US2431398A - Supercharger with controllable inlet - Google Patents

Supercharger with controllable inlet Download PDF

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Publication number
US2431398A
US2431398A US550655A US55065544A US2431398A US 2431398 A US2431398 A US 2431398A US 550655 A US550655 A US 550655A US 55065544 A US55065544 A US 55065544A US 2431398 A US2431398 A US 2431398A
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United States
Prior art keywords
piston
chamber
impeller
supercharger
air
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Expired - Lifetime
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US550655A
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Hasbrouck Augustus
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Raytheon Technologies Corp
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United Aircraft Corp
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Priority to US550655A priority Critical patent/US2431398A/en
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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
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • F04D29/464Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • 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
    • F04D27/0253Surge control by throttling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/33Compressors for piston combustion engines
    • F02M2700/331Charging and scavenging compressors
    • F02M2700/335Control therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/51Inlet

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Description

Nov. 25, 1947. A. HASBROUCK 2,431,398
SUPERCHARGER WITH C ONTROLLABLE INLET Filed Aug. 22, 1944 IN V EN TOR.
Patented Nov. 25, 1947 SUPERCHARGER WITH CON TROLLABLE INLET Augustus Hasbrouck, Middletown, Conn., assignor to United Aircraft Corporation, East Hartford, Conn., a corporation of Delaware Application August 22, 1944, Serial No. 550,655
7 Claims.
This invention relates to superchargers for internal combustion engines and has for its object to provide a novel and improved device of this type with means for varying the supply of air to the engine.
Another object of the invention is to provide means for throttling the entrance to a supercharger in such a way as to insure the symmetrical distribution of air to the impeller under all conditions of throttling and loading.
Another object is to vary the amount of air pumped by a supercharger by varying the inlet area of the system, and at the same time provide a beneficial pre-rotation of air as it enters the impeller.
Still another object is to provide a simple and efficient supercharger of the foregoing type having novel and improved details of construction and features of operation.
Various other objects and advantages will be apparent as the nature of the invention is more fully disclosed.
In the embodiment of the invention disclosed herein for'purposes of illustration, I vary the amount of air pumped by a supercharger by providing a movable baffle or piston to vary the inlet area of the supercharger. The intake air passes between a stationary wall and the movable piston, and, as the piston is moved with respect to said wall, the intake area and consequently the amount of intake air is varied.
The control means for the piston may comprise, for example, a rotatable shaft acting through suitable gears to rotate a spur gear meshing with teeth on the piston. To translate the resulting rotary movement of the piston into axial movement, helical threads or splines are provided between the piston and a stationary hub on which the piston is mounted.
A particular advantage of my improved construction is that it insures the symmetrical distribution of air to the impeller under all conditions of throttling and loading. non-turbulent flow is obtained because a Venturilike shape for the inlet passage is maintained at all throttle, or control lever, positions. Smooth throttle or control lever operation is insured. by the provision of means for equalizing the pressure on opposite sides of the piston, thus maintaining the force required to move the same substantially constant.
Although the novel features which are characteristic of this invention are set forth more in detail in the claims appended hereto, the nature and scope of the invention may be better under- Substantially.
2 stood by referring to the following description, taken in connection with the accompanying drawing forming a part thereof, in which a specific embodiment has been set forth for purposes of illustration.
The drawing is a schematic vertical sectional view illustrating a supercharger constructed in accordance with the invention.
In the following description certain specific terms are used for convenience in referring to the various details of the invention. These terms, however, are to be interpreted as broadly as the state of the art will permit.
The drawing shows the casing 5 of an internal combustion engine, within which is journaled a shaft 6 carrying the impeller I. The shaft 6 is driven by the engine, or by the exhaust gases, in any suitable manner well understood in the art.
An air inlet passage 8 communicates with the intake chamber 9 which has a stationary Venturishaped wall ID. The blades of the impeller 'I make a close running fit with the Venturi-shaped wall Ill which leads through a passage containing the usual stationary directional blades I2 to the inlet manifold I3.
The intake chamber 9 contains a, stationary cylindrical hub or drum I4 in axial alignment with the impeller shaft 6. Mounted on the hub I4, and movable axially thereof, is a bafile or.-
piston I5 having a cylindrical skirt l6 telescoped within the cylindrical wall ll of casing 5, and a front wall 18 suitably shaped to direct the air in chamber 9 to the impeller. The skirt l6 of the piston is preferably provided with piston rings I9 engaging the cylindrical wall II of the casing for sealing purposes.
The piston I5 is actuated by a control lever 2| carried by a rotatable shaft 22 journaled in casing 5. Shaft 22 carries a bevel gear 23 meshing with a similar gear 24 on shaft 25 which also carries a spur gear 26 meshing with teeth 21 on the piston l5 to rotate the latter. This rotary movement of the piston I5 is translated into axial movement by means of cooperating helical threads or splines 28 on the piston and the stationary hub M, as shown in the drawing.
Accordingly, whenever the control lever 2| is actuated, the piston I5 is moved axially upon the hub I4, either toward or away from the stationary Venturi-shaped wall l0 depending upon the direction of movement of the control lever. In the position shown in full lines in the drawing the control lever 2| is in its open position, and in this position the piston I5 is withdrawn the maximum distance into the cylindrical 'wall II of the casing. However, when control lever 2lis moved to the dotted line position shown in the drawing, the piston I5 is moved outwardly to its maximum limiting position adjacent the wall in as indicated ,throttle or control lever positions, with resulting symmetrical distribution of air to the impeller under all conditions of throttling and loading. The foregoing construction also results in a beneficial pre-rotation of air as it enters the impeller. Heretofore, such uniformity of distribution and pre-rotative effect have been obtainable only by using an axial inlet, and limits on engine length have precluded the possibility of suflicient length of axial inlet to accomplish any beneficial result.
