US2511213A - Carbureting apparatus - Google Patents

Carbureting apparatus Download PDF

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US2511213A
US2511213A US590379A US59037945A US2511213A US 2511213 A US2511213 A US 2511213A US 590379 A US590379 A US 590379A US 59037945 A US59037945 A US 59037945A US 2511213 A US2511213 A US 2511213A
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air
fuel
manifold
pressure
engine
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US590379A
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John H Leslie
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Stewart Warner Corp
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Stewart Warner Corp
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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
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2720/00Engines with liquid fuel
    • F02B2720/15Mixture compressing engines with ignition device and mixture formation in the cylinder
    • F02B2720/152Mixture compressing engines with ignition device and mixture formation in the cylinder with fuel supply and pulverisation by injecting the fuel under pressure during the suction or compression stroke

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  • Another object of the invention is to provide new and improved means for maintaining a substantially constant air pressure immediately adjacent the point of discharge of each of the nozzles.
  • a further object of the invention is to provide a new and improved fuel control valve with means responsive to variations in the pressure of the fuel supply to regulate the pressure at which the fuel is fed to the engine intake and to automatically vary the flowl of fuel in accordance with changes in the rate of engine air induction.
  • FIG. 1 fragmentary side elevation of a multiple cylinder internal combustion engine with the intake passage and air induction tube shown in section;
  • Fig. 2 is a fragmentary top plan view of the engine shown in Fig. l but with the air induction tube shown ⁇ in transverse section, as indicated at line 2-2 on Fig. l;
  • Fig. 3 is a vertical detail section. taken suby stantially as indicated at line 3-3 on Fig. 1 but on a larger scale; L
  • Fig. 4 is a vertical detail sectional view of the sure. It is preferable to arrange the nozzles in such a way that they shall be subject to constant pressure at their discharge openings; then since the fuel is fed to the nozzles at variable pressures, depending upon the air flow rate, the rate of fuel supply can be proportioned properly to the air flow rate and will not be additionally altered -by other variable factors such as the pressure in the inlet manifold and intake passages. However, alteration of the proportions of fuel and air can still be effected intentionally, Iby use of the choke valve.
  • the drawings illustrate a multiple cylinder engine I0 having an exhaust manifold I2 which may be of conventional design and having an intake manifold I4 which is shown as provided with an air induction tube I6 connected into the middle of the length of the manifold I4 for distributing air to the several branch intake passages I8 each of which leads to one of the engine cylinders.
  • the air induction tube has the usual Venturi form with its constriction at 20 and is fitted with a throttle valve 22.and a choke valve 24.
  • the tube IB is shown surmounted by an air filter 26.
  • auxiliary passages 28, 2B extending along opposite sides of the air induction tube I6 and continuing in passages 30, 30, each associated with a portion of the intake manifold I4 and each having branch passages 32 associated with the re- .i fuel feeding valve device being taken substantially a5 indicated at line l--I 0n Fig. 2.
  • spective intake passages I8- which lead to the several cylinders.
  • the air intake ports 34 of the auxiliary passages 28 are-located adjacent the outer end of the induction tube I 6 beyond the choke 24 but in position to receive ltered air from the filter 26; and each of the branch passages 32 connects with the intake passage I8 by way of a port or orifice 38 which is preferably dimensioned to supply just enough air for idling the engine with the throttle valve 22 completely closed.
  • the auxiliary passages 28, are thus open to atmospheric pressure at all times independently of the adjustment of the choke 24 or throttle 22 and a space in each of their branches 32 adjacent the port 3G is thus maintained constantly at substantially atmospheric pressure.
  • each of the ports serves for introduction of the liquid fuel into the air stream by reason of the fact that a fuel injection nozzle 3l is mounted in the top wall of each branch e 32 in position to discharge a jet or fine spray of fuel across the air gap indicated at 4l in Fig. 3 and directly through the port It into the intake passage Il, adjacent the inlet valve 42 of the engine cylinder. Since the discharge opening 44 of the nozzle Il is spaced back from the port It with the air gap interposed, the nozzle will be subject to the substantially uniform atmospheric pressure which is maintained in the auxiliary passage 32.
  • Fuel is supplied to each of the nozzles Il by a feed tube 4I having a T-fltting 48 into which the supply tube Il is coupled.
  • the tube leads from a fuel control valve device denoted generally by the numeral l2 and shown in detail in Fig. 4.
  • the device includes a lower casting 54 containing a fuel chamber 54 with a valve seat fitting 58 screwed into the bottom'of the chamber in the inlet passage thereof into which is connected the supply pipe 60 leading from .the engine driven pump 82 as shown in Fig. 1.
