Title of Invention

"A FAN ASSEMBLY"

Abstract An aero acoustic fan assembly is provided and generally includes a fan wheel, a frame, and first and second air outlet diffusing structures. The fan wheel generally, and typically includes an axial air inlet delimited by an air inlet cone, an annular air outlet, a back plate, and front plate opposite the back plate. The frame within supports the fan wheel for rotation about a central axis thereof. The first air outlet diffusing structure is supported by a portion of the frame, adjacent the back plate of the fan wheel and includes a peripheral region. The second air outlet diffusing structure is similarly supported by a portion of the frame, adjacent the front plate of the fan wheel, and also includes a peripheral region, air exiting the annular air outlet of the fan wheel passing between the peripheral regions of the diffusing structures.
Full Text PLENUM/PLUG FAN ASSEMBLY
This is an international regular application filed under 35
U.S.C. §363 claiming priority under 35 U.S.C. §119(e)(l), of
provisional application Serial No. 60/604,571 having a filing
date of August 26, 2004.
TECHNICAL FIELD
The present invention generally relates to air moving
assemblies, more particularly, to plenum/plug fan assemblies
which boost static pressure/dynamic efficiency, and further
provide noise reduction, both broadband and tone components
thereof.
BACKGROUND OF THE INVENTION
Relatively inexpensive plenum or plug-type fans are well
known in the industrial and commercial fan industry. They are
commonly sold as an unhoused fan unit by the manufacturers
;
although they are mounted in a suitable support structure that
can include a front wall with an air inlet opening formed
therein. These fans are used instead of, or to replace,
centrifugal type fans which are commonly used in the air handling
industry. The wheel of the plenum fan is used to pressurize a
surrounding air plenum or housing in which the fan is installed.
A number of air ducts can be connected to the housing and these
can extend from any direction. In addition to being a reasonably
Inexpensive fan structure, a. plenum or plug fan unit can. save
space by eliminating a, special fan housing, transitions and
diffusers commonly characterizing centrifugal air handling
system. When required, two or more of these fans can be mounted
side-by-side on common or separate support frames.
A common and well known difficulty of plug or plenum fans
is that they can be inefficient in their operation and noisy
compared to other types of fans. Furthermore, such assemblies are
known to require considerably more electrical power for operation
of the one or more fans than more efficient units that produce
the same amount of or more air flow. With respect to the noise;
problem, it is noted that with many known plug type fans, low
frequency noises are generally produced, and there is no
currently available and practical solution to the noise problem.
Traditionally, noise reduction in air moving assemblies has been
achieved at the cost of dynamic performance, via the inclusion,
of dissipative silencers. Such silencers typically comprise
i
acoustically lined fan housings, ducting, etc. In an air handling
system, such structures create a static pressure drop which
results in a lowered static efficiency. Furthermore, dissipative
silencers are ill suited to reduce or eliminate the tone
component of sound, namely, blade pass frequency tone.
U.S. Pat. No. 5,749,702 (Datta et al.) describes, among
other things, a fixed center body for axially directing air flow
to and within a bladed fan wheel having an annular air outlet.
The center body extends through the axial .air intake, and
radially expands rearwardly, terminating at an end at the back
of the fan wheel, close to the rear plate thereof. Both inlet and
outlet structures, including the center body, incorporate sound
attenuating material for broadband noise reduction. Increased fan
wheel efficiency is alleged as attributable to a solid curved
rear end section of the center body, which redirects air flow in
a radial direction towards the annular outlet of the fan wheel.
Furthermore, a wall, spaced from a fixed sidewall or front wall
of a fan support structure so as to be positioned behind the fan
wheel, is further provided. The additional wall is preferably
filled with sound attenuating material, and more preferably
still, has a perforated front surface facing the back plate of
the fan wheel.
