The disclosure relates to compressors. More particularly, the disclosure relates to economized compressors.
Positive displacement compressors such as screw compressors are commonly used in applications such as chillers. Many such compressors are economized, having an economizer port intermediate to a suction port and discharge port. In the operation of a chiller compressor, economizer flow is bypassed from the main flow and is used to absorb heat from the main flow prior to returning to the economizer port. This expands the envelope of compressor and system operation.
A notable problem with such compressors is the propagation of pulsation from the economizer port. The opening and closing of compression pockets to the economizer port causes a pulsation which propagates upstream along the economizer flowpath exciting the system and producing annoying sound and unwanted vibration.
To address such sound and vibration, various measures may be taken including adding mufflers along the economizer line and adding sound damping material along the economizer line and/or compressor housing. US Patent Application Publication 2006/0127235A1 of Shoulders, published Jun. 15, 2006, discloses the formation of resonators along the economizer flowpath within the housing of the compressor to produce cancelling pulsation.
One aspect of the disclosure involves a compressor having a male rotor, a female rotor, and a housing. The housing has a first bore and a second bore respectively accommodating portions of the male rotor and the female rotor. The housing has an inlet, an outlet, an economizer port along at least one of the first bore and the second bore, and an external port communicating with the economizer port. The housing has a chamber between the economizer port and the external port having a volume of at least 0.8 liter.
In one or more embodiments of any of the foregoing embodiments, the volume is at least 1.0 liters.
In one or more embodiments of any of the foregoing embodiments, the volume is 1.0 liters to 2.0 liters.
In one or more embodiments of any of the foregoing embodiments, the volume is 1.10 liters to 1.50 liters.
In one or more embodiments of any of the foregoing embodiments, the volume is at least 30% of a displacement per revolution of the male rotor.
In one or more embodiments of any of the foregoing embodiments, the displacement per revolution of the male rotor is 1.0 liter to 5.0 liters.
In one or more embodiments of any of the foregoing embodiments, an area ratio of the economizer port to the external port is at least 0.130 and at most 0.170.
In one or more embodiments of any of the foregoing embodiments, the compressor is a two-rotor compressor.
In one or more embodiments of any of the foregoing embodiments, the compressor further comprises: a motor within the housing directly driving the male rotor.
In one or more embodiments of any of the foregoing embodiments, the economizer port is along the second bore and not the first bore.
In one or more embodiments of any of the foregoing embodiments, the chamber has a protuberant portion.
In one or more embodiments of any of the foregoing embodiments, at a first location the protuberant portion has a minimum cross-sectional area of at least twice an area of the external port.
In one or more embodiments of any of the foregoing embodiments, a cut plane through the protuberant portion parallel to a central axis of the at least one of the first bore and second bore has an area at least three times a cross-sectional area of a passageway leg to the external port and/or at least eight times a cross-sectional area of a passageway leg to the economizer port.
In one or more embodiments of any of the foregoing embodiments, a portion of the chamber has a surface portion opening to the economizer port and generally radially outwardly convex relative to an axis of said at least one of the first bore and second bore.
In one or more embodiments of any of the foregoing embodiments, a method for using the compressor comprises: driving rotation of the male rotor and female rotor to: intake a first flow of fluid through the inlet, compress the first flow and discharge the first flow from the outlet; and intake an additional flow of fluid through the economizer port to merge with the first flow.
In one or more embodiments of any of the foregoing embodiments, the chamber is effective to provide pulsation transmission loss of at least 3 dB rms over a majority of a male rotor speed range of 60 Hz to 105 Hz.
In one or more embodiments of any of the foregoing embodiments, the chamber is effective to provide pulsation transmission loss of at least 5 dB rms over a majority of said speed range.
Another aspect of the disclosure involves a vapor compression system comprising the compressor and further comprising: a first heat exchanger; a second heat exchanger; a flowpath passing from the compressor outlet through the first heat exchanger and then the second heat exchanger and then returning to the compressor inlet; and an economizer flowpath branching from the flowpath and returning to the external port.
In one or more embodiments of any of the foregoing embodiments, the vapor compression system further comprises: an economizer along the economizer flowpath.
In one or more embodiments of any of the foregoing embodiments, the economizer comprises a heat exchanger with a first leg along the flowpath and a second leg along the economizer flowpath and in heat exchange relation with the first leg.