In the embodiment illustrated, smooth throttle or control lever operation is insured by the provision of balance holes 30 in the front wall l8 of the piston to equalize the air pressure on opposite sides of the piston, thus maintaining the force required to move the same substantially constant.
A plurality of holes 3i in the annular throat of the Venturi wall In open into an annular passage 32 which is connected to an air duct 33 which may be utilized to provide the suction side of the metering differential for a pressure type carburetor. The static side of such difierential may be connected to any suitable point upstream from the annular Venturi throat.
Although a specific embodiment has been shown and described herein for purposes of iilustration, it will be evident to those skilled in the art that numerous modifications and adaptations may be made without departing from the scope and spirit of the invention as defined in the appended claims.
What is claimed is:
1. A supercharger for internal combustion engines comprising an air intake chamber having a stationary Venturi-shaped wall, a rotary impeller in said chamber, a, stationary cylindrical hub in said chamber in axial alignment with said impeller, a piston movably mounted on said hub and cooperating with said stationary wall to direct the air in said chamber to said impeller,
- means for imparting rotary movement to said piston, and means for converting said rotary movement of said piston into axial movement thereof to vary the effective intake area of said chamber.
2. A supercharger for internal combustion engines comprising an air intake chamber having a stationary Venturi-shaped wall, a rotary impeller in said chamber, a stationary cylindrical hub in said chamber in axial alignment with said impeller, a piston movably mounted on said hub and cooperating with said stationary wall to direct the air in said chamber to said impeller, means for imparting rotary movement to said piston, and cooperating helical threads on said hub and said piston for converting rotary movement of said piston into axial movement thereof to vary the effective intake area of said chamber.
3. A supercharger for internal combustion engines comprising an air intake chamber having a stationary Venturi-shaped wall, a rotary impeller in said chamber, a stationary cylindrical hub in said chamber in axial alignment with said impeller, a piston movably mounted o said hub and cooperating with said stationary wall to direct the air in said chamber to said impeller, means for imparting rotary movement to said piston, cooperating helical threads on said hub and said piston for converting rotary movement of said piston into axial movement thereof to vary the effective intake area of said chamber, and means for equalizing the pressure on opposite sides of said piston to maintain the force required to move same substantially constant.
4. A supercharger for internal combustion engines comprising an air intake chamber having a stationary Venturi-shaped wall, a rotary impeller in said chamber, a stationary cylindrical hub in said chamber in axial alignment with said impeller, a piston movably mounted on said hub and cooperating with said stationary wall to direct the air in said chamber to said impeller, means for imparting rotary movement to said piston, and cooperating helical threads on said hub and said piston for converting rotary movement of said piston into axial movement thereof to vary the effective intake area of said chamber, said piston containing balance holes to equalize the pressure on opposite sides thereof,
5. A supercharger for internal combustion engines comprising an air inlet chamber having a circular depression in the end wall thereof, a stationary threaded hub anchored in said end wall, a piston on said hub having grooves engaging the threads of said hub and movable into adjusted positions in said depression, a revoluble shaft extending into said chamber in alignment with said hub and having an impeller thereon and a Venturi wall surrounding said impeller.
6. The supercharger of claim 5 in which said Venturi wall is provided with a pluarlity of holes in the throat thereof.
7. The supercharger of claim 5 in which said Venturi wall is provided with a plurality of holes in the throat thereof and an air duct is connected to an annular passage into which said holes extend.
AUGUSTUS HASBROUCK.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 860,668 Jaeger July 23, 1907 1,011,313 Bretherick Dec. 12, 1911 1,517,329 Weiss et al. Dec. 2, 1924 1,813,747 Kirgan July 7, 1931 1,834,959 May Dec, 8, 1931 1,858,071 Chester May 10, 1932 2,083,184 Anderson June 8, 1937 2,143,100 Anderson Jan. 10, 1939 2,156,405 Smoot May 2, 1939 2,188,547 Anderson Jan. 30, 1940 2,357,527 Lundquist Sept. 5, 1944 2,405,282 Birmann Aug. 6, 1946 FOREIGN PATENTS Number Country D te 346,968 Great Britain Sept. 30, 1930 576,643 Germany May 27, 1933
US550655A 1944-08-22 1944-08-22 Supercharger with controllable inlet Expired - Lifetime US2431398A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2588198A (en) * 1948-10-13 1952-03-04 B & R Mfg Company Litter control for vacuum cleaners
US2684634A (en) * 1946-04-16 1954-07-27 Sfindex Guiding means for liquids and gases
US2702157A (en) * 1949-09-28 1955-02-15 Edward A Stalker Compressor employing radial diffusion
US2923526A (en) * 1955-03-31 1960-02-02 Gen Electric Turbine
US3019963A (en) * 1955-07-08 1962-02-06 Eck Bruno Christian Radial blower for gases with high dust content
US3071345A (en) * 1961-04-27 1963-01-01 United Aircraft Corp Throttle valve
US3160112A (en) * 1958-07-31 1964-12-08 Westinghouse Electric Corp Check valve and application thereof
US3227418A (en) * 1963-11-04 1966-01-04 Gen Electric Variable clearance seal
US3481145A (en) * 1966-11-02 1969-12-02 Plessey Co Ltd Engine-starting gas turbine systems
FR2468752A1 (en) * 1979-10-31 1981-05-08 Messerschmitt Boelkow Blohm DEVICE FOR MOUNTING AND DRIVING A VALVE COMMANDING THE TRANSVERSE SECTION FOR THE FLOW OF HOT GASES, PARTICULARLY GASES RICH IN FUEL ENTERING THE COMBUSTION CHAMBER OF STATOREACTORS
US4808068A (en) * 1986-10-28 1989-02-28 Intertherm Investments, Inc. Blower unloading device
US5161941A (en) * 1990-08-28 1992-11-10 Sinko Kogyo, Co, Ltd. Actuator assembly for controlling inlet air flow to centrifugal fans
US5214920A (en) * 1990-11-27 1993-06-01 Leavesley Malcolm G Turbocharger apparatus
WO2002044527A1 (en) * 2000-11-30 2002-06-06 Honeywell Garrett Sa Variable geometry turbocharger with sliding piston
US20060037317A1 (en) * 2002-11-25 2006-02-23 Leavesley Malcolm G Variable turbocharger apparatus with bypass
US20110173973A1 (en) * 2010-01-20 2011-07-21 International Engine Intellectrual Property Company, LLC Turbine inlet flow modulator
EP2626573A1 (en) * 2012-02-09 2013-08-14 Lg Electronics Inc. Centrifugal compressor
US20190264603A1 (en) * 2016-09-14 2019-08-29 Cpt Group Gmbh Turbocharger For An Internal Combustion Engine