U.S. Pat. No. 5,426,268 (Yazici et al.) describes combined
utilization of air duct inlet and outlet silencer apparatuses for
an air handling system. Both apparatuses include interior walls,
arranged between interior and exterior wall's thereof, comprised
of sound attenuating material, with at least portions of the
interior walls constructed of perforated metal sheets. In the
outlet duct apparatus, the main passageway is substantially
straight and increases in transverse cross-section from the inlet
to the outlet. The transverse cross-section changes from circular
at the end of the passageway adjacent the fan to rectangular at
the opposite end.
U.S. Pat. No. 5,066,194 (Amr et al.) describes a fan orifice
structure intended for use in conjunction with an outside
enqlosure, usually containing a heat exchanger and compressor of
an ait conditioner. The orifice is defined by an annular curved
surface that extends downwardly from a top wall of the cover. The
curved surface is generated by rotating a planar and curvilinear
line about a coplanar axis of generation. It is said that the
contour -of the orifice enhances fan efficiency and reduces
radiated noise. The orifice cover is made from plastic materials
by a molding process.
U.S. Pat. No. 4,576,549 (Lanier) is generally directed to
a centrifugal fan having a plurality of vortex generators fixed
onto the outer wall of an annular member leading into an air
inlet of the fan wheel. An inlet cone is shown as a concave
annular form tapered inwardly from the larger diameter air inlet
in the fan wheel plate. Vortex generators are shown as formed
plates having lateral edges contoured to fit the curved annular
wall of the inlet cone. It is believed that such structures, so
arranged, permit merger of skin friction induced air current with
the lower velocity air being discharged from the rotating fan
wheel blades .
As is readily appreciated, it remains advantageous to
provide a fan unit which is simple to build and construct which
employs a bladed fan wheel haying an. axial air intake and an
annular air outlet,- and at least "one outlet diffuser for -
directing airflow from the fan wheel such that static efficiency
is improved, and noise is greatly reduced. It is further
advantageous to enhance the noise reduction capabilities of fan
assemblies for air handling systems, more particularly, both the
broadband and tone aspects thereof.
SUMMARY OF THE INVENTION
Fan silencers have traditionally achieved noise reductiot
at the expense of a static pressure drop resulting in an increase
in power input to the fan, and consequently lowering its static
efficiency. The subject invention achieves noise reduction by
boosting the static pressure and -static efficiency. Principles
of dissipative silencer design have beenx employed for both the
fan wheel inlet and outlet. Outlet or discharge considerations
included principles of aerodynamic vane-less diffuser design.
In a first embodiment, a rear (hub) diffuser element, e.g.,
ring, is utilized adjacent the back plate of the fan wheel. The
subject rear diffuser ring, as well as structures of the further
embodiments, are readily, and preferably, but not necessarily,
adapted for enhanced sound attenuation as xwill later • be
discussed.
In a further embodiment, a specially configured front
(shroud) diffuser element, e.g., ring, is utilized, more
generally, a structure which slows, the air discharge velocity
from the fan wheel/fan unit, is provided. In yet a further
embodiment, an inlet diffuser^is provide to selectively guide air
flow into the fan wheel, preferably,, but hot necessarily, the
inlet diffuser incorporates a blade pass frequency (BPF) tuned
resonator. More specific features and advantages obtained in view
of those features will become apparent with reference to the
drawing figures and DETAILED DESCRIPTION OF THE INVENTIQN.