Another aspect of the disclosure involves a compressor comprising: a male rotor and a female rotor; and housing. The housing has: a first bore and a second bore respectively accommodating portions of the male rotor and the female rotor; an inlet; an outlet; an economizer port along at least one of the first bore and the second bore; an external port communicating with the economizer port; and means between the economizer port and the external port for dissipating pulsations propagating from the economizer port.
The details of one or more embodiments are set forth in the accompanying drawings and the description below. Other features, objects, and advantages will be apparent from the description and drawings, and from the claims.
Like reference numbers and designations in the various drawings indicate like elements.
The exemplary system 20 is an economized system having an economizer heat exchanger 36. The exemplary economizer heat exchanger 36 (e.g., a brazed plate heat exchanger) has a first leg 38 along the main refrigerant flowpath. The economizer further includes a second leg 40 in heat exchange relation with the first leg 38 along an economizer flowpath 42 branching off the main flowpath. The economizer flowpath 42 enters the associated economizer line and extends from junction 44 with the main flowpath to an economizer port 46 of the compressor. An alternative economizer configuration is a flash tank economizer.
Each of the rotors 52, 54 has a lobed working portion or section 64, 66 extending from a first end 68, 70 to a second end 72, 74. The rotors include shaft portions 80, 82 protruding from the first ends and 84, 86 protruding from the second ends. The shaft portions may be mounted to bearings 90, 92, 94, and 96. The bearings support the respective rotors for rotation about respective axes 500, 502 (
The respective rotor working portions 64, 66 have lobes 110, 112 enmeshed with each other. The rotor lobes combine with housing bores 114, 116 receiving the respective rotors to form compression pockets. In operation, the compression pockets sequentially open and close at a suction plenum 120 and at a discharge plenum 122. This opening/closing action serves to draw fluid in through the inlet 26, then to the suction plenum, then compress the fluid and discharge it into the discharge plenum, to in turn pass to the outlet. The fluid drawn in through the suction port 26 may pass through/around the motor so as to cool the motor before reaching the suction plenum.
In operation, the motor directly drives the male rotor. The interaction of the male rotor lobes with the female rotor lobes, in turn, drives rotation of the female rotor. Alternative compressors may have other drive arrangements such as reducing gearboxes. For an exemplary air-cooled compressor with R134A refrigerant, exemplary basic full-load compressor volume index is 3.35 or 2.7, more broadly, 1.7 to 4.0 or 2.0 to 4.0 or 2.5 to 3.5. For a variable capacity compressor, one or more unloading and/or volume index (VI) valves may be used to reduce compression below such basic full-load values. The exemplary motor is an induction motor. An exemplary induction motor is a two-pole motor.
The opening of the compression pockets at the internal economizer port 150 produces a pulsation. For example, when a compression pocket just begins to open to the internal economizer port 150 the pressure in the pocket may be less than the pressure in the economizer line. Consequently refrigerant flow rushes into the compression pocket from the economizer line. As the pocket crosses over the internal economizer port, the pressure in the compression pocket rises above the pressure in economizer line causing the gas to rush out of the compression pocket through the internal economizer port 150. This movement of gas in and out of the compression pocket causes pulsation in the economizer passageway 152. The pulsation will propagate back upstream along the economizer branch 42. The pulsation may thus produce annoying sound and may also produce equipment-damaging vibration.
In order to help dissipate the vibration before exiting the compressor,
Table I below shows the exemplary properties of exemplary compressors and exemplary cavities. Compressors are nominally sized via a frame number with increasing number associated with increasing size. The second column of Table I identifies the properties of exemplary size of two-rotor compressors, exemplary size measured as cubic feet per revolution which identifies the volume of intake fluid per revolution of the male rotor. The third column identifies the total cavity volume of the passageway 152. As is discussed below, this may include a dead leg or branch 170 (
The exemplary Frame 1, 2, and 3 cavities are representative of tested examples and are not limiting at to particular geometry. Cavity volume may be sufficiently large so to provide space for pulsation waves to spread out and be broken up by reflection and the like. There may become diminishing marginal returns above a threshold volume which are then overwhelmed by cost issues. An exemplary volume is at least 0.8 liters, or at least 1.0 liter or 1.0 liter to 2.0 liters or 1.10 to 1.50 liters.
As an example of relative size, the volume may be at least 30% of a displacement per revolution of the male rotor. However, testing reflected in the table above shows relative insensitivity of sufficient cavity size to compressor size. Such exemplary sizes include displacements of an exemplary one liter to five liters.
