US2367499A - Load and altitude control - Google Patents
Load and altitude control Download PDFInfo
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- US2367499A US2367499A US474017A US47401743A US2367499A US 2367499 A US2367499 A US 2367499A US 474017 A US474017 A US 474017A US 47401743 A US47401743 A US 47401743A US 2367499 A US2367499 A US 2367499A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M9/00—Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position
- F02M9/10—Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position having valves, or like controls, of elastic-wall type for controlling the passage, or for varying cross-sectional area, of fuel-air mixing chambers or of the entry passage
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M17/00—Carburettors having pertinent characteristics not provided for in, or of interest apart from, the apparatus of preceding main groups F02M1/00 - F02M15/00
- F02M17/02—Floatless carburettors
- F02M17/04—Floatless carburettors having fuel inlet valve controlled by diaphragm
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M7/00—Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
- F02M7/12—Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
- F02M7/18—Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice
- F02M7/20—Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice operated automatically, e.g. dependent on altitude
Definitions
- the object of this invention is to improve the art of carburetion and particularly to improve the measurement of fuel responsive to airflow by means of a venturi in the air stream.
- the principles in my invention are applied, to a device designed to deliver the correct amount of fuel to an engine; however, the application of this invention is not limited to this one device.
- One object of my invention is to correct the metering characteristics of a fixed or variable venturi, to provide a device which automatically corrects the actual curve of pressure drop versus air flow to the theoretically correct curve for that venturi taking into account the air density of the entering air and the changes in density at the throat of the venturi due to the elasticity of air at high air velocities.
- the diagrammatic sketch shows a conventional pressure type carburetor of the variable venturi type with the improvements mentioned above incorporated therein.
- the drawing shows diagrammatically the essential elements of my invention.
- i3 is the metering channel casting containing the passages l4, I5 and i6 and 5
- the passages l5 and I6 communicate with the throat of the variable venturi.
- Passage l4 communicates through a pipe 32 with the chamber 25 in the entrance to which is located a contoured valve 23.
- Two springs 29 and 30 maintain the valve 23 in the position shown.
- a diaphragm 21 is connected to the valve 23 and is supported by the two springs 29 and 30. Diaphragm 21 thus separates the chamber 25 from the chamber 28.
- Chamber 28 communicates through a pipe 34 with the annular chamber 48 which communicates with the air entrance III at a large number of openings so as to give a fair average of the pressure.
- This annular chamber 48 is also connected through a pipe 3
- has a restricted communication 19 with chamber 49.
- Chamber 49 also communicates through pipe 22 with a chamber 50 located on the right hand side of a diaphragm 20.
- Chamber I8 is located on the left hand side of the diaphragm 20 and communicates through a restricted opening l9 and a, pipe ll with the channel 5
- the chamber l8 also communicates through the pipe 35 with a chamber 52, which chamber communicates with a chamber 53 through a restricted opening, this communication being controlled by a metering valve 54 which slides through an opening in the partition 40 between the two chambers 52 and 53.
- the chamber 53 contains a barometric element 84 and a spring 55 and communicates through the pipe 56 with the annular chamber 48 in the air entrance Ill.
- the end of valve 54 is subjected to atmospheric pressure by means of the chamber 51, which is connected to the pipe 56, that is to say to the atmospheric pressure existing in the air entrance I.
- the pressure differential across diaphragm 20 is transmitted to a second diaphragm 60 through a pin 46.
- This pressure difierential causes a valve 6
- the size of the restricted opening through the valve 65 is controlled by means of a lever 66, link 62 and lever 63, which is attached to the Venturi throttle element ll.
- Fuel pressure on the discharge side of valve 65 is applied to a chamber 11 through a pipe 68.
- Fuel from valve 65 is delivered to a balanced exit valve 69 through pipe 61.
- the exit valve 59 is attached to a diaphragm 10.
- Chamber I2 is balanced to inlet pressure through pipe 14.
- diaphragm 60 may be affected by equal areas on either side pin 18 equal in diameter to pin 46 is subjected to fuel pressure in chamber 16 through a pipe equal to that in chamber 11.
- the pressure difference across diaphragm 20 can be adjusted so as to be the theoretically correct pressure differential for the particular venturi and air flow because chamber I8 can be corrected for changes in density at the air entrance, and chamber 50 can be corrected for changes in density at the Venturi restriction.
- Valve 54 is actuated by a set of bellows 84 responsive to density changes at the vent ring 48 and modifies the pressure in chamber [8 to compensate for changes in density at the inlet of the carburetor.