  • 'I'he cast element 54 is surmounted by a second casting 64 and a cover plate it with a flexible diaphragm Bl interposed between the parts 54 and B4 and with a larger flexible diaphragm 1l peripherally clamped between the parts I4 and It.
  • the diaphragm 6l thus forms the top wall of the fuel chamber N and it is provided with a centrally disposed button 12 which engages the stem 14 of the fuel inlet valve 16.
  • the valve is normally urged toward its seat 1l by means of a spring 80 disposed below the valve in the valve seat fitting BI.
  • the cast body element 44 together with the diaphragms tl and 10 defines a suction or vacuum chamber 82 which is maintained in communication with the air induction tube It of the engine by means of a pipe 44 having a terminal fitting l. which leads from a port Il located at the construction 2l of the venturi.
  • the chamber I2 and the flexible diaphragm 1II are thus subject at all times to variations in suction produced at the Venturi throat by adjustment of the throttle 22 or the choke 24.
  • a high vacuum is produced which pulls strongly against the diaphragm 1li drawing it downwardly in the chamber l2.
  • a pin IB is clamped to the center of the diaphragm 10 and projects downwardly therefrom into engagement with a small hollow shell 92 secured to the upper side of the diaphragm 6l by the button 12.
  • the downward movement of the diaphragm 1l is transmitted by the pin ll to the button 12 and to the valve stem 14, forcing the valve open in opposition to its spring Il and permitting the liquid fuel supplied under pressure by the pump l2 to flow from the orifices I4 into the chamber It and thence by way of the the engine and as the choke is opened admit- .f ting air, a more correct mixture for continued operation is supplied.
  • the diaphragm 1l is readily responsive to the suction produced at the Venturi throat 20 because the upper side of the diaphragm is exposed to atmospheric pressure through the constantly open vent $4 in the top wall Il of the fuel control device.
  • Fig. 4 shows a spring Illreacting between the diaphragm 10 and a flange disc
  • the valve control mechanism would function as described without the spring Ill but this spring is supplied to counteract or balance the spring Il which urges the valve 1l toward its seat.
  • the balancing pressure furnished by the spring Ill may then be varied by means of the screw ll4 so as to provide the desired adjustment in the effective strength of the spring I4 for seating the valve and this adjustment may be maintained by means of a lock nut III on the screw
  • a charge forming device of a multiple outlet type which mixes a metered quantity of fuel prises a temporarily rich mixture for starting with air immediately adjacent the several outlets
  • the combination comprising an intake air manifold having an atmospheric opening and a plurality of outlet openings, said air manifold having a Venturi section therein to form a flow meter, a throttle valve downstream of said venturi so that actuation of said throttle valve controls the air delivery rate from all of said outlets while the pressure at said venturi is a function of the flow rate through said manifold and is independent of the pressure prevailing in said manifold downstream of said throttle valve.
  • said manifold having a plurality of openings through the wall thereof each disposed immediately adjacent one of said outlets, a plurality of fuel nozzles each disposed adjacent to and in axial alignment with one of said openings and so disposed as to project jets of fuel from said nozzles through the intervening free space and through said openings and into said manifold immediately adjacent each of said outlets, means forming a second manifold enclosing the separate spaces between each of said nozzles and its associated opening, said second manifold having a connection to said first manifold at a point upstream of said throttle valve, and means including control means responsive to the preslsure at said venturi to supply said nozzles with fuel at a pressure which is a function of thel Venturi pressure.
  • a charge forming device having the combination called for in claim 1 and an air filter connected to the atmospheric opening of said air intake manifold whereby said air cleaner serves to remove dust particles and the like from the air stream passing through said air intake manifold and through said second manifold.
  • a charge forming device for a multiple cylinder combustion engine of the type which mixes a metered quantity of fuel with air immediately adjacent the several engine intake ports, the combination comprising an intake air manifold having an atmospheric opening at one end and a plurality of outlet openings adapted to communicate with the individual engine ports, said air manifold having a Venturi section therein to form a flow meter, a throttle valve downstream of said venturi so that actuation of said throttle valve controls the air delivery rate from all of said outlet openings while the pressure at said venturi is -a function of the flow rate through said manifold and is independent of the pressure prevailing in said manifold downstream of said throttle valve, said manifold having a plurality of openings through the side wall thereof each disposed immediately adjacent one of said outlet openings, a plurality of fuel noze zles each disposed adjacent to and in axial alignment with one of said openings and so disposed as to project jets of fuel from said nozzles through the intervening free space and through said openings and into said manifold immediately

