US2223381A - Carburetor - Google Patents

Carburetor Download PDF

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Publication number
US2223381A
US2223381A US126133A US12613337A US2223381A US 2223381 A US2223381 A US 2223381A US 126133 A US126133 A US 126133A US 12613337 A US12613337 A US 12613337A US 2223381 A US2223381 A US 2223381A
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Prior art keywords
fuel
pressure
conduit
valve
nozzle
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US126133A
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Frank C Mock
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Frank C Mock
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    • 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
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • 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
    • F02M2700/43Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
    • F02M2700/4397Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air or fuel are admitted in the mixture conduit by means other than vacuum or an acceleration pump
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/02Airplane
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/51Carburetors with supercharging blowers

Description

F. C. MOCK Dec. 3, 1940.
CARBURETOR Filed Feb. 1'7, 1937 INVENTOR. FRA NK ct/wow Q @WS ATTORNEY Patented Dec. 3, 1940 UNITED STATES PATENT OFFICE 16 Claims.
This invention relates to charge forming devices and more particularly to devices for form,- ing a combustible mixture of air and fuel externally of an internal combustion engine and for supplying such mixture to the engine cylinders.
Charge forming devices of the type heretofore commonly used have supplied fuel under a substantially constant head, as by means of a float chamber, to a nozzle opening into a Venturi air passage so that fuel is aspirated from the nozzle by the suction produced in the venturi. In these devices the fuel in the nozzle is, at times, subjected to a very high degree of suction thereby causing boiling of the fuel which interferes with proper metering thereof.
It is one of the objects of the present invention to provide a charge forming device in which there is substantially no tendency for the fuel to boil, and to attain this object the device is so constructed that the fuel nozzle is not subjected at any time to the extremes of suction encountered in an ordinary carburetor. In addition the fuel is supplied under positive pressure which may always be equal to or in excess of atmospheric.
Another object of the invention is to provide a charge'forming device in which icing is prevented. For this purpose the fuel nozzle is preferably arranged to discharge into the air stream at a point posterior to the throttle and into a part of the manifold which is relatively warm. 'Ihus there is no chance for ice to collect on the throttle or on relatively cold parts of the manifold.
A further object of the invention relates to fuel metering and fuel control to maintain the fuel-air ratio at the optimum value for all operating conditions.
Other objects, advantages and novel features f the invention will be apparent from the following description of the accompanying drawing, in which the single gure is a diagrammatic view of a charge `forming device embodying the invention.
The device illustrated includes an air conduit In shown with a right angle bend therein and having a venturi I2. One end of the conduit IIJ may be open as shown to form a scoop tube or it may, if desired, be connected to a supercharger. The opposite end discharges into the inlet of a supercharger I4 which supplies the mixture to a manifold I6 connected to the engine cylinders, not show n.
Alongside of the conduit I0 there is a smaller conduit I8 terminating in a nozzle-like portion 20 substantially at the Venturi throat. The conduits I0 and I8 are controlled by throttle valves 22 and 24 interconnected by a link 26 in such a manner that when one is, open the other is closed. Both throttle valves are controlled smultaneously by a link 28 connected to the valve 22 and extending to any convenient point for easy access by an operator.
Fuel is supplied .by an engine driven pump 30 connected by a pipe 32 to any convenient source of fuel and having a by-pass from its outlet to its inlet controlled by a pressure responsive valve 34 to maintain the outlet pressure substantially constant. 'I'he pump discharges into a fuel chamber 36 which communicates past a control valve 38 with a diaphragm chamber 48 and the latter communicates through a passage 42 with a fuel nozzle 46. The diaphragm chamber 40 is divided from a chamber ,48 which communicates with atmosphere through a vent 50 by a diaphragm 52 which is connected to the stem 54 0f the valve 38. A similar `diaphragm 56 also connected to the valve stem 54 serves to separate two chambers 58 and 60, the former of which is separated from the chamber 48 by a packing diaphragm 62 and the latter of which communicates with atmosphere through a vent 64. Preferably a light spring 66 is mounted in the chamber 60 and acts on the valve stem 54 to urge the valve open.