- Valve 23 is actuated by diaphragm 21 and modifies the pressure in chamber 50 for changes in density at the air metering orifice l6. Diaphragm 21 is moved by a differential pressure between the air entrance pressure in annular chamber 48 and the pressure in the throat of the variable Venturi as transmitted through the opening 15.
- variable opening through the valve 65 varies with the throttle opening by means of the linkage 63, 62, 65.
- linkage 63, 62, 65 there is a definite fuel restriction through the valve 65.
- a given pressure drop across the valve 65 at a given position therefore, corresponds to a definite fuel flow.
- the outlet through pipe 61 creates in chamber 18 a definite pressure below the pressure in the fuel entrance 63 because the pipe 14 transmits maximum fuel pressure to the left hand side of diaphragm 10.
- air flow is balanced against fuel flow and the air flow is corrected for both altitude and for velocity of air flow through the venturi.
- a carburetor having an air entrance a variable Venturi throttle therein, a fuel entrance, fuel metering means therefor comprising an air chamber, a moving wall therein dividing said air chamber into two, a passage connecting the first half of said air chamber with the throat of said venturi, a second passage connecting the second half of said air chamber with the said air entrance, a second air chamber, a second moving wall therein dividing said second air chamber into two halves, a pipe connecting the first half of said chamber with the air entrance so as to establish air entrance pressure therein at all times, a pipe connecting the second half of said second chamber with the throat of said variable Venturi, a third air chamber communicating with said second chamber through a restricted opening, a valve means connected to said second moving wall, said valve being adapted to control the said restricted communication, said second passage connecting said third air chamber with the air entrance through a restricted opening and with the said second half of said first air chamber so as to modify the pressure difference acting on said first mentioned moving wall in response to changes in the depression in the throat of said vent
- a carburetor as set forth in claim 1 in which there is a 4th air pressure regulating chamber, a restricted communication between said 4th air chamber, and the first half of said first air chamber, barometric means located in said 4th air chamber, a valve connected thereto, said valve being adapted to control said restricted connection, an unrestricted passage connecting said 4th chamber with the pressure existing in said air entrance.
- a carburetor as set forth in claim 1 in which there is a 4th air pressure regulating chamber, a restricted communication between said 4th air chamber and the first half of said first air chamber, barometric means located in said 4th air chamber, a valve connected thereto, said valve being adapted to control said restricted connection, an unrestricted passage connecting said 4th air chamber with the pressure existing in said air entrance, means for maintaining a constant pressure drop between the pressure of the entering fuel and the pressure of the fuel as it issues from said metering means into said air passage of said carburetor including a 2nd fuel chamber, a 4th moving wall therein dividing said fuel chamher into two, a passage connecting the 1st half of said chamber with the fuel entrance, a passage connecting the restricted outlet of said lst fuel chamber with the second half of said 2nd fuel chamber, an outlet therefrom, a valve in said outlet connected to said 4th moving wall.
- a carburetor having an air entrance, a variable Venturi throttle therein, a fuel entrance, fuel metering means therefore comprising a chamber, a moving wall therein dividing said chamber into two, a passage connecting the first half of said chamber with the throat of said variable venturi, a second passage connecting the second half of said chamber with said air entrance so as to establish air entrance pressure therein at all times, a second chamber, a second moving wall therein dividing said chamber into two halves, a pipe connecting the first half of said chamber with the air entrance, a pipe connecting second half of said second chamber with throat of said variable venturi, a third chamber communicating with said second chamber through a restricted opening, valve means connected to said second moving wall, said valve being adapted to control the area of said restricted communication, said second passage connecting said third chamber with the air entrance through a restricted opening and with the said second half of said first chamber which'oommunicates with the air entrance so as to modify the pressure difference acting on said first mentioned moving wallin response to changes in the depression in' the throat of said variable venturi
- said metering means into said air passage of said carburetor, including a 2nd fuel chamber, a 4th moving wall therein dividing said able venturi, a third air chamber communicating with said second chamber through a restricted opening, a valve means connected to said second moving wall, said valve beingadapted to control the said restricted communication, a passage connecting said third air chamber with the air entrance through a restricted opening and with said second half of said first air chamber which ,communicates with air entrance so as to modify the pressure difference acting on said first mentioned moving wall in response to changes in the depression 'in the throat of said venturi, a fuel fuel chamber into two, a passage connecting the 1st half of said chamber with the fuel entrance. a passage connecting restricted outlet of said 1st fuel chamber,.with the 2nd half of said 2nd fuel chamber, an outlet therefrom, .a valve in said outlet connected to said-1th moving wall.
