US2470565A - Surge preventing device for centrifugal compressors - Google Patents

Surge preventing device for centrifugal compressors Download PDF

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US2470565A
US2470565A US621193A US62119345A US2470565A US 2470565 A US2470565 A US 2470565A US 621193 A US621193 A US 621193A US 62119345 A US62119345 A US 62119345A US 2470565 A US2470565 A US 2470565A
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chamber
valve
pressure
impeller
port
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US621193A
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Isidor R Loss
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Ingersoll Rand Co
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Ingersoll Rand Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0207Surge control by bleeding, bypassing or recycling fluids

Definitions

  • This invention relates to compressors, but more particularly to compressors of the centrifugal type.
  • One object of the invention is to prevent the surging of compressed air back through the discharge line of the compressor into the impeller chamber.
  • Figure 1 is a longitudinal elevation, partly broken away, of a centrifugal compressor. equipped with a surge preventing device constructed in accordance with the practice of the invention and showing the device connected for operation in response to pressure values existing at relatively spaced points in the discharge channel of the compressor, and
  • Figure 2 is a view similar to Figure 1 showing the surge preventing device connected for operation in response to pressure values existing at relatively spaced points in the inlet conduit of the compressor.
  • 20 designates a centrifugal compressor the casing 2
  • an impeller 25 for pumping fluid medium from the inlet opening 26 of the compressor to the chambers 23 and 24, and said impeller is interlockingly secured to the end of a shaft 21 extending axially into the impeller chamber.
  • the compressor is provided with means for preventing the compressed medium from breaking back through the discharge line into the impeller chamber whenever the normal pressure condition in the discharge line is disturbed, as when operating at light load or when a machine operated by the compressed fluid is suddenly shut-off and in consequence of which a pressure will build up in the discharge channels of the compressor that will overcome the current issuing from the impeller and cause a pulsation or pumping effect. in the compressor.
  • the means serving to obviate this unfavorable occurrence includes a relief port 28 for the discharge channel and a passage 29 leading from the port 28 to the inlet opening 26.
  • the port 28 opens into the diil'usor chamber 23. It is preferably 5 Claims. (Cl. 230-115) 2 located immediately adjacent the impeller tip and is controlled by a valve 20 of the poppet type the stem 2
  • the outer end of the cylinder is sealed by a cover 34 that also acts as an abutment for the end of the stem 2! which, in the example shown.
  • the inner end of the cylinder 22 contains a compression spring l9 that seats against the end wall of the cylinder 33 and against the piston 32 and is biased to hold the valve 22 away from the port 28.
  • Any suitable pressure medium may be introduced into the chamber 36 for holding the valve 36 in position to seal the port 28, and such medium is conveyed to and from the chamber 35 by a conduit 36 leading from a valve casing 31 that may be aflixed to the compressor and has a chamber 38 for the accommodation of a reciprocatory valve 39;
  • the valve 29 is of generally cylindrical shape and in its periphery is an annular groove 40 to afford communication between the conduit 36 and a pressure medium supply conduit 4
  • the valve 39 also controls the exhaust of fluid medium from the chamber 35 and to this end is provided, in the side thereof, with a recess 42 of suitable length to span the end of the conduit 36 and. an end of a discharge conduit 43 threaded into the casing 31 and communicating with the chamber 38.
  • the ends of the casing 31 are suitably vented to the atmosphere to assure the unrestricted movement of the valve 39 in the casing.
  • the valve 39 is shifted by an actuator that moves responsively to a differential existing between pressures acting on the opposed sides thereof and derived from up-stream and down-stream points in the discharge channel of the compressor.
  • the actuator consists of a flexible diaphragm 44 the marginal portion of which is clamped between two plates 45 and 46 that are recessed to provide pressure chambers 41 and 48, respectively.
  • the axial portion of the diaphragm 44 is secured to the end of a stem 49 carried by the valve 39, and the aperture 50 in the plate 46 through which the stem 49 extends is sealed by a suitable packing device 5
  • the diaphragm 44 is so positioned with respect to the valve 39 that when the interposed between the plate 48 and the dia-.