WO 2006/026295 PCT/US2005/030082
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a. schematic cross-section view taken through the
axial center of the fan unit or assembly of the subject
invention;
FIG. 2 is an perspective end view, shaft side, of the
assembly of FIG. 1, illustrating annular" ai'r outlet related
structures, e.g., air outlet diffusing elements;
FIG. 3 is a perspective sectional side view of the assembly
of FIG. 1, illustrating the relationship between, among .other
things, the back plate and acoustic element of the diffusing
structure;
FIG. 4 is a schematic cross-section view taken through the
axial center of an alternate embodiment of the fan unit or
assembly of the subject invention;
FIG. 5 is an perspective end view of the generally assembly
of FIG. 4, illustrating fan inlet particulars;
FIG. 6 .is a perspective side view of the general assembly
of FIG. 4, illustrating fan outlet particulars;
FIG. 7 is a plot of pressure coefficient/efficiency as a
function of flow coefficient for select fan units, including that
of the subject invention; and, -
FIG. 8 is a plot of sound power as a function of frequency
and rotational speed, more particularly, the base ten 3,og of ,the
quotient thereof, for select fan units, including that of the
subject invention. ' . ,
DETAILED DESCRIPTION OF THE INVENTION
As a preliminary matter, fan assemblies 10 of the subject
invention are generally shown in FIGS. 1 & 4, the assembly of
FIG. 4 including features of the assembly of FIG. 1, e.g., a rear
or hub diffusing structure 12, modified features of the assembly
of FIG. 1, e.g., an alternately configured front or shroud
diffusing structure 14, and supplemental select advantageous
features, e.g., a mid-span diffusing structure 16 and/or an air
inlet diffusing structure 18 optionally having an inlet >tuned
resonator section 20. Features of the assembly of FIG. 1 are
further illustrated in FIGS. 2 & 3, and features of the assembly
of FIG. 4 are selectively illustrated in FIGS. 5 & 6. Finally,
aero-acoustic performance of the assembly of the subject
invention in relation to conventional known fan wheel/fan
assemblies is presented in FIGS. 7 & 8 vis-a-vis comparative
representations of both static efficiency and specific sound
power. ,
With reference now to FIGS. 1 & 4, preferred and optional
assemblies of the subject invention, shown or otherwise,
generally include a fan wheel 22 and a frame or base 24 within
which or on which the fan wheel 22 is supported for rotation,
more particularly, rotation about a central axis 26 thereof, such
arrangements being conventional and well known to plenum/plug fan
artisans. The fan wheel 22 generally has an axial air inlet 28,
delimited by an air inlet cone 30 forwardly supported by the
frame 24, an annular air outlet 32, a back 'plate 34, a front
WO 2006/026295 PCT/US2005/030082
plate 36 spaced apart or opposite the back plate 34, and several
blades 38 disposed between the plates 34, 36.
The assembly 10 further includes rear or hub diffusing
structure 12, i.e., a first air outlet diffusing structure or
element, (e.g., a ring, or fractions thereof, i.e., ' halves,
thirds, quarters, etc. as will later be described), depending .or
otherwise supported by the frame 24, or a portion thereof,
adjacent the back plate 34 of the fan wheel 32,x and front or
shroud diffusing structure 14, i.e., a second air outlet
diffusing element (e.g., a ring, or fractions thereof, i.e.,
halves, thirds, quarters, etc. as will later be described),
depending or otherwise supported by the frame 24, or portion
thereof, adjacent the front plate 36 of the fan wheel 32. As
will later be detailed, each of the first and second air outlet
diffusing structures include a peripheral region or segment 40,
air exiting the annular air outlet 32 of the fan wheel 32 passing
between the peripheral regions 40 of the diffusing elements 12,
14.
With particular reference to FIG. 4, the assembly of FIG.
1, or variants thereof, advantageously, but not necessarily, may
furthet, selectively include mid-span diffusing structure 16, air
inlet diffusing structure or assembly. 18, or both in combination
as illustrated. The mid-span diffusing structure 16, i.e., a
third air outlet diffusing element (e.g., a ring, or fractions
thereof, i.e., halves, thirds, quarters, etc. as.will later be
described), depends or is otherwise supported by the frame 24,
or portion thereof, intermediate the first 12 and second 14
diffusing structures. The assembly of the subject invention
advantageously includes such mid-span element when the fan wheel
diameter D exceeds about twenty inches.
The air inlet diffusing assembly 18 (FIGS. 4 & 5),
optionally equipped with inlet tuned resonator 20 (FIG. 4),
depends or is otherwise supported by the frame 24 so as to extend
i
from a forward portion thereof, more particularly and preferably,
to extend therefrom in a spaced apart relationship with the air
inlet cone 30, so as to define or delimit a circumferential air
ingress passage 42 for the assembly generally.