- a carburetor having an air entrance, at venturi therein, a fuel entrance, fuel metering means therefor comprising an air chamber, moving wall therein dividing said air chamber into two, a passage connecting the first half of said air chamber'with the throat of said venturi, a passage connecting the second half of said airchamber with the said air entrance, a second air chamber, a second moving wall therein dividing said second air chamber into two halves, a pipe connecting the first half of said chamber with the air entrance, a pipe connecting the .second half of said second chamber with the throat of said varichamber, a 3rd moving wall therein dividing said fuel chamber into two, a valve admitting fuel under pressure to the lsthalf of said chamber, a restricted outlet from said fuel chamber, a
- a carburetor as set forth in claim 1 in which there is a fourth air pressure regulating chamber, a restricted communication between said fourth air chamber and the first half of said first air chamber, barometric means located in said fourth air chamber, a valve connected thereto, said valve 40 being adapted to "control said restricted connection, an unrestricted passage connecting said fourth air chamber with the pressure existing in said air entrance, means for maintaining a constant pressure drop between the press'ureof the entering fuel and the pressure of the fuel as it issues from said metering means into said air passage of said carburetor including a second fuel chamber, a fourth moving wall therein dividing said fuel chamber into two halves, a passage connecting the first half of said chamber with the fuel entrance, a passage connecting the restricted outlet of said first fuel chamber with the second half of said second fuel chamber, an outlet therefrom, a. valve in said outlet connected to said fourth moving wall.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
Description
Jan. 16, 1945. HQLLEY, JR 2,367,499
LOAD AND ALTITUDE CONTROL Filed Jan. 29, 1943 INVENTOR.
?atented Jan. 16, 1945 2,367,499 LOAD AND ALTITUDE CONTROL George M. Holley, Jr., Grosse Pointe Woods, Mich, assignor to George M. Holley and Earl Holley Application January 29, 1943, Serial No. 474,017
7 Claims.
The object of this invention is to improve the art of carburetion and particularly to improve the measurement of fuel responsive to airflow by means of a venturi in the air stream. The principles in my invention are applied, to a device designed to deliver the correct amount of fuel to an engine; however, the application of this invention is not limited to this one device.
There is a tendency, at high airflow, for the density of the air at the throat of a venturi to fall to such a degree that it introduces an error in the metering characteristic of the venturi. Thus, when due to the elasticity of the air, the density falls at the throat of the venturi at high velocity, the venturi will no longer follow the theoretical square root curve called for in the equation V=c\/2gh where V is the velocity and h the drop in pressure due to the velocity and c is a constant.
One object of my invention is to correct the metering characteristics of a fixed or variable venturi, to provide a device which automatically corrects the actual curve of pressure drop versus air flow to the theoretically correct curve for that venturi taking into account the air density of the entering air and the changes in density at the throat of the venturi due to the elasticity of air at high air velocities.
In an attempt to avoid the necessity of making this correction for flow through the air venturi with fixed venturi there has been a tendency to make fixed venturi so large that they are not responsive to low airflows.
The diagrammatic sketch shows a conventional pressure type carburetor of the variable venturi type with the improvements mentioned above incorporated therein.
The drawing shows diagrammatically the essential elements of my invention. In the drawing is the air entrance H and I2 and the throttles which form the walls of the variable venturi. i3 is the metering channel casting containing the passages l4, I5 and i6 and 5|. The passages l5 and I6 communicate with the throat of the variable venturi. Passage l4 communicates through a pipe 32 with the chamber 25 in the entrance to which is located a contoured valve 23. Two springs 29 and 30 maintain the valve 23 in the position shown. A diaphragm 21 is connected to the valve 23 and is supported by the two springs 29 and 30. Diaphragm 21 thus separates the chamber 25 from the chamber 28. Chamber 28 communicates through a pipe 34 with the annular chamber 48 which communicates with the air entrance III at a large number of openings so as to give a fair average of the pressure. This annular chamber 48 is also connected through a pipe 3| with a chamber 49 located in the left hand side of chamber 25 and the pressure in this chamber 49 is determined by the fiow of air from annular chamber 48 to the chamber 25 and hence is determined by the position of the valve 23. It will be noted that the pipe 3| has a restricted communication 19 with chamber 49. Chamber 49 also communicates through pipe 22 with a chamber 50 located on the right hand side of a diaphragm 20. Chamber I8 is located on the left hand side of the diaphragm 20 and communicates through a restricted opening l9 and a, pipe ll with the channel 5|.
