US3041848A - Variable head compressor - Google Patents
Variable head compressor Download PDFInfo
- Publication number
- US3041848A US3041848A US817187A US81718759A US3041848A US 3041848 A US3041848 A US 3041848A US 817187 A US817187 A US 817187A US 81718759 A US81718759 A US 81718759A US 3041848 A US3041848 A US 3041848A
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- compressor
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- inlet
- swirl
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B1/00—Compression machines, plants or systems with non-reversible cycle
- F25B1/04—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type
- F25B1/053—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type of turbine type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0238—Details or means for fluid reinjection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0246—Surge control by varying geometry within the pumps, e.g. by adjusting vanes
Definitions
- This invention relates to a centrifugal compressor in which the head or change in pressure through the compressor may be regulated in accordance with load requirements without changing the speed of rotation of the compressor and has for its object the provision of simple and effective means for imparting a pre-swirl to the elastic fluid or gas at the compressor inlet to vary the pressure change through the compressor.
- While the fluid fed tangentially of the inlet to create the pre-swirl may be secured from any source, it is conveniently by-passed from the discharge side of the compressor and in a refrigeration system, for example, may be withdrawn from the receiver above the liquid level therein.
- Another advantageous efl'ect of the pre-swirl imparted to the inlet fluid according to this invention is a lessening of the tendency of the compressor to surge or hammer because of light loads and low flow, Where such surging or hunting would otherwise manifest itself in a backflow of fluid into the impeller which adversely affects the chiciency of operation of the unit.
- an object of the invention to provide an improved and simplified means for imparting a preswirl to fluid drawn into the impeller of a centrifugal compressor by feeding fluid into the inlet of the compressor in a direction to produce a rotation of pre-swirl of the inlet fluid.
- Another object of the invention is the provision of means for varying the pressure change through a centrif ugal compressor in accordance with the preceding object, in which the auxiliary fluid producing the pre-swirl is by-passed from the system at the discharge side of the compressor.
- a further object of the invention is to provide direction controlling means for the auxiliary fluid, useable in accordance with the preceding objects, which is readily reversible to eflect pre-swirl in either the same or opposite direction of rotation as that of the compressor impeller, so as to decrease or increase the head or pressure change through the compressor as desired.
- FIG. 1 is a schematic representation of the system employing a variable head compressor according to the present invention, and more particularly representing a closed cycle refrigeration system;
- FIG. 2 is a vertical, sectional view through a variable head compressor according to the invention
- FIG. 3 is a transverse sectional view through the compressor inlet, showing the feeding nozzles for the preswirl producing fluid
- FIG. 4 is a view similar to FIG. 3 but showing the nozzle ring reversed to produce a pre-swirl rotating contrary to the direction of impeller rotation.
- FIG. 1 In the schematic representation of FIG. 1 there is shown a typical refrigeration system including a centrifugal compressor 1 having an inlet 2 and impeller 3, and an outlet scroll 4. From the outlet scroll 4 the compressed refrigerant fluid, which may by way of example only be Freon gas, is fed through a duct 5 to a condenser 6 where it is liquefied to be received within a receiver 7. Liquid from receiver 7 passes through an expansion means 8, which may be an expansion valve, a restrictive tube, an orifice or other means well known in the art for I producing a pressure drop, to an evaporator 9, where it performs its cooling function with the gas exhausting through a duct 11 to the inlet 2 of the compressor.
- an expansion means 8 which may be an expansion valve, a restrictive tube, an orifice or other means well known in the art for I producing a pressure drop
- by-pass fluid is drawn from the system, for example from above the liquid level in the receiver 7, through a duct 12, having therein a head control valve 13, to an annular chamber 14 disposed about the compressor inlet and supplying a plurality of tangential nozzles 15.
- compressor housing 15, defining in its upper portion the inlet 2 has disposed therein a ring 17 defining an annular chamber 18 disposed between the ring 17 and the housing 16 and communicating with the duct 12.