Exemplary compressor speeds are characterized by the rotational speed of the male rotor (e.g., in Hz). Pulsation frequency will reflect a combination of that speed and the lobe count, but there normally is only a slight variation in lobe count with most compressors having between 5 and 8 lobes on their male rotors. With variable speed drive, an exemplary baseline compressor may have an operational range of 45 Hz to 90 Hz. Pulsations generally are not problems in the lower portion of this range (e.g., below 60 Hz).
The protuberant nature of the region 160 may help cause partial wave reflections that dissipate the output pulses at the external port relative to the internal port. In one characterization of the protuberant nature of the volume of the region 160, at a first location the protuberant portion has a minimum cross-sectional area of at least twice an area of the external port or at least 3.0 times. That minimum cross-sectional area is defined by pinning a hypothetical plane at a given point in space (the location) in the region 160. The area of the region 160 cut by the plane will vary depending on plane orientation. The first location may thus be selected to provide the maximum value of that minimum.
In a further example, a cut plane 520 is shown in
Other characterizations, may involve comparing the cross-sectional areas of the branches 304 and 306 (and their associated passageway legs) to the surface areas where they intersect the protuberance 320 and region 160. For the branch 306, this may involve comparison to the concave surface portion 340. The ratio may be an exemplary at least five times or an exemplary at least eight times or substantially more. Similarly, for the branch 304, it merges with a generally flat region 350 (
The pulsation cancellation may expand the compressor operational envelope. For example, with the baseline compressor noted above having an operational range of 45 Hz to 90 Hz, the upper end may be pulsation-limited. The cancellation may expand the usable upper limit to an exemplary 105 Hz or above (e.g., 120 Hz, 130 Hz, 150 Hz or more). Compared to the baseline lacking the enlarged passageway, the revision may be effective to provide pulsation transmission loss of at least 3 dB or at least 5 dB over a majority (or more such as 75%) of a sensitive portion of the male rotor speed range (e.g., a majority of the of 60 Hz to 105 Hz range or substituting lower limits of 70 hz or 80 Hz and any of the upper limits noted above). The pulsations and their reduction may be measured by a dynamic pressure transducer in the economizer line (e.g., close to the economizer port). Resonances or other happenstance my mean that at some locations in that range the revision might not reduce the transmission and might increase it.
The compressor may be made using otherwise conventional or yet-developed materials and techniques.
The use of “first”, “second”, and the like in the description and following claims is for differentiation within the claim only and does not necessarily indicate relative or absolute importance or temporal order. Similarly, the identification in a claim of one element as “first” (or the like) does not preclude such “first” element from identifying an element that is referred to as “second” (or the like) in another claim or in the description.
Where a measure is given in English units followed by a parenthetical containing SI or other units, the parenthetical's units are a conversion and should not imply a degree of precision not found in the English units.
One or more embodiments have been described. Nevertheless, it will be understood that various modifications may be made. For example, when applied to an existing basic system, details of such configuration or its associated use may influence details of particular implementations. Accordingly, other embodiments are within the scope of the following claims.
Benefit is claimed of U.S. Patent Application No. 62/203,858, filed Aug. 11, 2015, and entitled “Screw Compressor Economizer Plenum for Pulsation Reduction”, the disclosure of which is incorporated by reference herein in its entirety as if set forth at length.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2016/046459 | 8/11/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/027657 | 2/16/2017 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3568466 | Brandin et al. | Mar 1971 | A |