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US860668A (en) * 1903-03-09 1907-07-23 Int Steam Pump Co Rotary pump.
US1011313A (en) * 1911-01-17 1911-12-12 Clarence O Bretherick Current-inducing apparatus.
US1517329A (en) * 1921-08-29 1924-12-02 Weiss Leo Centrifugal fan or blower
GB346968A (en) * 1930-03-28 1931-04-23 Holden & Brooke Ltd Improvements relating to the regulation of centrifugal pumps
US1813747A (en) * 1928-12-20 1931-07-07 Ingersoll Rand Co Centrifugal pump
US1834959A (en) * 1929-02-14 1931-12-08 Comb Eer Inc Blower
US1858071A (en) * 1931-10-20 1932-05-10 Chester Thomas Centrifugal apparatus
DE576643C (en) * 1933-05-27 Demag Akt Ges Multi-stage centrifugal compressor
US2083184A (en) * 1936-03-23 1937-06-08 American Blower Corp Fan
US2143100A (en) * 1937-04-19 1939-01-10 American Blower Corp Blower
US2156405A (en) * 1935-12-20 1939-05-02 Theophilus H Smoot Oil burner
US2188547A (en) * 1940-01-30 Dust collector
US2357527A (en) * 1943-01-14 1944-09-05 Wright Aeronautical Corp Impeller throttle
US2405282A (en) * 1938-02-02 1946-08-06 Fed Reserve Bank Variable ratio compressor