- a plurality of slots 19 spaced around and through the ring and directed substantially tangential to the inner wall of the ring or at least in a direction having a substantial component tangential to the ring wall.
- the fluid passing from chamber 18 through the nozzles 19 is directed so as to produce a pre-swirl or rotation of the fluid in the compressor inlet in the same direction as the rotation of the compressor impeller so that, as previously described, there will be eifected a lessening of the head or pressure change through the compressor.
- FIG. 2 Above the ring 17 in FIG. 2, there is shown a second ring 21 defining a second annular chamber 22 communicating with a passage 23 in the housing 16, this structure being designed to feed by-passed cooling fluid back to the compressor inlet and forming no part of this invention, although the ring 21 in conjunction with inlet conduit 24 serves to maintain the nozzle ring 17 in assembled position.
- the compressor of FIG. 2 is shown as a two-stage compressor, With the discharge from impeller 3 passing through passageway 25 to a second impeller 26 and thence to the outlet scroll 4.
- the impellers 3 and 26 are driven by a suitable motor 27 through a shaft 28.
- FIG. 4 illustrates the mode of operation with the nozzle ring 17 reversed top-for-bottom from the position of FIG. 2, so that the nozzles are now directing the preswirl imparting fluid in a direction opposite to the direction of rotation of the compressor impeller, whereby the operation is such that the pre-swirl or rotation of the inlet fluid increases the head or pressure change through the compressor.
- the head control valve 13 which regulates the flow of the by-passed gas into the pre-swirl producing chamher, is placed in communication with the compressor output, as by communicating means 30, for response to pressure, temperature or other condition in response to variation of which it is desired to vary the head or pressure change through the compressor, this usually being a condition varying in accordance with the load on the compressor so that the head will be varied in accordance with the requirements of the system.
- Such valves and their operation are well known in the art, such a valve being shown, for example, in the patent to Wood, No. 2,734,443. Suitable controls therefor are found in the patent to Wood, No. 2,479,991 which shows a pressure responsive valve control, and to Jensen, No. 2,780,413 which shows a temperature responsive valve control.
- the nozzles 19 have been shown as fixed in their directions through the ring 17, but it will be obvious that adjustable nozzles of known form may be used to vary the direction of fluid flow therethrough to vary the tangential component of fluid movement and thereby control the degree of rotation imparted to the incoming fluid by a given amount of by-pass fluid.
- FIG. 1 While the invention has been specifically shown in FIG. 1 as applying to a refrigeration system, it is obvious that the pre-swirl producing arrangement of this invention may be utilized as Well in any desired system and may be used where the compressor 1 is acting on other gases, for example air.
- variable head compressor comprising a housing having an inlet and an outlet, a centrifugal impeller within said housing drawing a gas in through said inlet and discharging through said outlet, said impeller having its axis of rotation substantially aligned with the axis of said inlet, a condenser for the compressed gas and a receiver for the liquid discharging from said condenser, means by-passing a portion of the gas from said receiver above the liquid level therein, an evaporator, expansion means controlling the passage of the liquid from said receiver to said evaporator, means connecting the exhaust from said evaporator to said compressor inlet, means including a head control valve for feeding said by-passed gas into said compressor inlet in a direction having a substantial component tangential to the inlet to impart a pre-swirl to the gas feeding into the impeller, and condition responsive means operating said control valve in accordance with the output of the compressor.
- a closed circuit refrigeration system including a centrifugal compressor, a condenser, a liquid receiver, an expansion means and an evaporator connected in a closed circuit in that order, means for bypassing part of the fluid output compressed by the compressor and feeding it into the compressor inlet in a direction having a substantial component tangential to the inlet to impart a preswirl to the entering fluid, and means for controlling the amount of fluid so bypassed in accordance with the compressor output.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Description
July 3, 1962 H. A. GREENWALD VARIABLE HEAD COMPRESSOR Filed June 1, 1959.