Prior to a further or more developed discussion of the air
outlet diffusing structures, it is to be appreciated that in
addition to prospective air handling applications, select
structures of the assembly described herein (e.g., one or more
of the air outlet diffusing elements, and or variants of the air
inlet diffusing structure) may advantageously be supplied as a
"kit" for after-market conversion of in-place, operational air
handling assemblies. In furtherance of retrofitting such systems,
select structures, e.g., first, second, and/or third air outlet
diffusing elements may be fractionally supplied, preferably, but
not necessarily, in halves (see e.g., FIG. 2 .with regard to hub
12 and shroud 14 structures, and 'FIG. 3 with regard to hub
structure portions 12a, 12b) for incorporation into the preexisting
assembly as the specific application warrants. It is tc
be further appreciated, and understood, that variations ir
fabrication methodology, and modifications of one or more
elements, structures, assemblies, or sub-assemblies of or
relating to the disclosed invention necessitated thereby, is
contemplated.
Referring now generally to FIGS. 1-3, or FIGS. 4-6, the hub
12 and shroud 14 diffusing structures include peripheral regions
or segments 40, as previously noted, more particularly,
peripheral regions 40 adjacent or proximal outer free edges 44,
i.e., outer circumferential edges, of each of the structures. The
peripheral regions 40, which are radially adjacent
circumferential edges 46, 48 of the back 34 and front 36 plates
respectively (see e.g., FIGS. 1, 3 & 4), are advantageously
/
adapted so as to include (i.e., house, contain, etc.) an acoustic
insulation 50. For example, the peripheral regions 40 of each of
the structures 12, 14 may include compartment defining -walls,
e.g., opposing radially spaced apart side walls 52 extending from
a portion of a base 54 of each of the diffusing structures 12,
14 united by a perforated plate 56, within which the sound
attenuating material 50 resides. Sheets, i.e., diffusing
structure surfaces, exposed to air flow (i.e., in direct contact
therewith) are perforated, more generally adapted to "admit"
noise into the insulating material for "capture" therein.
Fabrication of the inlet and outlet diffuser elements in this way
enhances broadband sound attenuation. Omission of the
perforations 'from the air exposed surfaces nonetheless provides
a boost in static pressure/efficiency.
Advantageously, as shown in FIG. 4, the-shroud diffusing
structure 14 may be further adapted to include insulation beyond
a boundary of its peripheral region 40, more particularly,
adapted to retain insulation throughout the entirety of its
radial extent (i.e., adapted to include insulation in a region
or segment 58 radially extending toward an inner circumferential
periphery 60 thereof). Similarly, as shown in FIGS. 4 & 5, both
I
the mid-span diffusing structure 16 and air inlet diffusing
structure 18 preferably include sound insulative material 50.
With regard to the sound insulating material 50, the density
thereof is preferably within the range,of about 0.5 to 8.0 pounds
per cubic foot, with the preferred material thickness within the
range of about 0.05 to 0.1 times the diameter (D) of a the fan
wheel, i.e., ID = fan wheel outside diameter (OD). One suitably
known combination of thickness/density, wherein ID = 18.25
inches, is 1.5 inch thick insulation having a density of about
6.3 pounds per cubic foot, such material being commercially
available and well known.
In connection .to the air contacting surfaces of the
insulated portions of the one or more air" outlet diffusing
' I
elements, and/or air inlet diffusing structure, as has been
heretofore described, perforated surfaces are 'especially
advantageous. Although a variety of perforated surface
configuration have, or are likely to have utility, those
characterized by a transparency index (TI), defined by Theodore
J. Schultz, "Acoustic Uses for Perforated Metals," within a range
of about 1,000 to 20,000 are desirable. The perforated steel
plate used for the diffuser prototype is 20 GA cold rolled steel,
with 0.060 diameter holes spaced on 3/32 inch staggered centers.
The material has approximately one hundred "twenty six holes per
square inch, and a TI value of 13,887.