The chamber l8 also communicates through the pipe 35 with a chamber 52, which chamber communicates with a chamber 53 through a restricted opening, this communication being controlled by a metering valve 54 which slides through an opening in the partition 40 between the two chambers 52 and 53. The chamber 53 contains a barometric element 84 and a spring 55 and communicates through the pipe 56 with the annular chamber 48 in the air entrance Ill. The end of valve 54 is subjected to atmospheric pressure by means of the chamber 51, which is connected to the pipe 56, that is to say to the atmospheric pressure existing in the air entrance I.
The pressure differential across diaphragm 20 is transmitted to a second diaphragm 60 through a pin 46. This pressure difierential causes a valve 6| to open the fuel entrance from a passage 63 into a chamber 62 and from there through a pipe 64 to a variable restriction or valve 65. The size of the restricted opening through the valve 65 is controlled by means of a lever 66, link 62 and lever 63, which is attached to the Venturi throttle element ll. Fuel pressure on the discharge side of valve 65 is applied to a chamber 11 through a pipe 68. Fuel from valve 65 is delivered to a balanced exit valve 69 through pipe 61. The exit valve 59 is attached to a diaphragm 10. Chamber I2 is balanced to inlet pressure through pipe 14. By the proper calibration of a, spring I I which engages with diaphragm lll pressure equal to the pressure in the fuel entrance less a constant is maintained in chamber 88 so that there is always a constant pressure drop across the entire fuel system,- hence the pressure drop across the valve 65 will change with air flow at any given throttle opening. From the exit valve, fuel is delivered to the engine through pipe I3 and 41. The differential pressure acting on the diaphragm 60 must always equal the pressure acting on the diaphrag'm 20. Whenever there is an unbalance, fuel valve 6| is either opened or closed and hence the fuel fiow varies automatically with the air fiow.
In order that diaphragm 60 may be affected by equal areas on either side pin 18 equal in diameter to pin 46 is subjected to fuel pressure in chamber 16 through a pipe equal to that in chamber 11.
It will be seen from studying the diagrammatic sketch that a group of parts-valve 23, springs 29, 30, diaphragm 2|-together with passages 34, 32 and 22 apply a corrective pressure to chamber 50. The amount of this correction is determined by differential pressure between Venturi and the vent ring 48 so that this valve compensates for changes in density at the nozzle bar. A group of partsvalve 54, spring 55, aneroid bellows 84-and passages 56 and 35 modify the pressure in chamber l8 for changes in density at the inlet of the venturi. This valve 54 at high altitudes admits more air to chamber 18 and raises the pressure therein.
The pressure difference across diaphragm 20 can be adjusted so as to be the theoretically correct pressure differential for the particular venturi and air flow because chamber I8 can be corrected for changes in density at the air entrance, and chamber 50 can be corrected for changes in density at the Venturi restriction.
It is the differential pressure between the annular chamber 48 and I5 which responds to Venturi suction which causes the change in density at I5, therefore, since valve 23 is subject to this pressure, it can be made to properly correct the pressures. Exit valve 69 and diaphragm 10 control the fuel pressure drop through the entire fuel meterin system.
Operation Valve 54 is actuated by a set of bellows 84 responsive to density changes at the vent ring 48 and modifies the pressure in chamber [8 to compensate for changes in density at the inlet of the carburetor. Valve 23 is actuated by diaphragm 21 and modifies the pressure in chamber 50 for changes in density at the air metering orifice l6. Diaphragm 21 is moved by a differential pressure between the air entrance pressure in annular chamber 48 and the pressure in the throat of the variable Venturi as transmitted through the opening 15.
The variable opening through the valve 65 varies with the throttle opening by means of the linkage 63, 62, 65. Hence, at any given air venturi opening between I I and I2, there is a definite fuel restriction through the valve 65. A given pressure drop across the valve 65 at a given position therefore, corresponds to a definite fuel flow.
The outlet through pipe 61 creates in chamber 18 a definite pressure below the pressure in the fuel entrance 63 because the pipe 14 transmits maximum fuel pressure to the left hand side of diaphragm 10.
Hence, air flow is balanced against fuel flow and the air flow is corrected for both altitude and for velocity of air flow through the venturi.