[CONDENSER E V4 POI-PA TOR HEAD CON TROL VALVE EXPANSION MEANS United States Patent Ofilice 3,041,848 Fatented July 3, 1962 3,041,848 VARIABLE HEAD COMPRESSOR Harold A. Greenwald, Los Angeles, Calif., assignor to The Garrett Corporation, Los Angeles, Calif., a corporation of California Filed June 1, 1959, Ser. No. 817,187 2 Claims. (Cl. 62197) This invention relates to a centrifugal compressor in which the head or change in pressure through the compressor may be regulated in accordance with load requirements without changing the speed of rotation of the compressor and has for its object the provision of simple and effective means for imparting a pre-swirl to the elastic fluid or gas at the compressor inlet to vary the pressure change through the compressor.
In the operation of centrifugal compressors it is often desired to operate at constant speed while varying the compressor head in accordance with load requirements without changing compressor speed, or starting and stopping the compressor. In other cases it may be desired to maintain a constant head or pressure change through the compressor irrespective of variation in the speed of rotation of the compressor. Both of these results can be obtained by imparting a pre-sWirl to the fluid drawn into the impeller of the compressor and according to this invention, such pre-swirl is created by feeding into the compressor inlet, fluid which has a substantial directional component tangential to the inlet so as to eliect rotation of the inlet fluid prior to its entrance into the impeller.
While the fluid fed tangentially of the inlet to create the pre-swirl may be secured from any source, it is conveniently by-passed from the discharge side of the compressor and in a refrigeration system, for example, may be withdrawn from the receiver above the liquid level therein.
When the pre-swirl imparted to the inlet fluid has a direction of rotation the same as the direction of rotation of the compressor impeller, the head or pressure change through the compressor will be lowered and, conversely, when the pre-swirl has a direction of rotation opposite to the direction of rotation of the compressor impeller, the pressure change through the compressor will be increased.
Another advantageous efl'ect of the pre-swirl imparted to the inlet fluid according to this invention, is a lessening of the tendency of the compressor to surge or hammer because of light loads and low flow, Where such surging or hunting would otherwise manifest itself in a backflow of fluid into the impeller which adversely affects the chiciency of operation of the unit.
It is, therefore, an object of the invention to provide an improved and simplified means for imparting a preswirl to fluid drawn into the impeller of a centrifugal compressor by feeding fluid into the inlet of the compressor in a direction to produce a rotation of pre-swirl of the inlet fluid.
Another object of the invention is the provision of means for varying the pressure change through a centrif ugal compressor in accordance with the preceding object, in which the auxiliary fluid producing the pre-swirl is by-passed from the system at the discharge side of the compressor.
A further object of the invention is to provide direction controlling means for the auxiliary fluid, useable in accordance with the preceding objects, which is readily reversible to eflect pre-swirl in either the same or opposite direction of rotation as that of the compressor impeller, so as to decrease or increase the head or pressure change through the compressor as desired.
Other objects and features of the invention will be readily apparent to those skilled in the art from the specification and appended drawing illustrating certain preferred embodiments in which:
FIG. 1 is a schematic representation of the system employing a variable head compressor according to the present invention, and more particularly representing a closed cycle refrigeration system;
FIG. 2 is a vertical, sectional view through a variable head compressor according to the invention;
FIG. 3 is a transverse sectional view through the compressor inlet, showing the feeding nozzles for the preswirl producing fluid; and
FIG. 4 is a view similar to FIG. 3 but showing the nozzle ring reversed to produce a pre-swirl rotating contrary to the direction of impeller rotation.