With reference again to FIGS. 1/4, the hub diffusing
structure 12 is generally configured within the assembly of the
subject invention, in all its contemplated embodiments, to 'be
orthogonally disposed with respect to axial centerline 26 of the
fan wheel 32, i.e., substantially parallel to the back plate 34,
and spaced apart therefrom. Preferably configured as an annular
element, the structure has an interior circumferential edge 62
opposite its outer circumferential edge 44, or the sidewall 52
associated therewith, and an intermediate circumferential edge
64 therebetween, namely, that associated with the interior
sidewall 52a of the insulation retaining compartment 51.
Dimensionally, the diffuser outside diameter (D0) , i.e.,
maximum dimension from opposing sites on the outer
circumferential edge 44, is within the range of about 1.3-1.6D,
and typically substantially equivalent to the frame size; the
diffuser inside diameter (DJ , i.e., maximum dimension from
opposing sites on the interior circumferential edge 62, being
within the range of about 0.6-0.7D; and, the diameter associated
with the commencement of the peripheral region 40 (Dpr) , i.e.,
maximum dimension from opposing sites on the intermediate
circumferential edge 64 or interior sidewall 52a of the
insulation retaining compartment 51, is within the range of about
1.01-1.02D. With such configuration, the perforated surface 56
of the peripheral region 40 of the hub diffusing structure 12
radial extends from the back plate 34, with clearance as noted
(i.e., (Dpr-Dbp {~lD})/2), so as to be substantially coplanar
therewith, and in all cases, delimits a "rear" boundary or guide
for air exiting from the annular air outlet 32.
With continued reference to FIGS. 1/4, the shroud diffusing
structure 14, like the hub diffusing structure 12, is preferably
configured as an annular element, the structure having interior
circumferential edge 60 opposite its outer circumferential edge
44 or the sidewall 52a associated therewith, and an intermediate
circumferential edge 66 therebetween, namely, that associated
with the interior sidewall 52a of the insulation retaining
compartment 51 coextensive with the peripheral region 40 as
previously discussed. Although dimensionally similar to/with the
hub diffusing structure, at least with respect to the
configuration of FIG. 1, i.e., the ranges of D0, Dif and Dpr for
the shroud diffusing structure 14 being substantially equivalent
to the ranges previously described for D0, Di, and Dpr for the hub
diffusing structure,12.,
Advantageously, as shown in FIGS. 1 & 4, interior 60,
exterior 44 and intermediate 66 circumferential edges of the
shroud diffusing structure 14 are not co-planar (i.e., the
structure may suitably be a ring of frusto-conical arrangement),
however, the edges may be, so as to thereby essentially resemble
the configuration for the hub diffusing structure 12. With the
contemplated configurations, several alternative spacings between
free edges 44 of peripheral regions 40 of the diffusing elements
12, 14, i.e., the "width" of passage 42 for air exiting the
annular outlet 32 of the fan wheel 22 (Wp) , result: (1) Wp is
less than a spacing between a free edges 46, 48 of the back 34
and front 36 plates (WJ , as show in FIGS. 1 & 4 (i.e.,- Wp more particularly, as a function of fan wheel diameter D, Ww is
advantageously within the range of about 0.3 to 0.4D (0.356D),
with Wp being a function of Ww and 6; (2) Wp ~/=Ww; and, (3) Wp >
Ww. Alternately, it is believed advantageous to have an angle of
inclination 6 between a plane normal to the axial centerline 26
of the fan wheel 32, and passing through (i.e., including) the
intermediate circumferential edge 66 (or front plate 36 of the
fan wheel 32) , and a plane coextensive with the perforated
surface 56 of the peripheral region 40 thereof, within the range
of About -5 to 25° (10° indicated in FIGS. 1 & 4).