The chamber 58 is connected through passages 68 and 10, restricted orice I2 and passage 'I4 'to the conduit I8 so that the lower surface of the diaphragm B issubject to the suction prevailing in this conduit modified by certain other factors to be described later. The passage 'I4 communicates through a restricted orifice 16 and through a passage 'I8 controlled by a manually adjustable plug valv 88 with a chamber 82 having an atmospheric vent 84 slightly larger than the orice 1B. 'I'he passage I4 also communicates with the chamber 82 past a valve 86 controlled by a diaphragm 88 exposed on its opposite sides to the pressure in chambers 90 and 92, a spring 93 being provided to urge the valve 86 closed. The chamber 88 is connected to the manifold I6 and the chamber 92 is connected to the inlet end of the conduit I Il to be subjected to the pressure of air entering the device which may be atmospheric or greater than atmospheric when a supercharger is used. The chamber 82 houses bellows 94 connected to a valve 96 which controls admission of atmospheric pressure to the passageand thence to the chamber 58. The bellows 94 is lled with air or othersuitable gas and sealed at some predetermined pressure, as. for example, 30" of mercury.
The fuel nozzle r48 is controlled by a needle 98 slidably mounted therein and which variably restricts .the area thereof. `The needle 98 carries a pair of plates to receive between them one end of a lever |02 pivoted intermediate its ends at |04 and the opposite end of which enaages a cam |08 carried by and turned with the shaft of valve 24. The cam |08 and the needle 88 may be given any desired contour to effect the desired fuel regulation but are so arranged that the valve 98 is opened as the main throttle 22 is opened. 'Ihe pivot |04 preferably carries a coil spring |08 to hold the upper end of the lever |02 in engagement with the cam |06 and to move the valve 98 toward its closed position as the throttle 22 is closed.
The parts are shown in the idling position with the main throttle valve 22 closed and the valve 24 open, the valve 98 also being substantially closed to restrict the flow of fuel. In this position the conduit |0 is subjected to a high degree of suction, the absolute pressure therein being in the neighborhood of ten inches of mercury, and the manifold I6 is also at a subatmospheric pressure. The diaphragm 88 is accordingly subjected to a pressure differential between chambers 90 and 92 to open the valve 86 and the chamber 82 will be open substantially without restriction to the conduit I8. While the suction in this conduit is relieved to a large extent by air entering past the throttle valve 24, a subatmospheric pressure in the neighborhood of twenty-four inches of mercury exists therein and this pressure, relieved slightly by air entering through vents 12 .and 84, will be communicated to the chamber 82 to cause the bellows 94 to expand and open valve 96. Since the opening controlled by this valve is substantially larger than the orifice 12, the chamber 58 will be subjected to substantially atmospheric pressure so that the diaphragm 58 will be balanced.
The chamber 48 being open to atmosphere through vent 50, it is apparent that the fuel pressure in chamber 40 must be equal to atmospheric pressure plus the force of spring 68 to balance the diaphragm 52. If the fuel pressure is too low the diaphragm 52 will move down to open the valve 38 and admit more fuel while if it is too high the valve 38 will tend to close until it falls. Thus fuel will be supplied to the nozzle 48 under a pressure equal to or slightly in excess of atmospheric. This, coupled with the fact that the fuel at nozzle 48 is subjected to a suction of only about six inches of mercury (atmospheric pressure minus 24" absolute in conduit I8) instead of the twenty inches to which it wouldbe subjected if it discharged directly into the conduit I0 (atmospheric pressure minus absolute in conduit I0), eliminates any tendency for the fuel to boil and insures accurate metering thereof by the valve 98.
As the throttle valve 22 is opened the flow of air through the conduit I0 increases and the suction therein decreases and at the same time the valve 98 is opened to increase the flow of fuel. Simultaneously the valve 24 is closed but the suction in the conduit |8 will not increase because its outlet into the conduit I0 is subjected to a decreasing suction.
When the throttle 22 is opened wide the pressure in the manifold I8 will be increased to substantially atmospheric pressure or greater d ue to operation of the supercharger and the valve 85 will be closed by the diaphragm 98 and spring 93. The pressure in chamber 02 will then rise to substantially atmospheric due to the fact that the vent 84 is of greater capacity than the combined capacities of the orifice 18 and the orifice 18, valve 80 being adustable to regulate to some extent the relative areas of the vents and orifices and consequently the pressure in chamber 82. With the valve 98 closed the pressure in chamber 58 will equal that in conduit I8 due to the connecting passages 88, 10, 12 and 14 and the diaphragm 58 will be subected to a pressure diiierential tending to open the fuel valve 88. Since this force must be balanced by fuel pressure in the chamber 40, the fuel pressure will be correspondingly increased to increase the flow through nozzle 46 and provide a richer mixture.