  • the pressure fluid serving to actuate the diaphragm is conveyed to the chamber 48 from the diffuser chamber 23 by a conduit 52 threadedly connected to the cover 48 at one end and at its other end to the casing 2
  • conveys pressure fluid from the discharge end 88 of the volute chamber 24 to the chamber 41.
  • valve 39 will blank off the supply conduit 4
  • the spring i9 will then shift the valve 30 away from the port 28 and permit the com-v
  • the diaphragm 44 and the valve 39 move in response to a differential between pressures existing at relatively spaced points in the.
  • inlet conduit 51 of the compressor which has means for creating a sub-normal pressure therein.
  • Such means is shown as being in the form of an orifice meter 58 and the space encircling it and that directly adjacent thereto constitute a zone 59 of sub-normal pressure.
  • This zone 59 is in communication with the chamber 48 through a conduit 88, and a conduit 8
  • a spring 82 is phragm 44 to augment the pressure in the cham-. ber 48 for shifting the valve 39 leftward to blank I 4 38 in position to establish communication between the conduits 38 and 43.
  • the pressure within the chamber 41 being normal inlet pressure, will overcome the pressure of the fluid in the chamber 48 and that of the spring 82 and move the valve 39 to the right hand limiting position in the chamber 38. In this position of the valve 39 pressure medium will flow into the chamber 35 against the piston 32 and move the valve 38 into sealing relationship with the port 28.
  • valves will remain in the positions described as long as pressure conditions in the inlet and discharge channels remain normal. But if the pressure in the discharge channel closely approaches the value at which it may surge back toward the impeller this pressure condition is communicated through the impeller chamber and the zone 59 to the chamber 48 and will cause the pressure therein, together with the force exerted by the spring 82 to shift the valve 38 leftward.
  • valve will first cutoff the pressure chamber 35 from the source of fluid medium supply and next place said chamber into communication with the atmosphere through the recess 42 and the conduit 43.
  • a centrifugal compressor having an inlet channel and a discharge channel, an impeller to pump fluid from the inlet channel into the discharge channel, a relief port for the discharge channel adjacent the tip of the impeller, and means acting in response to an ab.- normal ratio of pressure values substantially at the impeller and at a point existing at a point relatively spaced-from the first mentioned point to valve fluid from the discharge channel and thereby prevent the surging of compressed fluid from the discharge channel back through the impeller.
  • a centrifugal compressor having an inlet opening and a discharge channel and a diffusor chamber, an impeller to pump fluid from the inlet opening into said channel, a relief port for the difiusor chamber adjacent the tip of the impeller, and means acting in response to an abnormal ratio of fluid pressure values existing at a point substantially at the tip of the impeller and at a point relatively spaced from the first mentioned point to valve fluid from said discharge channel and thereby prevent the surging of compressed fluid from the channel back through the impeller.
  • a centrifugal compressor having an inlet opening and a discharge channel, an impeller to pump fluid from the inlet opening into the discharge channel, a relief port positioned adjacent the tip of the impeller for the discharge channel, a fluid actuated relief valve to govern .fiuid flow through the relief port, a spring acting constantly to position the relief valve :or opening the port, a control valve for regulating flow of a pressure medium to position the rea off-the supply conduit 4
  • a centrifugal compressor flow through the relief port, a spring acting constantly to position the relief valve for opening the port, a control valve for regulating fiow of a having inlet and discharge channels, an impeller pressure medium to position the relief valve for closing the port and for controlling the exhaust of such pressure medium from the relief valve. and a flexible diaphragm for actuating the control valve acting responsively to a pressure differential existing in one of said channels.

Description

Ht" 1 5' L R, oss 2fi7,fi
SURGE PREVENTING DEVICE FOR CENTRIFUGAL COMPRESS ORS Filed 001;. 9, 1945 HIS ATTORNEY.
