaches the respective designated pressure, thereby increasing the mass flow rate through the compressor. 7. An apparatus as claimed in any one of the preceding claims, wherein the recycle pressure relief device(s) open when the driver reaches a respective designated percentage of the maximum power of the driver. 8. An apparatus as claimed in any one of the preceding claims wherein: the compressor is a multi-stage gas compressor having a gas inlet for each stage and a gas outlet for each stage; there is a respective said recycle pressure relief device in fluid communication with each gas outlet; and the conduit means is in fluid communication between at least one of the gas inlets and the respective recycle pressure relief devices, 9. An apparatus as claimed in Claim 8, wherein the conduit means provides fluid communication between each gas inlet and the respective recycle pressure relief device receiving compressed gas from the same stage. 10. An apparatus as claimed in Claim 8, wherein the conduit means provides fluid communication between the gas inlet of an intermediate stage and at least some of the respective recycle pressure relief device receiving compressed gas from the later stage(s). 11. An apparatus as claimed in any one of the preceding claims, further comprising at least one relief pressure safety device in fluid communication with the gas outlet to receive an additional stream of the compressed gas and opening to vent compressed gas when the discharge pressure from the gas outlet reaches a designated pressure above the pressure at which all recycle pressure relief devices receiving compressed gas from said outlet open. 12. An apparatus as claimed in any one of the preceding claims, wherein the conduit means comprises cooling means to increase the fluid density of the recycled compressed gas. 13. A baseload LNG plant comprising an apparatus as claimed in any one of the preceeding claims. 14. A method of regulating a driver driving a gas compressor (104; 204; 304) having a gas inlet and a gas outlet, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip, characterized in that, when the discharge pressure of compressed gas from the gas outlet reaches a designated pressure, at least a portion of the compressed gas is recycled to the gas inlet thereby increasing the mass flow rate through the compressor. 15. A method as claimed in Claim 14, wherein additional portions of the compressed gas are recycled to the gas inlet as the discharge pressure reaches one or more respective higher designated pressures. 16. A method as claimed in Claim 15, wherein said respective designated pressure is determined from a designated percentage of the maximum power of the driver. 17. A method of limiting flare loading during a blocked compressor discharge event in a baseload LNG plant comprising a gas compressor (104; 204; 304) having a gas inlet and a gas outlet and a driver driving the gas compressor, said driver slowing down when the power requirement of the gas compressor exceeds the maximum power of the driver and having a low speed trip, characterized in that, when the discharge pressure of compressed gas from the gas outlet reaches a designated pressure lower than the pressure at which flare-off occurs, at least a portion of the compressed gas is recycled to the gas inlet thereby increasing the mass flow rate through the compressor and slowing the driver. 18. A method as claimed in Claim 17, wherein additional portions of the compressed gas are recycled to the gas inlet as the discharge pressure reaches one or more respective higher designated pressures lower than the pressure at which flare-off occurs. |
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0659-chenp-2006 claims-duplicate.pdf
0659-chenp-2006 description (complete)-duplicate.pdf
659-CHENP-2006 CORRESPONDENCE OTHERS.pdf
659-CHENP-2006 CORRESPONDENCE PO.pdf
659-chenp-2006-correspondence-others.pdf
659-chenp-2006-description(complete).pdf
Patent Number | 229530 | ||||||||||||
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Indian Patent Application Number | 659/CHENP/2006 | ||||||||||||
PG Journal Number | 13/2009 | ||||||||||||
Publication Date | 27-Mar-2009 | ||||||||||||
Grant Date | 18-Feb-2009 | ||||||||||||
Date of Filing | 23-Feb-2006 | ||||||||||||
Name of Patentee | AIR PRODUCTS AND CHEMICALS, INC. | ||||||||||||
Applicant Address | 7201 HAMILKTON BOULEVARD, ALLENTOWN, PA 18195-1501, | ||||||||||||
Inventors:
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PCT International Classification Number | F04D27/02 | ||||||||||||
PCT International Application Number | PCT/IB04/02422 | ||||||||||||
PCT International Filing date | 2004-07-28 | ||||||||||||
PCT Conventions:
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