When the throttle 22 is wide open the suction in conduit I0 is very low, approximately one inch of mercury. Since the valve 24 is closed the same suction will prevail in the conduit I8 and will be transmitted to the chamber 58. Thus at open throttle the fuel pressure will be increased by an amount'substantially equal to the suction in the air conduit.
It will be noted fromthe above that the fuel nozzle is not subjected to a very wide range of suction as is the case in an ordinary carburetor,
particularly a carburetor having an anterior throttle. On the contrary the maximum variation in suction at the nozzle discharge does not exceed flve or six inches of mercury, or between fifteen and twenty percent, as opposed to a variation of approximately twentyinches of mercury or nearly seventy percent in an ordinary carburetor. Accordingly the range of control required of the valve 98 is correspondingly less than in an ordinary carburetor and the fuel can be metered much more accurately.
Between the idling and open-throttle positions are an infinite number of throttle adjustments in the normal operating range in which the main throttle 22 occupies some position between fully closed and fully open. In these positions the valves 86 and 98 may occupy a partially open position to cause a pressure in the chamber 58 lsomewhere between atmospheric and that existing in the conduit I0. 'Ihus the fuel pressure will be slightly increased to increase the ilow from the nozzle 48.
Since the bellows 94 is sealed at a pressure of about 30" of mercury, or atmospheric pressure at sea level, it is sensitive to changes in barometric pressure due to changes in altitude. Ii' the device is employed on an aircraft which rises above. sea level, the reduced barometric pressure around the bellows 94, even with the valve 88 closed, will cause it to expand partially to open the valve 96. This will reduce the suction in chamber 58 to produce a corresponding reduction in fuel pressure so that the mixture will be leaner. Thus decreasing density of the air is automatically compensated for and a correct mixture is maintained.
It will be understood that in actual practice the vents 48, 64, 84 and the vent controlled by valve 98 are connected to the air inlet conduit l0 to be subjected to the pressure of the incoming air therein. This pressure is normally greater than atmospheric due to impact onthe usual air scoop or to increased pressure due to a supercharger.
While only one embodiment of the invention has been shown and described it will be apparent that many changes could be made therein and it is not intended that the scope of the invention shall limited to the form shown'or otherwise than by the terms of the appended claims.
What is claimed is:
1. A charge forming device comprising an air conduit, a fuelmixture conduit discharging into said air conduit, a fuel nozzle discharging into said'mixture conduit, means to supply fuel to said nozzle under positive pressure, and means responsive to the suction in one of said conduits to control the pressure of the fuel at the fuel nozzle.
2. A charge forming device comprisingan air A conduit, a fuel mixture conduit discharging into said air conduit,'a fuel nozzledischarging into aoA , fuel to said nozzle underpressure, and means responsive to the suction in said mixture conduit to control the fuel ypressure at the fuel nozzle.
4. A charge forming device comprising an air conduit, a fuel mixture conduit discharging into said air conduit, a fuel nozzle discharging into said mixture conduit, throttle valves in said conduits anterior to the points of fuel discharge and offuelmixture discharge respectively, means for operating said throttle valves simultaneously to open one and close the other, a valve controlling said fuel nozzle, means controlled by said operating means to control said valve, and means to supply fuel under positive pressure to said nozzle.
5. A charge forming device comprising an air conduit, a fuelmixture lconduit discharging into saidair conduit, a fuel nozzle discharging into said mixture conduit, throttle valves in said conduits anterior to the points of fuel discharge and of fuel mixture discharge respectively, means for operating said throttle valves simultaneously to open one and close the other, a valve controlling said fuel nozzle, means controlled by said operating means to control said valve, means to supply fuel under positive pressure to said nozzle, and means responsive to the suction in said mixture conduit to control the fuel supply means to vary the fuel pressure.
6. A charge forming device comprising an air conduit, a fuel mixture conduit discharging into said air conduit, 'a fuel nozzle discharging into said mixture conduit, throttle valves in said conduits anterior to the points of fuel discharge and of fuel mixture discharge respectively, means for operating said throttle valves simultaneously to open one and close the other, a valve controlling said'fuel nozzle, means controlled by said operating means to control said valve, and means to supply fuel under positive pressure to said nozzle, a pressure responsive regulating device to control the fuel pressure, a connection from said regulating device to the mixture conduit, a valve controlling communication of said connection with atmosphere, and means responsive to air density to control said valve.'