Patented May 17, 1949 SURGE PREVENTING navroa Foa em- TRIFUGAL comraassons Isidor R. Loss; Rowayton, Conn., auignor to Ingersoll-Rand Company, New York, N. Y., a cotporation of New Jersey Application October 9, 1945, Serial No. 621,193
This invention relates to compressors, but more particularly to compressors of the centrifugal type.
One object of the invention is to prevent the surging of compressed air back through the discharge line of the compressor into the impeller chamber. 3
Other objects will be in part obvious and in part pointed out hereinafter.
In the drawings accompanying this specification and in which similar reference numerals refer to similar parts,
Figure 1 is a longitudinal elevation, partly broken away, of a centrifugal compressor. equipped with a surge preventing device constructed in accordance with the practice of the invention and showing the device connected for operation in response to pressure values existing at relatively spaced points in the discharge channel of the compressor, and
Figure 2 is a view similar to Figure 1 showing the surge preventing device connected for operation in response to pressure values existing at relatively spaced points in the inlet conduit of the compressor.
Referring more particularly to the drawings, 20 designates a centrifugal compressor the casing 2| of which is recessed to provide an impeller chamber 22, a diifusor chamber 23 encircling the impeller chamber and a volute discharge chamber 24 around the diifusor chamber 23. Within the impeller chamber 22 is an impeller 25 for pumping fluid medium from the inlet opening 26 of the compressor to the chambers 23 and 24, and said impeller is interlockingly secured to the end of a shaft 21 extending axially into the impeller chamber.
In accordance with the practice of the invention, the compressor is provided with means for preventing the compressed medium from breaking back through the discharge line into the impeller chamber whenever the normal pressure condition in the discharge line is disturbed, as when operating at light load or when a machine operated by the compressed fluid is suddenly shut-off and in consequence of which a pressure will build up in the discharge channels of the compressor that will overcome the current issuing from the impeller and cause a pulsation or pumping effect. in the compressor.
The means serving to obviate this unfavorable occurrence includes a relief port 28 for the discharge channel and a passage 29 leading from the port 28 to the inlet opening 26. The port 28 opens into the diil'usor chamber 23. It is preferably 5 Claims. (Cl. 230-115) 2 located immediately adjacent the impeller tip and is controlled by a valve 20 of the poppet type the stem 2| of which carries a piston 22 that is slidazb'le in a cylinder 22 on the compressor cas- The outer end of the cylinder is sealed by a cover 34 that also acts as an abutment for the end of the stem 2! which, in the example shown. projects from the piston 22 to abut the cover 34 and hold the piston in spaced relation therewith to define a pressure chamber 26 in the outer end of the cylinder 23 for fluid medium serving to hold the valve 20 in its port-closing position. The inner end of the cylinder 22 contains a compression spring l9 that seats against the end wall of the cylinder 33 and against the piston 32 and is biased to hold the valve 22 away from the port 28.
Any suitable pressure medium may be introduced into the chamber 36 for holding the valve 36 in position to seal the port 28, and such medium is conveyed to and from the chamber 35 by a conduit 36 leading from a valve casing 31 that may be aflixed to the compressor and has a chamber 38 for the accommodation of a reciprocatory valve 39; The valve 29 is of generally cylindrical shape and in its periphery is an annular groove 40 to afford communication between the conduit 36 and a pressure medium supply conduit 4| threadedly connected to the casing 31.
The valve 39 also controls the exhaust of fluid medium from the chamber 35 and to this end is provided, in the side thereof, with a recess 42 of suitable length to span the end of the conduit 36 and. an end of a discharge conduit 43 threaded into the casing 31 and communicating with the chamber 38. The ends of the casing 31 are suitably vented to the atmosphere to assure the unrestricted movement of the valve 39 in the casing.
The valve 39 is shifted by an actuator that moves responsively to a differential existing between pressures acting on the opposed sides thereof and derived from up-stream and down-stream points in the discharge channel of the compressor. In the form illustrated the actuator consists of a flexible diaphragm 44 the marginal portion of which is clamped between two plates 45 and 46 that are recessed to provide pressure chambers 41 and 48, respectively.