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2188547A (en) * 1940-01-30 Dust collector
DE576643C (en) * 1933-05-27 Demag Akt Ges Multi-stage centrifugal compressor
US860668A (en) * 1903-03-09 1907-07-23 Int Steam Pump Co Rotary pump.
US1011313A (en) * 1911-01-17 1911-12-12 Clarence O Bretherick Current-inducing apparatus.
US1517329A (en) * 1921-08-29 1924-12-02 Weiss Leo Centrifugal fan or blower
US1813747A (en) * 1928-12-20 1931-07-07 Ingersoll Rand Co Centrifugal pump
US1834959A (en) * 1929-02-14 1931-12-08 Comb Eer Inc Blower
GB346968A (en) * 1930-03-28 1931-04-23 Holden & Brooke Ltd Improvements relating to the regulation of centrifugal pumps
US1858071A (en) * 1931-10-20 1932-05-10 Chester Thomas Centrifugal apparatus
US2156405A (en) * 1935-12-20 1939-05-02 Theophilus H Smoot Oil burner
US2083184A (en) * 1936-03-23 1937-06-08 American Blower Corp Fan
US2143100A (en) * 1937-04-19 1939-01-10 American Blower Corp Blower
US2405282A (en) * 1938-02-02 1946-08-06 Fed Reserve Bank Variable ratio compressor
US2357527A (en) * 1943-01-14 1944-09-05 Wright Aeronautical Corp Impeller throttle

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684634A (en) * 1946-04-16 1954-07-27 Sfindex Guiding means for liquids and gases
US2588198A (en) * 1948-10-13 1952-03-04 B & R Mfg Company Litter control for vacuum cleaners
US2702157A (en) * 1949-09-28 1955-02-15 Edward A Stalker Compressor employing radial diffusion
US2923526A (en) * 1955-03-31 1960-02-02 Gen Electric Turbine
US3019963A (en) * 1955-07-08 1962-02-06 Eck Bruno Christian Radial blower for gases with high dust content
US3160112A (en) * 1958-07-31 1964-12-08 Westinghouse Electric Corp Check valve and application thereof
US3071345A (en) * 1961-04-27 1963-01-01 United Aircraft Corp Throttle valve
US3227418A (en) * 1963-11-04 1966-01-04 Gen Electric Variable clearance seal
US3481145A (en) * 1966-11-02 1969-12-02 Plessey Co Ltd Engine-starting gas turbine systems
FR2468752A1 (en) * 1979-10-31 1981-05-08 Messerschmitt Boelkow Blohm DEVICE FOR MOUNTING AND DRIVING A VALVE COMMANDING THE TRANSVERSE SECTION FOR THE FLOW OF HOT GASES, PARTICULARLY GASES RICH IN FUEL ENTERING THE COMBUSTION CHAMBER OF STATOREACTORS
US4353389A (en) * 1979-10-31 1982-10-12 Messerschmitt-Bolkow-Blohm G.M.B.H. Hot gas valve
US4808068A (en) * 1986-10-28 1989-02-28 Intertherm Investments, Inc. Blower unloading device
US5161941A (en) * 1990-08-28 1992-11-10 Sinko Kogyo, Co, Ltd. Actuator assembly for controlling inlet air flow to centrifugal fans
US5214920A (en) * 1990-11-27 1993-06-01 Leavesley Malcolm G Turbocharger apparatus
WO2002044527A1 (en) * 2000-11-30 2002-06-06 Honeywell Garrett Sa Variable geometry turbocharger with sliding piston
US20040025504A1 (en) * 2000-11-30 2004-02-12 Perrin Jean-Luc Hubert Variable geometry turbocharger with sliding piston
US7024855B2 (en) 2000-11-30 2006-04-11 Honeywell International, Inc. Variable geometry turbocharger with sliding piston
KR100737377B1 (en) 2000-11-30 2007-07-09 허니웰 가렛트 에스아 Variable geometry turbocharger with sliding piston
CN100340742C (en) * 2000-11-30 2007-10-03 霍尼韦尔加勒特股份有限公司 Variable geometry turbocharger with sliding piston
US20060037317A1 (en) * 2002-11-25 2006-02-23 Leavesley Malcolm G Variable turbocharger apparatus with bypass
US7272929B2 (en) * 2002-11-25 2007-09-25 Malcolm George Leavesley Variable turbocharger apparatus with bypass
US20110173973A1 (en) * 2010-01-20 2011-07-21 International Engine Intellectrual Property Company, LLC Turbine inlet flow modulator
EP2626573A1 (en) * 2012-02-09 2013-08-14 Lg Electronics Inc. Centrifugal compressor
US20190264603A1 (en) * 2016-09-14 2019-08-29 Cpt Group Gmbh Turbocharger For An Internal Combustion Engine
US10883418B2 (en) * 2016-09-14 2021-01-05 Cpt Group Gmbh Turbocharger for an internal combustion engine

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