7. A charge forming device comprising anv air conduit, a fuel mixture conduit discharging into saidair conduit, a fuel nozzle discharging into said mixture conduit, throttle valves in said conduits anterior to the points of fuel discharge and of fuel mixture discharge respectively, means for operating said throttle valves simultaneously to open one and close the other, a valve controlling said fuel nozzle, means controlled by said operating means to control said valve, and means to supply fuel under positive pressure to said nozzle,
a pressure responsive regulating device to con-fv trol the fuel pressure, a connection from said regulating device to the mixture conduit, a valve 'controlling communication of said connection with atmosphere, V`and means including. a device responsive to manifold pressure to control 'said valve.
8. A charge'forming device comprising an air conduit, a fuel mixture conduit discharging into said air conduit, a fuel nozzle discharging into said mixture conduit, throttle valves in sani conduits anterior to the points of fuel discharge andof fuel mixture discharge respectively, means for operating said throttle valves simultaneously to open one and close the other, a valve controlling said fuel nozzle, means controlled by said operat-v ing'means to control said valve, and means to supply fuel under positive pressure to said nozzle, a pressure responsive regulating device to control the fuel pressure, a connection from said regulating device to the mixture conduit, a valve controlling communication oli said 'connection with atmosphere, means' responsive to air density to control said valve, a connection froml said last named means to the mixture conduit, and
9.v Ina charge forming device, an induction passage, a fuel mixture passage connected in parallel with th'e induction passage, a fuel nozzle discharging in the mixture passage, means for supplying fuel under pressure to the nozzle, throttles in the induction passage and the mixture passage anterior to the fuel nozzle to the connection ybetween the passages, and a connection'between the throttles for opening the mixture passage throttle as the induction passage throttle is closed and vice versa, the eective cross section of the mixture passage being small relative to that of the induction passage so that the suction existing within the mixture passage and eiective at the nozzle will uctuate Within narrower limits than the suction in the induction passage posterior to the throttle thereof, and means responsive to suction within the mixture passage to control the pressure of fuel supplied to the nozzle. v
10. The invention defined in claim 9 wherein the suction withirrthe mixture passage is modifled by barometric' pressure for controlling the pressure of fuel supplied to the nozzle.
11. The invention defined in claim 9 wherein the means to control the pressure of fuel supplied to the nozzle is jointly responsive to pressure in the mixture passage, to barometric pressure, and to pressure -anterior to the induction passage throttle.
12. A charge forming device comprising an air conduit, a throttle controlling said air conduit, a fuel mixture -conduit discharging into said air conduitpost'erior to the throttle, asfuel nozzle discharging into said mixture conduit, means to supply fuel to said nozzle under positive pressure, a pressure responsive regulating device to control the fuel pressure at'the fuel' nozzle, and a pressure transmittingpassageway interconnecting one of said conduits and the regulating device -for controlling said regulating device.
said air conduit, a fuel nozzle discharging into said mixture conduit, means to supply fuel to said nozzle under positive pressure, a pressure responsive regulating device to control the fuel pressure at the fuel nozzle, a pressure transmitting duct interconnecting one of lsaid conduits and said pressure responsive regulating device, means lncluding a valve for modifying the pressure trans--l mitted to the regulating device by said duct, and means responsive to variations in air density for controllingsaid valve.
l5. A charge forming device comprising anl air conduit, a throttle in said air conduit, a fuel mixture conduit discharging into said air conduit posterior to said throttle, a fuel nozzle discharging into said mixture conduit, a throttle operated valve controlling the iiow of fuel from said nozzle, means to supply fuel to said nozzle under positive pressure, and means responsive to the pressure in one of -said conduits to control the pressureof the fuel at the fuel nozzle. 16. The invention defined in claim 15 wherein the means to control the pressure of the fuel .supplied to the nozzle is jointly responsive to pressure in the said one conduit and to barometric pressure.
FRANK C. MOCK.