The axial portion of the diaphragm 44 is secured to the end of a stem 49 carried by the valve 39, and the aperture 50 in the plate 46 through which the stem 49 extends is sealed by a suitable packing device 5|. The diaphragm 44 is so positioned with respect to the valve 39 that when the interposed between the plate 48 and the dia-.
3 diaphragm occupies the neutral or relaxed position both the annular groove 48 and the recess 42 will be out ofcommunication with the supply conduit 4| and said conduit will be blanked off by a cylindrical portion of the valve 38 located between the annular groove 48 and the recess 42.
The pressure fluid serving to actuate the diaphragm is conveyed to the chamber 48 from the diffuser chamber 23 by a conduit 52 threadedly connected to the cover 48 at one end and at its other end to the casing 2| to communicate with a port 53 opening into the diflusor chamber 28 adjacent the tip 54 of the impeller 25. Similarly, a conduit 55 threadedly connected to the cover 45 and to the casing 2| conveys pressure fluid from the discharge end 88 of the volute chamber 24 to the chamber 41.
During the normal operation of the machine, the superior pressure in the chamber 41 acting against the diaphragm will shift the valve 39 toward the right hand end of the casing 31 and thereby place the annular groove 40 in communication with the supply conduit 4i and the conduit 88. Pressure medium will then flow through the conduits into the chamber 35 against the piston 32 and move the valve 30 into sealing relationship with the port 28. All the air there-. after discharged by the impeller will pass through the discharge channels of the compressor, for utilization, and the valves 39 and 30 will remain in the positions described as long as the pressure in the chamber 41 predominates over that in the chamber 48.
If, for any reason, the pressure in the discharge channel surges back toward the impeller, such impulse will be communicated through the conduit 52 against the side of the diaphragm in the chamber 48 and will shift the valve 39 leftward.
In this position the valve 39 will blank off the supply conduit 4| and will establish communication between the conduits 38 and 43 to effect an outlet for the pressure medium in the chamber 35. The spring i9 will then shift the valve 30 away from the port 28 and permit the com-v In the modified form of the invention shownin Figure 2, the diaphragm 44 and the valve 39 move in response to a differential between pressures existing at relatively spaced points in the.
inlet conduit 51 of the compressor which has means for creating a sub-normal pressure therein. Such means is shown as being in the form of an orifice meter 58 and the space encircling it and that directly adjacent thereto constitute a zone 59 of sub-normal pressure. This zone 59 is in communication with the chamber 48 through a conduit 88, and a conduit 8| affords communication between the chamber 41 and the inlet conduit 51 at a point on the up-stream side of the orifice meter 58. 1
In this form of the invention, a spring 82 is phragm 44 to augment the pressure in the cham-. ber 48 for shifting the valve 39 leftward to blank I 4 38 in position to establish communication between the conduits 38 and 43.
During the operation of the device, the pressure within the chamber 41, being normal inlet pressure, will overcome the pressure of the fluid in the chamber 48 and that of the spring 82 and move the valve 39 to the right hand limiting position in the chamber 38. In this position of the valve 39 pressure medium will flow into the chamber 35 against the piston 32 and move the valve 38 into sealing relationship with the port 28.
The valves will remain in the positions described as long as pressure conditions in the inlet and discharge channels remain normal. But if the pressure in the discharge channel closely approaches the value at which it may surge back toward the impeller this pressure condition is communicated through the impeller chamber and the zone 59 to the chamber 48 and will cause the pressure therein, together with the force exerted by the spring 82 to shift the valve 38 leftward.
During this movement, the valve will first cutoff the pressure chamber 35 from the source of fluid medium supply and next place said chamber into communication with the atmosphere through the recess 42 and the conduit 43. The
spring l9 will then shift the valve .30 away from the port'28, and any compressed fluid surging back through the discharge channel in the direction of the impeller will escape through the port 28 and the passage 29 into the inlet conduit. These movements of the valves will take place in anticipation of a surge in the discharge line and the port 28 will, therefore, be uncovered before the surge reaches the impeller.