What I claim is:
l. A carburetor having an air entrance a variable Venturi throttle therein, a fuel entrance, fuel metering means therefor comprising an air chamber, a moving wall therein dividing said air chamber into two, a passage connecting the first half of said air chamber with the throat of said venturi, a second passage connecting the second half of said air chamber with the said air entrance, a second air chamber, a second moving wall therein dividing said second air chamber into two halves, a pipe connecting the first half of said chamber with the air entrance so as to establish air entrance pressure therein at all times, a pipe connecting the second half of said second chamber with the throat of said variable Venturi, a third air chamber communicating with said second chamber through a restricted opening, a valve means connected to said second moving wall, said valve being adapted to control the said restricted communication, said second passage connecting said third air chamber with the air entrance through a restricted opening and with the said second half of said first air chamber so as to modify the pressure difference acting on said first mentioned moving wall in response to changes in the depression in the throat of said venturi, a fuel chamber, a 3rd moving wall therein dividing said fuel chamber into two, a valve admitting fuel under pressure to the 1st half of said chamber, a restricted outlet from said fuel chamber, a control valve therefor, adapted to be opened by said variable Venturi throttle. a passage connecting the 2nd half of said fuel chamber with the downstream side of said restriction, said lst-3rd moving walls being connected together and adapted to control said fuel admission valve so as to balance fuel flow against air flow.
2. A carburetor as set forth in claim 1 in which there is a 4th air pressure regulating chamber, a restricted communication between said 4th air chamber, and the first half of said first air chamber, barometric means located in said 4th air chamber, a valve connected thereto, said valve being adapted to control said restricted connection, an unrestricted passage connecting said 4th chamber with the pressure existing in said air entrance.
3. A carburetor as set forth in claim 1 in which there is a 4th air pressure regulating chamber, a restricted communication between said 4th air chamber and the first half of said first air chamber, barometric means located in said 4th air chamber, a valve connected thereto, said valve being adapted to control said restricted connection, an unrestricted passage connecting said 4th air chamber with the pressure existing in said air entrance, means for maintaining a constant pressure drop between the pressure of the entering fuel and the pressure of the fuel as it issues from said metering means into said air passage of said carburetor including a 2nd fuel chamber, a 4th moving wall therein dividing said fuel chamher into two, a passage connecting the 1st half of said chamber with the fuel entrance, a passage connecting the restricted outlet of said lst fuel chamber with the second half of said 2nd fuel chamber, an outlet therefrom, a valve in said outlet connected to said 4th moving wall.
4. A carburetor having an air entrance, a variable Venturi throttle therein, a fuel entrance, fuel metering means therefore comprising a chamber, a moving wall therein dividing said chamber into two, a passage connecting the first half of said chamber with the throat of said variable venturi, a second passage connecting the second half of said chamber with said air entrance so as to establish air entrance pressure therein at all times, a second chamber, a second moving wall therein dividing said chamber into two halves, a pipe connecting the first half of said chamber with the air entrance, a pipe connecting second half of said second chamber with throat of said variable venturi, a third chamber communicating with said second chamber through a restricted opening, valve means connected to said second moving wall, said valve being adapted to control the area of said restricted communication, said second passage connecting said third chamber with the air entrance through a restricted opening and with the said second half of said first chamber which'oommunicates with the air entrance so as to modify the pressure difference acting on said first mentioned moving wallin response to changes in the depression in' the throat of said variable venturi, a fourth chamber, a third moving wall therefor dividing said fourth chamber into two halves, fuel metering means connected to said third moving wall and to said first mentioned moving wall, said fuel metering means being adapted to admit fuel 'to create a pressure difference on said third moving wall so as to balance said first mentioned moving wall, arestricted outlet from the fuel chamber,
in said air entrance, means for maintaining con-.
stant pressure drop between the pressure of the entering fuel and the pressure of the fuel as it issuesfrom. said metering means into said air passage of said carburetor, including a 2nd fuel chamber, a 4th moving wall therein dividing said able venturi, a third air chamber communicating with said second chamber through a restricted opening, a valve means connected to said second moving wall, said valve beingadapted to control the said restricted communication, a passage connecting said third air chamber with the air entrance through a restricted opening and with said second half of said first air chamber which ,communicates with air entrance so as to modify the pressure difference acting on said first mentioned moving wall in response to changes in the depression 'in the throat of said venturi, a fuel fuel chamber into two, a passage connecting the 1st half of said chamber with the fuel entrance. a passage connecting restricted outlet of said 1st fuel chamber,.with the 2nd half of said 2nd fuel chamber, an outlet therefrom, .a valve in said outlet connected to said-1th moving wall.