US126133A 1937-02-17 1937-02-17 Carburetor Expired - Lifetime US2223381A (en)

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Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416907A (en) * 1943-09-14 1947-03-04 Niles Bement Pond Co Carburetor
US2429781A (en) * 1943-08-16 1947-10-28 George M Holley Fuel control device
US2432664A (en) * 1943-06-26 1947-12-16 United Aircraft Corp Control automatically variable with altitude
US2442463A (en) * 1945-04-26 1948-06-01 Niles Bement Pond Co Fuel supply system for internalcombustion engines
US2445099A (en) * 1944-10-19 1948-07-13 Bendix Aviat Corp Fuel system
US2447265A (en) * 1939-11-03 1948-08-17 Bendix Aviat Corp Fuel control device
US2466441A (en) * 1943-09-01 1949-04-05 Bendix Aviat Corp Pressure responsive selector valve
US2506995A (en) * 1945-12-01 1950-05-09 Niles Bement Pond Co Fuel supply system
US2561106A (en) * 1945-01-20 1951-07-17 Detroit Lubricator Co Fuel feeding control means responsive to air blower pressure
US2576475A (en) * 1944-03-31 1951-11-27 Gen Motors Corp Internal-combustion engine carburetion system
US2581276A (en) * 1945-05-30 1952-01-01 Bendix Aviat Corp Fuel feed and power control system for gas turbines, jet propulsion, and the like
US2581275A (en) * 1944-10-09 1952-01-01 Bendix Aviat Corp Fuel feed responsive to air pressure and temperature, fuel flow, and speed for gas turbines
US2638739A (en) * 1947-11-20 1953-05-19 Niles Bement Pond Co Fuel supply control system for intermittent jet engines
US2674847A (en) * 1948-04-22 1954-04-13 Rolls Royce Control means in fuel system of gas-turbine engines
US2688229A (en) * 1948-07-30 1954-09-07 Niles Bement Pond Co Fuel and speed control for internalcombustion engines
US2697909A (en) * 1946-04-23 1954-12-28 Niles Bement Pond Co Fuel control for turbojet engines
US2778720A (en) * 1957-01-22 Gas carburetor system
US2860616A (en) * 1957-05-31 1958-11-18 Gen Motors Corp Atmospheric nozzle control
US3005448A (en) * 1958-08-13 1961-10-24 Chrysler Corp Fuel injection system
US3347536A (en) * 1966-08-05 1967-10-17 Bendix Corp Carburetor
US3348824A (en) * 1965-06-10 1967-10-24 Inst Francais Du Petrole Automatic arrangement for a carburetor
US3455283A (en) * 1966-09-01 1969-07-15 Harold Phelps Inc Fuel feeding system
US3608872A (en) * 1968-07-18 1971-09-28 Aisan Kogyo Co Ltd Engine fuel supply having separate air and fuel mixing bores
US4000225A (en) * 1976-01-15 1976-12-28 Ford Motor Company Sonic flow variable area venturi carburetor
DE2819474A1 (en) * 1977-05-04 1978-11-09 Aisan Ind FUEL SUPPLY DEVICE FOR COMBUSTION ENGINES
US4142494A (en) * 1977-10-03 1979-03-06 General Motors Corporation Turbocharged engine with vacuum bleed valve
US4157084A (en) * 1977-09-20 1979-06-05 Wallis Marvin E Fuel injection system and method for internal combustion engine
US4216174A (en) * 1977-12-31 1980-08-05 Osrodek Badawczo-Rozwojowy Samochodow Malolitrazowych "Bosmal" Method and apparatus for preparation and control of an air-fuel mixture
US4224904A (en) * 1977-06-27 1980-09-30 Clerk Ernest J Carburettor for air and liquid fuel under pressure for internal combustion engines
US4241711A (en) * 1978-12-05 1980-12-30 Schmelzer Corporation Fuel control system
US4264539A (en) * 1979-12-12 1981-04-28 Samuel Ray Dickenson Liquid fuel vaporizer
US4353338A (en) * 1979-11-13 1982-10-12 Colt Industries Operating Corp. Engine idle air valve means and system
US4378761A (en) * 1978-11-01 1983-04-05 Nissan Motor Co., Ltd. Fuel supply system for a multi-cylinder internal combustion engine
US6786208B1 (en) * 2003-06-10 2004-09-07 Hector H. Velez-Velez Boost fuel enricher
US6827338B2 (en) * 2001-09-27 2004-12-07 Zama Japan Scavenging air/fuel-air mixture control device for a stratified scavenging two-cycle engine

Cited By (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778720A (en) * 1957-01-22 Gas carburetor system
US2447265A (en) * 1939-11-03 1948-08-17 Bendix Aviat Corp Fuel control device