I claim:
1. In combination, a centrifugal compressor having an inlet channel and a discharge channel, an impeller to pump fluid from the inlet channel into the discharge channel, a relief port for the discharge channel adjacent the tip of the impeller, and means acting in response to an ab.- normal ratio of pressure values substantially at the impeller and at a point existing at a point relatively spaced-from the first mentioned point to valve fluid from the discharge channel and thereby prevent the surging of compressed fluid from the discharge channel back through the impeller.
2. In combination, a centrifugal compressor having an inlet opening and a discharge channel and a diffusor chamber, an impeller to pump fluid from the inlet opening into said channel, a relief port for the difiusor chamber adjacent the tip of the impeller, and means acting in response to an abnormal ratio of fluid pressure values existing at a point substantially at the tip of the impeller and at a point relatively spaced from the first mentioned point to valve fluid from said discharge channel and thereby prevent the surging of compressed fluid from the channel back through the impeller.
3. In combination, a centrifugal compressor having an inlet opening and a discharge channel, an impeller to pump fluid from the inlet opening into the discharge channel, a relief port positioned adjacent the tip of the impeller for the discharge channel, a fluid actuated relief valve to govern .fiuid flow through the relief port, a spring acting constantly to position the relief valve :or opening the port, a control valve for regulating flow of a pressure medium to position the rea off-the supply conduit 4| and to place the valve lief valve for closing the port and to control the exhaust of suchpressure medium from the relief valve, and a flexible diaphragm acting responsively to a pressure differential existing in th nel, a relief port for the difl'usor chamber positioned adjacent the tip of the impeller, a fluid actuated relief valve for the relief port, a control valve to regulate the flow of a pressure fluid to the relief valve and to exhaust said fluid therefrom, means within the inlet channel for creating a subnormal pressure area therein, and a flexible diaphragm responsive to pressure variations in the subnormal pressure area for actuating the control valve.
5. In combination, a centrifugal compressor flow through the relief port, a spring acting constantly to position the relief valve for opening the port, a control valve for regulating fiow of a having inlet and discharge channels, an impeller pressure medium to position the relief valve for closing the port and for controlling the exhaust of such pressure medium from the relief valve. and a flexible diaphragm for actuating the control valve acting responsively to a pressure differential existing in one of said channels.
ISIDOR R. LOSS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Price Feb. 22, 1944
US621193A 1945-10-09 1945-10-09 Surge preventing device for centrifugal compressors Expired - Lifetime US2470565A (en)

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Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2574631A (en) * 1950-04-28 1951-11-13 Ely George William Constant pressure centrifugal pump
US2660366A (en) * 1950-05-03 1953-11-24 Klein Harold Compressor surge inhibitor
US2661145A (en) * 1947-03-11 1953-12-01 Guardite Corp Antisurge control for refrigeration compressors
US2798657A (en) * 1954-08-30 1957-07-09 Gen Electric Compressor
US2888809A (en) * 1955-01-27 1959-06-02 Carrier Corp Gas compression apparatus
US2933236A (en) * 1955-12-09 1960-04-19 Power Jets Res & Dev Ltd Rotary dynamic compressors
US2986327A (en) * 1957-11-04 1961-05-30 Fairchild Engine & Airplane Axial flow centrifugal compressor and surge control system therefor
US3002521A (en) * 1956-10-09 1961-10-03 Fairchild Stratos Corp Surge controller for compressors and pumps
US3029633A (en) * 1957-09-23 1962-04-17 Marquardt Corp Buzz detector