In the schematic representation of FIG. 1 there is shown a typical refrigeration system including a centrifugal compressor 1 having an inlet 2 and impeller 3, and an outlet scroll 4. From the outlet scroll 4 the compressed refrigerant fluid, which may by way of example only be Freon gas, is fed through a duct 5 to a condenser 6 where it is liquefied to be received within a receiver 7. Liquid from receiver 7 passes through an expansion means 8, which may be an expansion valve, a restrictive tube, an orifice or other means well known in the art for I producing a pressure drop, to an evaporator 9, where it performs its cooling function with the gas exhausting through a duct 11 to the inlet 2 of the compressor. To impart the pro-swirl to the fluid or refrigerant gas in the inlet 2, by-pass fluid is drawn from the system, for example from above the liquid level in the receiver 7, through a duct 12, having therein a head control valve 13, to an annular chamber 14 disposed about the compressor inlet and supplying a plurality of tangential nozzles 15.
Referring now to FIGS. 2, 3 and 4, compressor housing 15, defining in its upper portion the inlet 2, has disposed therein a ring 17 defining an annular chamber 18 disposed between the ring 17 and the housing 16 and communicating with the duct 12. Through the walls of the ring 17 are disposed a plurality of slots 19 spaced around and through the ring and directed substantially tangential to the inner wall of the ring or at least in a direction having a substantial component tangential to the ring wall. With the nozzle ring 17 disposed as shown in FIGS. 2 and 3, the fluid passing from chamber 18 through the nozzles 19 is directed so as to produce a pre-swirl or rotation of the fluid in the compressor inlet in the same direction as the rotation of the compressor impeller so that, as previously described, there will be eifected a lessening of the head or pressure change through the compressor.
Above the ring 17 in FIG. 2, there is shown a second ring 21 defining a second annular chamber 22 communicating with a passage 23 in the housing 16, this structure being designed to feed by-passed cooling fluid back to the compressor inlet and forming no part of this invention, although the ring 21 in conjunction with inlet conduit 24 serves to maintain the nozzle ring 17 in assembled position. The compressor of FIG. 2 is shown as a two-stage compressor, With the discharge from impeller 3 passing through passageway 25 to a second impeller 26 and thence to the outlet scroll 4. The impellers 3 and 26 are driven by a suitable motor 27 through a shaft 28.
FIG. 4 illustrates the mode of operation with the nozzle ring 17 reversed top-for-bottom from the position of FIG. 2, so that the nozzles are now directing the preswirl imparting fluid in a direction opposite to the direction of rotation of the compressor impeller, whereby the operation is such that the pre-swirl or rotation of the inlet fluid increases the head or pressure change through the compressor.
The head control valve 13, which regulates the flow of the by-passed gas into the pre-swirl producing chamher, is placed in communication with the compressor output, as by communicating means 30, for response to pressure, temperature or other condition in response to variation of which it is desired to vary the head or pressure change through the compressor, this usually being a condition varying in accordance with the load on the compressor so that the head will be varied in accordance with the requirements of the system. Such valves and their operation are well known in the art, such a valve being shown, for example, in the patent to Wood, No. 2,734,443. Suitable controls therefor are found in the patent to Wood, No. 2,479,991 which shows a pressure responsive valve control, and to Jensen, No. 2,780,413 which shows a temperature responsive valve control.
The nozzles 19 have been shown as fixed in their directions through the ring 17, but it will be obvious that adjustable nozzles of known form may be used to vary the direction of fluid flow therethrough to vary the tangential component of fluid movement and thereby control the degree of rotation imparted to the incoming fluid by a given amount of by-pass fluid.
While the invention has been specifically shown in FIG. 1 as applying to a refrigeration system, it is obvious that the pre-swirl producing arrangement of this invention may be utilized as Well in any desired system and may be used where the compressor 1 is acting on other gases, for example air.
While a certain preferred embodiment of the invention has been specifically disclosed, it is understood that the invention is not limited thereto, as many variations will be readily apparent to those skilled in the art and the invention is to be given its broadest possible interpretation consistent with the prior art.