US2432664A (en) * 1943-06-26 1947-12-16 United Aircraft Corp Control automatically variable with altitude
US2429781A (en) * 1943-08-16 1947-10-28 George M Holley Fuel control device
US2466441A (en) * 1943-09-01 1949-04-05 Bendix Aviat Corp Pressure responsive selector valve
US2416907A (en) * 1943-09-14 1947-03-04 Niles Bement Pond Co Carburetor
US2576475A (en) * 1944-03-31 1951-11-27 Gen Motors Corp Internal-combustion engine carburetion system
US2581275A (en) * 1944-10-09 1952-01-01 Bendix Aviat Corp Fuel feed responsive to air pressure and temperature, fuel flow, and speed for gas turbines
US2445099A (en) * 1944-10-19 1948-07-13 Bendix Aviat Corp Fuel system
US2561106A (en) * 1945-01-20 1951-07-17 Detroit Lubricator Co Fuel feeding control means responsive to air blower pressure
US2442463A (en) * 1945-04-26 1948-06-01 Niles Bement Pond Co Fuel supply system for internalcombustion engines
US2581276A (en) * 1945-05-30 1952-01-01 Bendix Aviat Corp Fuel feed and power control system for gas turbines, jet propulsion, and the like
US2506995A (en) * 1945-12-01 1950-05-09 Niles Bement Pond Co Fuel supply system
US2697909A (en) * 1946-04-23 1954-12-28 Niles Bement Pond Co Fuel control for turbojet engines
US2638739A (en) * 1947-11-20 1953-05-19 Niles Bement Pond Co Fuel supply control system for intermittent jet engines
US2674847A (en) * 1948-04-22 1954-04-13 Rolls Royce Control means in fuel system of gas-turbine engines
US2688229A (en) * 1948-07-30 1954-09-07 Niles Bement Pond Co Fuel and speed control for internalcombustion engines
US2860616A (en) * 1957-05-31 1958-11-18 Gen Motors Corp Atmospheric nozzle control
US3005448A (en) * 1958-08-13 1961-10-24 Chrysler Corp Fuel injection system
US3348824A (en) * 1965-06-10 1967-10-24 Inst Francais Du Petrole Automatic arrangement for a carburetor
US3347536A (en) * 1966-08-05 1967-10-17 Bendix Corp Carburetor
US3455283A (en) * 1966-09-01 1969-07-15 Harold Phelps Inc Fuel feeding system
US3608872A (en) * 1968-07-18 1971-09-28 Aisan Kogyo Co Ltd Engine fuel supply having separate air and fuel mixing bores
US4000225A (en) * 1976-01-15 1976-12-28 Ford Motor Company Sonic flow variable area venturi carburetor
DE2819474A1 (en) * 1977-05-04 1978-11-09 Aisan Ind FUEL SUPPLY DEVICE FOR COMBUSTION ENGINES
DE2819474C2 (en) * 1977-05-04 1987-05-21 Toyota Jidosha Kogyo K.K., Toyota, Aichi, Jp
US4224904A (en) * 1977-06-27 1980-09-30 Clerk Ernest J Carburettor for air and liquid fuel under pressure for internal combustion engines
US4157084A (en) * 1977-09-20 1979-06-05 Wallis Marvin E Fuel injection system and method for internal combustion engine
US4142494A (en) * 1977-10-03 1979-03-06 General Motors Corporation Turbocharged engine with vacuum bleed valve
US4216174A (en) * 1977-12-31 1980-08-05 Osrodek Badawczo-Rozwojowy Samochodow Malolitrazowych "Bosmal" Method and apparatus for preparation and control of an air-fuel mixture
US4378761A (en) * 1978-11-01 1983-04-05 Nissan Motor Co., Ltd. Fuel supply system for a multi-cylinder internal combustion engine
US4241711A (en) * 1978-12-05 1980-12-30 Schmelzer Corporation Fuel control system
US4353338A (en) * 1979-11-13 1982-10-12 Colt Industries Operating Corp. Engine idle air valve means and system
US4264539A (en) * 1979-12-12 1981-04-28 Samuel Ray Dickenson Liquid fuel vaporizer
US6827338B2 (en) * 2001-09-27 2004-12-07 Zama Japan Scavenging air/fuel-air mixture control device for a stratified scavenging two-cycle engine
US20050001335A1 (en) * 2001-09-27 2005-01-06 Takumi Nonaka Scavenging air/fuel-air mixture control device for a stratified scavenging two-cycle engine
US6843469B1 (en) 2001-09-27 2005-01-18 Zama Japan Scavenging air/fuel-air mixture control device for a stratified scavenging two-cycle engine
US6786208B1 (en) * 2003-06-10 2004-09-07 Hector H. Velez-Velez Boost fuel enricher

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