US3079121A (en) * 1957-06-11 1963-02-26 Garrett Corp Surge control device for centrifugal compressors
DE1157485B (en) * 1956-06-29 1963-11-14 Eta Corp G M B H Centrifugal or guide wheel with moving blades
US3150814A (en) * 1962-07-23 1964-09-29 Caterpillar Tractor Co System and method for controlling turbine speed
US3168870A (en) * 1962-12-12 1965-02-09 Ingersoll Rand Co Centrifugal pump with adjustable capacity
US3268155A (en) * 1964-02-07 1966-08-23 Ingersoll Rand Co Fluid-flow control system
US3348764A (en) * 1965-10-21 1967-10-24 Whirlpool Co Pressure equalizing means for compressors and the like
US3447469A (en) * 1967-10-17 1969-06-03 Nikolaus Laing Induction motor having spherical airgap
US3901620A (en) * 1973-10-23 1975-08-26 Howell Instruments Method and apparatus for compressor surge control
US3977809A (en) * 1974-02-14 1976-08-31 A. Petit & Co. S.A.R.L. Controlled discharge pressure pump for pumping liquids
US4039267A (en) * 1974-12-18 1977-08-02 Bbc Brown Boveri & Company Limited Method and apparatus for starting a blower
DE2941704A1 (en) * 1978-10-16 1980-04-17 Nissan Motor TURBOCHARGER FOR INTERNAL COMBUSTION ENGINES
US4205941A (en) * 1977-05-16 1980-06-03 Office National D'etudes Et De Recherches Aerospatiales (O.N.E.R.A.) Methods and apparatuses for avoiding surging phenomena in compressors
US4230437A (en) * 1979-06-15 1980-10-28 Phillips Petroleum Company Compressor surge control system
FR2459388A1 (en) * 1979-06-18 1981-01-09 Westinghouse Electric Corp METHOD AND APPARATUS FOR DETECTING AND CONTROLLING PUMPING IN CENTRIFUGAL GAS COMPRESSORS
US4347711A (en) * 1980-07-25 1982-09-07 The Garrett Corporation Heat-actuated space conditioning unit with bottoming cycle
US4413946A (en) * 1981-08-20 1983-11-08 Dresser Industries, Inc. Vented compressor inlet guide
EP0123515A1 (en) * 1983-04-22 1984-10-31 The Garrett Corporation Compressor apparatus
US4493607A (en) * 1982-12-16 1985-01-15 Hudson Engineering Company Tee-type valve for self-priming pump system
US4521156A (en) * 1982-12-16 1985-06-04 Hudson Engineering Company Self-priming pump system having diaphragm-type flow sensor
US4641495A (en) * 1985-02-05 1987-02-10 A/S Kongsberg Vapenfabrikk Dual entry radial turbine gas generator
US4653978A (en) * 1984-07-19 1987-03-31 Hale Fire Pump Company Relief valve system
US4662817A (en) * 1985-08-20 1987-05-05 The Garrett Corporation Apparatus and methods for preventing compressor surge
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US5618160A (en) * 1994-05-23 1997-04-08 Ebara Corporation Turbomachinery with variable angle fluid guiding devices
US5683223A (en) * 1994-05-19 1997-11-04 Ebara Corporation Surge detection device and turbomachinery therewith
US20030138317A1 (en) * 1998-12-10 2003-07-24 Mark Barnett Casing treatment for a fluid compressor
US20050022552A1 (en) * 2003-07-30 2005-02-03 Lucas Clifford E. Utilization of bogdown of single-shaft gas turbines to minimize relief flows in baseload LNG plants
EP1538339A1 (en) * 2003-12-04 2005-06-08 TCG Unitech Systemtechnik GmbH Radial pump
WO2008125381A1 (en) * 2007-04-16 2008-10-23 Continental Automotive Gmbh Compressor housing and turbocharger
US20110255963A1 (en) * 2010-04-19 2011-10-20 Chun Kyung Kim Centrifugal compressor
DE102014013224B3 (en) * 2014-09-05 2015-07-30 Geräte- und Pumpenbau GmbH Dr. Eugen Schmidt control device
US20160131148A1 (en) * 2013-09-27 2016-05-12 Ihi Corporation Centrifugal compressor and turbocharger
US20170037856A1 (en) * 2015-08-03 2017-02-09 Parker-Hannifin Corporation Integral pump pressure relief valve
US20180066573A1 (en) * 2015-06-18 2018-03-08 Bayerische Motoren Werke Aktiengesellschaft Turbocharger for a Motor Vehicle
US20190211845A1 (en) * 2016-11-17 2019-07-11 Ihi Corporation Centrifugal compressor
US11378084B2 (en) * 2013-09-12 2022-07-05 Ebara Corporation Apparatus and method for alleviating and preventing cavitation surge of water supply conduit system

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US1241372A (en) * 1913-07-08 1917-09-25 Escher Wyss Maschf Ag Apparatus for operating the blow-off valves of centrifugal compressors or pumps.