The shroud diffusing structure 14 is generally segmented,
a shroud segment 68 depending from the peripheral region thereo'f,
more particularly, extending radially inward therefrom. With
regard to the segmentation of the shroud diffusing structure of
FIG. 1, the segment or region 68 adjacent the peripheral region
40 thereof extends So as to be planar therewith, i.e., at an
angle a of 180°. The hub diffusing structure 12 is likewise
characterized by such arrangement. With reference to FIG. 4, the
interior segment 68 of the shroud structure 14 is shown
advantageously extending from the peripheral region 40 at an
angle or shroud diffusing structure is advantageously .adapted to include,
i.e., carry, retain, etc., acoustic insulation 50. Finally, it
is further advantageous that the spacing between the interior
circumferential edge 60 of the shroud diffusing structure 14 and
the air inlet cone 30, DG, be within the range of about 0.01 to
0.025D. Functionally, the shroud segment 68 depending from the
peripheral region 40 thereof acts as a front re-circulation
cutoff, essentially preventing short circuiting of discharge air
i
to the inlet of the fan wheel.
With particular reference to FIGS. 4. & 5, the air inlet
diffusing structure 18, preferably configured as a conical
frustuitr, generally includes a sidewall 70 which delimits first
and second circumferential ends or edges, more particularly, an
inlet cone proximal circumferential edge 72, hereinafter
"proximal" circumferential edge, and an inlet cone distal
proximal edge 74, hereinafter, "distal" circumferential edge. As
is readily appreciated with reference to FIGS. 4 & 5, the
diameter of the proximal end is less than that of the distal end.
With the proximal end being a clpsed end, an annular air inlet
path 76 is provided for the fan wheel 32 of the assembly 10, more'
particularly, the inlet cone 30 associated therewith.
As noted in connection to the one or more outlet diffusing
structures, the air inlet diffusing structure 18 is^ likewise
adapted so as to include/incorporated insulative material- 50;
As shown in FIG. 5, the air inlet diffusing structure 18 includes
opposingly paired, spaced apart sidewalls 70, 70a, i.e., inner
and .outer sidewalls, filled or finable with insulation. The
outer sidewall, i.e., the - air engaging sidewall, or sidewall
surface, preferably comprises a perforated sheet.
The resonator assembly of FIG. 4, more particularly, a blade
pass frequency tuned resonator 20, centrally extends from the
tapered, closed end of the inlet diffuser structure 18, i.e., the
proximal end. As to the interrelat'edness of the subject
structure in relation to other elements of the assembly, the
diffuser outside diameter (D0>), i.e., maximum dimension from
opposing sites on the outer or distal circumferential edge 74,
is within the range of about 1.3-1.6D, and typically
substantially equivalent to the-frame size; the diffuser inside
diameter (D.^), i.e., maximum dimension from opposing sites on
the interior or proximal circumferential edge 72, being within
the range of about 0.6 to 0.7D (0.55D); the distance between the
mouth of the inlet cone and the proximal end of the structure
(DPE) is within the range of about 0.2 to 0.3D (0.25D); and, the
extended distance of the inlet tuned resonator 20 from the
proximal end of the inlet diffusing structure 18 (DED) is 'within
the range of about 0/55 to 0.65D (0.60D).
With reference now to FIGS. 7 & 8, performance of the
'assembly of- the subject invention is evidenced, more
particularly,.both static efficiency and specific sound,power is
indicated therefore, in relation to conventional fan wheel/fan
ssemblies for air handling systems. Five (5) test units,
indicated in the legend of FIG. 4 as units I-V, were subject to
testing, with the results indicated. As shown, the diffusers of
the subject fan assembly (II), boost the static efficiency (SE)
of the plenum fan by up to 5%. The vane less diffuser outlet
silencer also improves the pressure generating capability of. the
fan. As indicated in the legend, test unit I omits the structures
of the subj.ect invention, namely those of test unit II, with test
units III-IV being commercially available fan units.
Noise reduction using both the outlet and inlet diffuser
elements is indicated in FIG. 5. Six (6) test units, indicated
in the legend of FIG. 5 as units I-VI, were subject to testing,
with the results indicated. Test-units I-IV, as indicated, are
commercially available fan units, with units V and VI indicated
embodiments of the subject invention. As noted, blade pass
frequency (BPF) tone is. reduced by 3 dB, with as much as 8 dB
reduction being achieved at the higher frequencies.