What is claimed is:
1. In a closed cycle refrigeration system, the combination of a variable head compressor comprising a housing having an inlet and an outlet, a centrifugal impeller within said housing drawing a gas in through said inlet and discharging through said outlet, said impeller having its axis of rotation substantially aligned with the axis of said inlet, a condenser for the compressed gas and a receiver for the liquid discharging from said condenser, means by-passing a portion of the gas from said receiver above the liquid level therein, an evaporator, expansion means controlling the passage of the liquid from said receiver to said evaporator, means connecting the exhaust from said evaporator to said compressor inlet, means including a head control valve for feeding said by-passed gas into said compressor inlet in a direction having a substantial component tangential to the inlet to impart a pre-swirl to the gas feeding into the impeller, and condition responsive means operating said control valve in accordance with the output of the compressor.
2. A closed circuit refrigeration system including a centrifugal compressor, a condenser, a liquid receiver, an expansion means and an evaporator connected in a closed circuit in that order, means for bypassing part of the fluid output compressed by the compressor and feeding it into the compressor inlet in a direction having a substantial component tangential to the inlet to impart a preswirl to the entering fluid, and means for controlling the amount of fluid so bypassed in accordance with the compressor output.
References Cited in the file of this patent UNITED STATES PATENTS 2,656,096 Schwarz Oct. 20, 1953 2,660,366 Klein et al Nov. 24, 1953 2,774,219 Kelley Dec. 18, 1956 2,798,658 McDonald July 9, 1957 2,834,534 Kadosch et al. May 13, 1958 2,921,446 Zulinke Jan. 19, 1960 2,936,595 Dillman et al. May 17, 1960 FOREIGN PATENTS 672,194 Great Britain May 14, 1952 803,422 Great Britain Oct. 22, 1958
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US817187A US3041848A (en) | 1959-06-01 | 1959-06-01 | Variable head compressor |
GB19263/60A GB943490A (en) | 1959-06-01 | 1960-05-31 | Improvements relating to refrigerating systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US817187A US3041848A (en) | 1959-06-01 | 1959-06-01 | Variable head compressor |
Publications (1)
Publication Number | Publication Date |
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US3041848A true US3041848A (en) | 1962-07-03 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US817187A Expired - Lifetime US3041848A (en) | 1959-06-01 | 1959-06-01 | Variable head compressor |
Country Status (2)
Country | Link |
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US (1) | US3041848A (en) |
GB (1) | GB943490A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3238534A (en) * | 1962-10-15 | 1966-03-01 | English Electric Co Ltd | Hydraulic pumps and reversible pump turbines |
US3408943A (en) * | 1965-08-31 | 1968-11-05 | Dowty Fuel Syst Ltd | Centrifugal pumps for liquids |
US3645110A (en) * | 1970-05-11 | 1972-02-29 | Gen Motors Corp | Turbulence control |
US3976390A (en) * | 1974-12-23 | 1976-08-24 | Chicago Pneumatic Tool Company | Means for controlling flow instability in centrifugal compressors |
EP0082578A1 (en) * | 1981-12-22 | 1983-06-29 | Thomassen International B.V. | Turbomachine such as a compressor or pump comprising means for improving its part-load behaviour |
EP0150729A2 (en) * | 1984-01-27 | 1985-08-07 | Pratt & Whitney Canada, Inc. | Method and apparatus for improving acceleration in a multi-shaft gas turbine engine |