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US2317723A (en) * 1939-02-04 1943-04-27 Becht Walter Air blower
US2342219A (en) * 1940-03-15 1944-02-22 Lockheed Aircraft Corp Centrifugal supercharger

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US1267880A (en) * 1918-05-28 Gen Electric Centrifugal compressor.
US1110864A (en) * 1912-10-25 1914-09-15 Ingersoll Rand Co Centrifugal compressor.
US1241372A (en) * 1913-07-08 1917-09-25 Escher Wyss Maschf Ag Apparatus for operating the blow-off valves of centrifugal compressors or pumps.
US2317723A (en) * 1939-02-04 1943-04-27 Becht Walter Air blower
US2342219A (en) * 1940-03-15 1944-02-22 Lockheed Aircraft Corp Centrifugal supercharger

Cited By (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2661145A (en) * 1947-03-11 1953-12-01 Guardite Corp Antisurge control for refrigeration compressors
US2574631A (en) * 1950-04-28 1951-11-13 Ely George William Constant pressure centrifugal pump
US2660366A (en) * 1950-05-03 1953-11-24 Klein Harold Compressor surge inhibitor
US2798657A (en) * 1954-08-30 1957-07-09 Gen Electric Compressor
US2888809A (en) * 1955-01-27 1959-06-02 Carrier Corp Gas compression apparatus
US2933236A (en) * 1955-12-09 1960-04-19 Power Jets Res & Dev Ltd Rotary dynamic compressors
DE1157485B (en) * 1956-06-29 1963-11-14 Eta Corp G M B H Centrifugal or guide wheel with moving blades
US3002521A (en) * 1956-10-09 1961-10-03 Fairchild Stratos Corp Surge controller for compressors and pumps
US3079121A (en) * 1957-06-11 1963-02-26 Garrett Corp Surge control device for centrifugal compressors
US3029633A (en) * 1957-09-23 1962-04-17 Marquardt Corp Buzz detector
US2986327A (en) * 1957-11-04 1961-05-30 Fairchild Engine & Airplane Axial flow centrifugal compressor and surge control system therefor
US3150814A (en) * 1962-07-23 1964-09-29 Caterpillar Tractor Co System and method for controlling turbine speed
US3168870A (en) * 1962-12-12 1965-02-09 Ingersoll Rand Co Centrifugal pump with adjustable capacity
US3268155A (en) * 1964-02-07 1966-08-23 Ingersoll Rand Co Fluid-flow control system
US3348764A (en) * 1965-10-21 1967-10-24 Whirlpool Co Pressure equalizing means for compressors and the like
US3447469A (en) * 1967-10-17 1969-06-03 Nikolaus Laing Induction motor having spherical airgap
US3901620A (en) * 1973-10-23 1975-08-26 Howell Instruments Method and apparatus for compressor surge control
US3977809A (en) * 1974-02-14 1976-08-31 A. Petit & Co. S.A.R.L. Controlled discharge pressure pump for pumping liquids
US4039267A (en) * 1974-12-18 1977-08-02 Bbc Brown Boveri & Company Limited Method and apparatus for starting a blower
US4205941A (en) * 1977-05-16 1980-06-03 Office National D'etudes Et De Recherches Aerospatiales (O.N.E.R.A.) Methods and apparatuses for avoiding surging phenomena in compressors
DE2941704A1 (en) * 1978-10-16 1980-04-17 Nissan Motor TURBOCHARGER FOR INTERNAL COMBUSTION ENGINES
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