With reference now to Table T, inlet and outlet diffuser
performance is indicated for an 18.25" OD bare fan wheel, no
bearing support on inlet, having 9 blades (i.e., 182 EPFN), with
and without the diffuser elements of the subject invention. The
outlet sound power level (dB), indicated by Lw, is for the
following frequencies (i.e., 1-8), respectively: 63hz, 125, 250,
500, 1000, 2000, 4000, and 8000. Furthermore, LwA indicates an
inlet A weighting. As can be seen, static efficiency improves
dramatically for higher pressures where the vane less diffuser
works best and, sound quality improves by various levels across
all bands consistently, and may be further improved with
selective perforation of the air contacting wall surface of the
diffuser element, and further still, via utilization of a
resonator to tune out BPF tone.
There are other variations of the subject invention, some
of which will become obvious to those skilled in the art. It will
be understood that this disclosure, in many respects, is only
illustrative. Changes may be made in details, particularly•in
matters of shape, size, material, and arrangement of parts, as
the case may be, without exceeding the scope of the invention.



What is claimed is:
1. A fan assembly comprising:
a. a fan wheel having an axial air inlet delimited by an
air inlet cone, an annular air outlet, a back plate, and
front plate opposite said back plate;
b. a frame within which said fan wheel is supported for
rotation about a central axis thereof;
c. first air outlet diffusing structure supported by a
portion of said frame adjacent said back plate of said fan
wheel, said first air outlet diffusing structure comprising
a peripheral region; and,
d. a second air outlet diffusing structure supported by a
portion of said frame adjacent said front plate of said fan
wheel, said second air outlet diffusing structure
comprising a peripheral region, air exiting said annular
air outlet of said fan wheel passing between said
'peripheral regions of said diffusing structures.
2. The fan assembly of claim 1 wherein a spacing between free
edges of peripheral regions of said diffusing structures is less ,
than a spacing between a free edge of said back plate and a free
edge of said front plate.
3. The fan assembly of claim 1 wherein a. spacing between free
edges of peripheral regions of said diffusing structures is
substantially equal to a spacing between a free edge of said
back plate and a free edge of said front plate.
4. The fan assembly of claim 1 wherein a spacing between free
edges of peripheral regions of said diffusing structures is
greater than a spacing between a free edge of said back plate and
a free edge of said front plate.
5. The fan assembly of claim 2 wherein said peripheral region of
said first air outlet diffusing structure includes sound
insulation.
6. The fan assembly of claim 5 wherein a portion of said sound
insulation is covered by a perforated plate.
7. The fan assembly of claim 5 wherein said peripheral region of•
said second air outlet diffusing structure includes sound
insulation.
8. The fan assembly of claim 7 wherein a portion of said sound
insulation is covered by a perforated plate.
9. The fan .assembly of claim 1 further comprising a third air
outlet diffusing structure supported by a portion of said frame
intermediate said .first and second air outlet diffusing
structures.
10. The fan assembly of claim 9 wherein a spacing between free
edges of peripheral regions of said diffusing structures is less
than a spacing between a free edge of said back plate and a free
edge of said front plate.
11. The fan assembly of claim 9 wherein a spacing between free
edges of peripheral regions of said diffusing structures is
substantially equal to a spacing between a free edge of said
back plate and-a free edge' of said front plate.
12. The fan assembly of claim 9 wherein a spacing between free
edges of. peripheral regions of said diffusing structures is
greater than a spacing between a free edge of said back plate and
a free edge of said front plate.
13. The fan assembly of claim 9 wherein said peripheral region
of said first air outlet diffusing structure includes sound
insulation.
14. The fan assembly of claim 13 wherein said peripheral region
of said second air, outlet diffusing structure includes sound
insulation.
15. The fan assembly of.claim 14 wherein said a third air outlet
diffusing structure includes sound insulation.
16. The fan assembly of claim 9 further, comprising an air inlet
diffusing assembly supported by a portion of said frame adjacent
said axial air inlet of said fan wheel.