6. A carburetor having an air entrance, at venturi therein, a fuel entrance, fuel metering means therefor comprising an air chamber, moving wall therein dividing said air chamber into two, a passage connecting the first half of said air chamber'with the throat of said venturi, a passage connecting the second half of said airchamber with the said air entrance, a second air chamber, a second moving wall therein dividing said second air chamber into two halves, a pipe connecting the first half of said chamber with the air entrance, a pipe connecting the .second half of said second chamber with the throat of said varichamber, a 3rd moving wall therein dividing said fuel chamber into two, a valve admitting fuel under pressure to the lsthalf of said chamber, a restricted outlet from said fuel chamber, a
passage connecting the 2nd half of said fuel chamber with the downstream side of said restriction, said 1st and 3rd moving walls being connected together and adapted to control said fuel admission valve so as to balance fuel flow against air fiow, means for maintaining a constant pressure drop between the pressure of the entering fuel and the pressure of the fuel as it issues from said metering means into said air passage of said carburetor including a 2nd fuel chamber, a 4th moving wall therein dividing said fuel chamber into two, a passage connecting the 1st half of said chamber with the fuel entrance, a passage connecting the restricted outlet of said 1st fuel chamber with the, 2nd half of said 2nd fuel chamber, an outlet therefrom, a valve in said outlet connected to said 4th moving wall.
7. A carburetor as set forth in claim 1 in which there is a fourth air pressure regulating chamber, a restricted communication between said fourth air chamber and the first half of said first air chamber, barometric means located in said fourth air chamber, a valve connected thereto, said valve 40 being adapted to "control said restricted connection, an unrestricted passage connecting said fourth air chamber with the pressure existing in said air entrance, means for maintaining a constant pressure drop between the press'ureof the entering fuel and the pressure of the fuel as it issues from said metering means into said air passage of said carburetor including a second fuel chamber, a fourth moving wall therein dividing said fuel chamber into two halves, a passage connecting the first half of said chamber with the fuel entrance, a passage connecting the restricted outlet of said first fuel chamber with the second half of said second fuel chamber, an outlet therefrom, a. valve in said outlet connected to said fourth moving wall.
GEORGE M. HOILEY, Jn.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US474017A US2367499A (en) | 1943-01-29 | 1943-01-29 | Load and altitude control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US474017A US2367499A (en) | 1943-01-29 | 1943-01-29 | Load and altitude control |
Publications (1)
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US2367499A true US2367499A (en) | 1945-01-16 |
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ID=23881876
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Application Number | Title | Priority Date | Filing Date |
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US474017A Expired - Lifetime US2367499A (en) | 1943-01-29 | 1943-01-29 | Load and altitude control |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2465535A (en) * | 1945-03-08 | 1949-03-29 | George M Holley | Aircraft carburetor |
US2465550A (en) * | 1946-02-18 | 1949-03-29 | George M Holley | Aircraft carburetor |
US2529100A (en) * | 1946-04-27 | 1950-11-07 | George M Holley | Aircraft carburetor |
US2569024A (en) * | 1945-05-07 | 1951-09-25 | Bendix Aviat Corp | Charge forming device |
US2633704A (en) * | 1947-08-14 | 1953-04-07 | Chrysler Corp | Fuel-air ratio regulator for gas turbine power plants |
US2699157A (en) * | 1950-12-30 | 1955-01-11 | Heftler Maurice Ben | Coasting economizer |
US3987132A (en) * | 1974-07-03 | 1976-10-19 | Dresser Industries, Inc. | Fluid flow regulation |
-
1943
- 1943-01-29 US US474017A patent/US2367499A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2465535A (en) * | 1945-03-08 | 1949-03-29 | George M Holley | Aircraft carburetor |
US2569024A (en) * | 1945-05-07 | 1951-09-25 | Bendix Aviat Corp | Charge forming device |
US2465550A (en) * | 1946-02-18 | 1949-03-29 | George M Holley | Aircraft carburetor |
US2529100A (en) * | 1946-04-27 | 1950-11-07 | George M Holley | Aircraft carburetor |
US2633704A (en) * | 1947-08-14 | 1953-04-07 | Chrysler Corp | Fuel-air ratio regulator for gas turbine power plants |
US2699157A (en) * | 1950-12-30 | 1955-01-11 | Heftler Maurice Ben | Coasting economizer |
US3987132A (en) * | 1974-07-03 | 1976-10-19 | Dresser Industries, Inc. | Fluid flow regulation |
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