US4640091A (en) * | 1984-01-27 | 1987-02-03 | Pratt & Whitney Canada Inc. | Apparatus for improving acceleration in a multi-shaft gas turbine engine |
US5816055A (en) * | 1994-02-03 | 1998-10-06 | Svenska Rotor Maskiner Ab | Refrigeration system anad a method for regulating the refrigeration capacity of such a system |
US20060081226A1 (en) * | 2002-10-01 | 2006-04-20 | Martin-Peter Bolz | Electrical charge air compressor provided with an integrated air cooling system |
WO2006043824A1 (en) | 2004-10-18 | 2006-04-27 | Troms Kraft Produksjon As | Device and method for suction pipe |
US20100005799A1 (en) * | 2007-01-19 | 2010-01-14 | Bahram Nikpour | Compressor |
US20110011379A1 (en) * | 2007-12-18 | 2011-01-20 | Neville Jackson | Compressor |
CN104454657A (en) * | 2013-09-25 | 2015-03-25 | 松下电器产业株式会社 | Turbo-compressor and refrigeration cycle apparatus |
EP3030791A1 (en) * | 2013-08-09 | 2016-06-15 | Aeristech Limited | Attachment arrangement for turbo compressor |
WO2017023578A1 (en) * | 2015-08-04 | 2017-02-09 | Carrier Corporation | Centrifugal compressor with swirl injection |
US20230057749A1 (en) * | 2021-08-20 | 2023-02-23 | Carrier Corporation | Compressor including aerodynamic swirl between inlet guide vanes and impeller blades |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004056185A1 (en) * | 2004-11-20 | 2006-06-08 | Bayerische Motoren Werke Ag | turbocharger |
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GB672194A (en) * | 1949-11-01 | 1952-05-14 | Westinghouse Electric Int Co | Improvements in or relating to fans |
US2656096A (en) * | 1946-01-04 | 1953-10-20 | Rateau Soc | Centrifugal pump and compressor |
US2660366A (en) * | 1950-05-03 | 1953-11-24 | Klein Harold | Compressor surge inhibitor |
US2774219A (en) * | 1954-10-27 | 1956-12-18 | Gen Motors Corp | Automobile refrigerating apparatus |
US2798658A (en) * | 1955-03-01 | 1957-07-09 | Westinghouse Electric Corp | Volume controls for centrifugal fans |
US2834534A (en) * | 1951-09-27 | 1958-05-13 | Snecma | Centrifugal air compressor control device |
GB803422A (en) * | 1954-01-27 | 1958-10-22 | Bruno Eck | Radial flow blower for conveying gases with a high dust content |
US2921446A (en) * | 1956-11-02 | 1960-01-19 | Carrier Corp | Refrigeration machine |
US2936595A (en) * | 1956-05-07 | 1960-05-17 | American Radiator & Standard | Air conditioning system |
-
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- 1959-06-01 US US817187A patent/US3041848A/en not_active Expired - Lifetime
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1960
- 1960-05-31 GB GB19263/60A patent/GB943490A/en not_active Expired
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
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US2656096A (en) * | 1946-01-04 | 1953-10-20 | Rateau Soc | Centrifugal pump and compressor |
GB672194A (en) * | 1949-11-01 | 1952-05-14 | Westinghouse Electric Int Co | Improvements in or relating to fans |
US2660366A (en) * | 1950-05-03 | 1953-11-24 | Klein Harold | Compressor surge inhibitor |
US2834534A (en) * | 1951-09-27 | 1958-05-13 | Snecma | Centrifugal air compressor control device |
GB803422A (en) * | 1954-01-27 | 1958-10-22 | Bruno Eck | Radial flow blower for conveying gases with a high dust content |
US2774219A (en) * | 1954-10-27 | 1956-12-18 | Gen Motors Corp | Automobile refrigerating apparatus |
US2798658A (en) * | 1955-03-01 | 1957-07-09 | Westinghouse Electric Corp | Volume controls for centrifugal fans |
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Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3238534A (en) * | 1962-10-15 | 1966-03-01 | English Electric Co Ltd | Hydraulic pumps and reversible pump turbines |