17. The fan assembly of claim 16 wherein said air inlet diffusing
assembly comprises a dissapative silencer.
18. The fan assembly of claim "16 wherein said air inlet diffusing
assembly further comprises a tuned resonator .section extending
from said dissapative silencer.
19. The fan assembly of claim 1 further comprising an air inlet
diffusing assembly .supported by a portion of said frame adjacent
said axial air inlet of said fan wheel.
20. The fan assembly of claim 19 wherein said air inlet diffusing
inlet defines an annular air inlet proximal said air inlet cone.
21. The fan assembly of claim 20 wherein said air inlet diffusing
assembly comprises- a dissapative silencer.
22. The fan assembly of claim 21 wherein said air inlet diffusing
assembly further comprises a tuned resonator section extending
from said dissapative silencer. . • : .
23. The fan assembly of claim 19 wherein a spacing between -free
edges of peripheral regions of said diffusing structures is less
than a spacing between a free edge of said back plate and a free
edge of said front plate.
24. The fan assembly of claim 19 wherein a spacing between free
edges of peripheral regions of said diffusing structures is
substantially equal to a spacing between a free edge of said
back plate ,and a free edge of said front plate.
,25. The fan assembly of claim 19 wherein a spacing between free
edges of peripheral regions of said diffusing structures is
greater than a spacing between a free edge of said back plate and
a free edge of said front plate.
26. An aero acoustic diffuser assembly for a plenum/plug fan/
said assembly comprising a first outlet diffusing structure
having at' least two portions for supported by a frame for the fan
adjacent a back plate thereof, a second outlet diffusing
structure having at least two portions supported by the frame for
the fan adjacent the front plate thereof,, said first and said
outlet diffusing structures configured so as to extend beyond
free edges of the front and back plates of the fan so as to
delimit an air discharge passage adjacent an annular air outlet
for the fan.
27. The aero acoustic diffuser assembly of claim 26 wherein a.
cross-section of said air discharge passage is greater than a
cross-section of the annular air outlet for the fan.
28. The aero acoustic diffuser assembly of claim 26 wherein a
cross-section of said air discharge passage is about equal to a
cross-section of the annular air outlet for the fan.
29. The aero acoustic diffuser assembly of claim 26 wherein a
cross-section of said air discharge passage is less than a crosssection
of the annular air outlet for the fan.
30. The aero acoustic diffuser assembly of claim 29 further"
comprising an air inlet diffuser assembly supportable in a spaced
apart, condition adjacent the air inlet cone of the fan.

Documents:

http://ipindiaonline.gov.in/patentsearch/GrantedSearch/viewdoc.aspx?id=5yZASVd8FEY9xZ1I+OKI2g==&loc=+mN2fYxnTC4l0fUd8W4CAA==


Patent Number 272585
Indian Patent Application Number 1868/DELNP/2007
PG Journal Number 16/2016
Publication Date 15-Apr-2016
Grant Date 11-Apr-2016
Date of Filing 09-Mar-2007
Name of Patentee TWIN CITY FAN COMPANIES, LTD.
Applicant Address 5959 TRENTON LANE, MINNEOPOLIS, MINNESOTA 55442 USA
Inventors:
# Inventor's Name Inventor's Address
1 GANESH RADHA KRISHNA 23516 BIRCH CIRCLE, ROGERS, MINNESOTA 55374 USA
2 WILLIAMSON RICHARD DAVID 1134 CHELSEA COURT, NEW BRIGHTON, MINNESOTA 55112 USA
3 WEEKS JONATHAN CHARLES 16411 TEMPLE DRIVE NORTH, MINNETONKA, MINNESOTA 55345 USA
4 SOLOMAKHOVA TATYANA STEPANOVNA 113556 TCHERNOMORSKIY, BULVAR, B.4,AP.186, MOSCOW RUSSIA
PCT International Classification Number H02K 23/60
PCT International Application Number PCT/US2005/030082
PCT International Filing date 2005-08-24
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 60/604,571 2004-08-26 U.S.A.