3871800 | Slayton | Mar 1975 | A |
4084405 | Schibbye | Apr 1978 | A |
4934482 | Herron et al. | Jun 1990 | A |
5180298 | DiRe | Jan 1993 | A |
5205719 | Childs et al. | Apr 1993 | A |
5224840 | Dreiman et al. | Jul 1993 | A |
5507151 | Ring et al. | Apr 1996 | A |
5616017 | Iizuka et al. | Apr 1997 | A |
6095777 | Nishihata et al. | Aug 2000 | A |
6257846 | Muramatsu et al. | Jul 2001 | B1 |
6360555 | Li et al. | Mar 2002 | B1 |
6902381 | Hur et al. | Jun 2005 | B2 |
7121814 | Rockwell et al. | Oct 2006 | B2 |
7156624 | Shoulders | Jan 2007 | B2 |
7568898 | Shoulders | Aug 2009 | B2 |
7988427 | Patrick | Aug 2011 | B2 |
7993112 | Rockwell | Aug 2011 | B2 |
8016071 | Martinus et al. | Sep 2011 | B1 |
8021126 | Sishtla et al. | Sep 2011 | B2 |
8317489 | Barth | Nov 2012 | B2 |
8496446 | Lai | Jul 2013 | B2 |
8845312 | Takaki | Sep 2014 | B2 |
20020051722 | Okada | May 2002 | A1 |
20030049146 | Dieterich | Mar 2003 | A1 |
20050144976 | Sishtla | Jul 2005 | A1 |
20060127235 | Shoulders | Jun 2006 | A1 |
20060165543 | Fox et al. | Jul 2006 | A1 |
20060239836 | Forster | Oct 2006 | A1 |
20070269325 | Candio et al. | Nov 2007 | A1 |
20080060622 | Prior | Mar 2008 | A1 |
20080219863 | Jung | Sep 2008 | A1 |
20080284161 | Dole et al. | Nov 2008 | A1 |
20100209280 | Flannigan et al. | Aug 2010 | A1 |
20100218536 | Rockwell | Sep 2010 | A1 |
20150004015 | Kienzle et al. | Jan 2015 | A1 |
20160097572 | Feller et al. | Apr 2016 | A1 |
Number | Date | Country |
---|---|---|
2197361 | Oct 1997 | CA |
1212333 | Mar 1999 | CN |
1221088 | Jun 1999 | CN |
2002053975 | Jul 2002 | CN |
1499080 | May 2004 | CN |
1851244 | Oct 2006 | CN |
101072946 | Nov 2007 | CN |
101144475 | Mar 2008 | CN |
201462139 | May 2010 | CN |
102878366 | Jan 2013 | CN |
203404544 | Jan 2014 | CN |
103821713 | May 2014 | CN |
203822630 | Sep 2014 | CN |
104204532 | Dec 2014 | CN |
104411974 | Mar 2015 | CN |
10011023 | Sep 2001 | DE |
202005001600 | Apr 2005 | DE |
202007005097 | Aug 2008 | DE |
102013106344 | Dec 2014 | DE |
0542169 | May 1993 | EP |
0926414 | Jun 1999 | EP |
1339407 | Oct 1963 | FR |
282752 | May 1928 | GB |
54129017 | Sep 1979 | JP |
57129286 | Aug 1982 | JP |
H01237389 | Sep 1989 | JP |
07332267 | Dec 1995 | JP |
08338386 | Dec 1996 | JP |
2003184767 | Jul 2003 | JP |
2435985 | Dec 2011 | RU |
0166946 | Sep 2001 | WO |
02053917 | Jul 2002 | WO |
2008045084 | Apr 2008 | WO |
2011152915 | Dec 2011 | WO |
2015006081 | Jan 2015 | WO |
Entry |
---|
International Search Report and Written Opinion dated Oct. 26, 2016 for PCT Patent Application No. PCT/US2016/046457. |
Anatomy of a Grooved Pipe Joint, Jan. 2010, Victaulic, Easton, Pennsylvania. |
Seal Selection Guide Elastometric Seal Construction, Mar. 2016, Victaulic, Easton, Pennsylvania. |
Aquaforce 30XW150-400 Water-Cooled Liquid Chillers, Installation Instructions, Jul. 2012, Carrier Corporation, Jupiter, Florida. |
International Search Report and Written Opinion dated Oct. 21, 2016, for PCT Patent Application No. PCT/US2016/046516. |
High Flow Compressor Outlet Pipe for Evo X Turbo, Jul. 23, 2014, BC, Canada, retrieved from Internet Mar. 22, 2018 https://www.exoticspeed.com/products/high-flow-compressor-outlet-pipe-for-evo-x-turbo, Exotic Speed. |
Chinese Office Action dated Jan. 2, 2019 for Chinese Patent Application No. 201680047232.X. |
Chinese Office Action dated Apr. 25, 2019 for Chinese Patent Application No. 201680056844.5. |
European Office Action dated Feb. 20, 2019 for European Patent Application No. 16754377.6. |
Russian Office Action dated Dec. 11, 2019 for Russian Patent Application No. 2018100095. |
Fang Danqun, Aerodynamic Noise and Muffler, Aug. 31, 1978, pp. 140-146, Science Press, Beijing, China. |
Chinese Office Action dated Nov. 29, 2018 for Chinese Patent Application No. 201680041008.X. |
International Search Report and Written Opinion dated Oct. 13, 2016 for PCT Patent Application No. PCT/US2016/046459. |
Russian Office action dated Mar. 25, 2020 for Russian Patent Application No. 2018100095. |
Number | Date | Country | |
---|---|---|---|
20180156501 A1 | Jun 2018 | US |
Number | Date | Country | |
---|---|---|---|
62203858 | Aug 2015 | US |