US3408943A (en) * | 1965-08-31 | 1968-11-05 | Dowty Fuel Syst Ltd | Centrifugal pumps for liquids |
US3645110A (en) * | 1970-05-11 | 1972-02-29 | Gen Motors Corp | Turbulence control |
US3976390A (en) * | 1974-12-23 | 1976-08-24 | Chicago Pneumatic Tool Company | Means for controlling flow instability in centrifugal compressors |
EP0082578A1 (en) * | 1981-12-22 | 1983-06-29 | Thomassen International B.V. | Turbomachine such as a compressor or pump comprising means for improving its part-load behaviour |
EP0150729A2 (en) * | 1984-01-27 | 1985-08-07 | Pratt & Whitney Canada, Inc. | Method and apparatus for improving acceleration in a multi-shaft gas turbine engine |
EP0150729A3 (en) * | 1984-01-27 | 1985-08-28 | Pratt & Whitney Canada, Inc. | Method and apparatus for improving acceleration in a multi-shaft gas turbine engine |
US4640091A (en) * | 1984-01-27 | 1987-02-03 | Pratt & Whitney Canada Inc. | Apparatus for improving acceleration in a multi-shaft gas turbine engine |
US5816055A (en) * | 1994-02-03 | 1998-10-06 | Svenska Rotor Maskiner Ab | Refrigeration system anad a method for regulating the refrigeration capacity of such a system |
US7425119B2 (en) * | 2002-10-01 | 2008-09-16 | Robert Bosch Gmbh | Electrical charge air compressor provided with an integrated air cooling system |
US20060081226A1 (en) * | 2002-10-01 | 2006-04-20 | Martin-Peter Bolz | Electrical charge air compressor provided with an integrated air cooling system |
US7802960B2 (en) | 2004-10-18 | 2010-09-28 | Troms Kraft Produksjon As | Device and method for suction pipe |
WO2006043824A1 (en) | 2004-10-18 | 2006-04-27 | Troms Kraft Produksjon As | Device and method for suction pipe |
US20080063510A1 (en) * | 2004-10-18 | 2008-03-13 | Troms Kraft Produksjon As | Device and Method for Suction Pipe |
US20100005799A1 (en) * | 2007-01-19 | 2010-01-14 | Bahram Nikpour | Compressor |
US8256218B2 (en) * | 2007-01-19 | 2012-09-04 | Cummins Turbo Technologies Limited | Compressor |
US8820073B2 (en) | 2007-01-19 | 2014-09-02 | Cummins Turbo Technologies Limited | Compressor |
US20110011379A1 (en) * | 2007-12-18 | 2011-01-20 | Neville Jackson | Compressor |
US8322138B2 (en) * | 2007-12-18 | 2012-12-04 | Cummins Turbo Technologies Limited | Compressor |
EP3030791A1 (en) * | 2013-08-09 | 2016-06-15 | Aeristech Limited | Attachment arrangement for turbo compressor |
US10451087B2 (en) | 2013-08-09 | 2019-10-22 | Aeristech Limited | Attachment arrangement for turbo compressor |
US20150086394A1 (en) * | 2013-09-25 | 2015-03-26 | Panasonic Corporation | Turbo-compressor and refrigeration cycle apparatus |
US9816517B2 (en) * | 2013-09-25 | 2017-11-14 | Panasonic Intellectual Property Management Co., Ltd. | Turbo-compressor and refrigeration cycle apparatus with heated guide vanes |
CN104454657B (en) * | 2013-09-25 | 2018-09-28 | 松下知识产权经营株式会社 | Turbo-compressor and refrigerating circulatory device |
CN104454657A (en) * | 2013-09-25 | 2015-03-25 | 松下电器产业株式会社 | Turbo-compressor and refrigeration cycle apparatus |
WO2017023578A1 (en) * | 2015-08-04 | 2017-02-09 | Carrier Corporation | Centrifugal compressor with swirl injection |
US20230057749A1 (en) * | 2021-08-20 | 2023-02-23 | Carrier Corporation | Compressor including aerodynamic swirl between inlet guide vanes and impeller blades |
US11655825B2 (en) * | 2021-08-20 | 2023-05-23 | Carrier Corporation | Compressor including aerodynamic swirl between inlet guide vanes and impeller blades |
Also Published As
Publication number | Publication date |
---|---|
GB943490A (en) | 1963-12-04 |
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