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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

June 13, 1950 J. H. LESLIE, It
CARBURETING APPARATUS 3 Sheets-Sheet 1 Filed April 26, 1945 June 13, 1950 J. H. LESLIE, 1I
CARBURETING APPARATUS 3 Sheets-Sheet 2 Filed April 26, 1945 June 13, 1950 .L H. LESLIE, 1I 2,511,213
CARBURETING APPARATUS Filed April ze, 1945 s shuts-sheet s lllllll VIII Illlll Maz/wsa Patented June 13, 1950 UNIT-Eo STATES` PATENT OFFICE.l
2,511,213 CARBURE'rmG APPARATUS John H. Leslie, 1I, Winnetka, lll., assigner to Stewart-Warner Corporation, Chicago, Ill., a A. corporation of Virginia Application April 26, 1945, Serial No. 590,379
' tions in the rate of engine air induction for controlling the rate at which the fuel is fed into the intake passage. f
Another object of the invention is to provide new and improved means for maintaining a substantially constant air pressure immediately adjacent the point of discharge of each of the nozzles.
A further object of the invention is to provide a new and improved fuel control valve with means responsive to variations in the pressure of the fuel supply to regulate the pressure at which the fuel is fed to the engine intake and to automatically vary the flowl of fuel in accordance with changes in the rate of engine air induction.
It is also an object of the invention to provide an internal combustion engine with an auxiliary air supply arranged to furnish a limited quantity of air to each of the engine cylinders independently of the throttle valve which controls the main air supply and to provide a space adjacent the intake passage of each cylinder and inl communication therewith to which the auxiliary air is furnished at substantially atmospheric pressure and into which space the fuel feeding nozzle extends so as to be subject to atmospheric pressure at all times in order to insure uniformity of operation of the fuel feeding means.
Other objects and advantages of the invention will appear from the following description taken in connection' with the drawings, in which: l
Fig. 1 fragmentary side elevation of a multiple cylinder internal combustion engine with the intake passage and air induction tube shown in section;
4 Claims. (C1. 261.-40)
In the fuel feeding and carbureting system to I which this invention relates, the liquid fuel is supplied by an engine driven pump and is re- V leased to the cylinders by a pressure control valve device which is responsive to variations of the air flow rate to the intake manifold, such varil ations being produced mainly by adjustment of the throttle valve and =by engine load and speed.
The liquid fuel is distributed from the control valve device to individual nozzles by which it is sprayed into the intake passage adjacent the inlet valve of each cylinder; but since -the pressure in the intake passages varies through wide limits in the course of operation of the engine, it is undesirable to have the outlet orifices of the i fuel nozzles subjected to these variations in pres- Fig. 2 is a fragmentary top plan view of the engine shown in Fig. l but with the air induction tube shown` in transverse section, as indicated at line 2-2 on Fig. l;
4Fig. 3 is a vertical detail section. taken suby stantially as indicated at line 3-3 on Fig. 1 but on a larger scale; L
Fig. 4 is a vertical detail sectional view of the sure. It is preferable to arrange the nozzles in such a way that they shall be subject to constant pressure at their discharge openings; then since the fuel is fed to the nozzles at variable pressures, depending upon the air flow rate, the rate of fuel supply can be proportioned properly to the air flow rate and will not be additionally altered -by other variable factors such as the pressure in the inlet manifold and intake passages. However, alteration of the proportions of fuel and air can still be effected intentionally, Iby use of the choke valve.
The drawings illustrate a multiple cylinder engine I0 having an exhaust manifold I2 which may be of conventional design and having an intake manifold I4 which is shown as provided with an air induction tube I6 connected into the middle of the length of the manifold I4 for distributing air to the several branch intake passages I8 each of which leads to one of the engine cylinders. The air induction tube has the usual Venturi form with its constriction at 20 and is fitted with a throttle valve 22.and a choke valve 24. The tube IB is shown surmounted by an air filter 26.
In addition to the air supplied by the induction tube I6 and intake manifold I4, the cylinders are furnished with a limited auxiliary air supply provided by auxiliary passages 28, 2B extending along opposite sides of the air induction tube I6 and continuing in passages 30, 30, each associated with a portion of the intake manifold I4 and each having branch passages 32 associated with the re- .i fuel feeding valve device being taken substantially a5 indicated at line l--I 0n Fig. 2.
spective intake passages I8- which lead to the several cylinders. The air intake ports 34 of the auxiliary passages 28 are-located adjacent the outer end of the induction tube I 6 beyond the choke 24 but in position to receive ltered air from the filter 26; and each of the branch passages 32 connects with the intake passage I8 by way of a port or orifice 38 which is preferably dimensioned to supply just enough air for idling the engine with the throttle valve 22 completely closed. The auxiliary passages 28, are thus open to atmospheric pressure at all times independently of the adjustment of the choke 24 or throttle 22 and a space in each of their branches 32 adjacent the port 3G is thus maintained constantly at substantially atmospheric pressure.
In addition to furnishing air for idling the engine, each of the ports serves for introduction of the liquid fuel into the air stream by reason of the fact that a fuel injection nozzle 3l is mounted in the top wall of each branch e 32 in position to discharge a jet or fine spray of fuel across the air gap indicated at 4l in Fig. 3 and directly through the port It into the intake passage Il, adjacent the inlet valve 42 of the engine cylinder. Since the discharge opening 44 of the nozzle Il is spaced back from the port It with the air gap interposed, the nozzle will be subject to the substantially uniform atmospheric pressure which is maintained in the auxiliary passage 32.
Fuel is supplied to each of the nozzles Il by a feed tube 4I having a T-fltting 48 into which the supply tube Il is coupled. The tube leads from a fuel control valve device denoted generally by the numeral l2 and shown in detail in Fig. 4. The device includes a lower casting 54 containing a fuel chamber 54 with a valve seat fitting 58 screwed into the bottom'of the chamber in the inlet passage thereof into which is connected the supply pipe 60 leading from .the engine driven pump 82 as shown in Fig. 1. 'I'he cast element 54 is surmounted by a second casting 64 and a cover plate it with a flexible diaphragm Bl interposed between the parts 54 and B4 and with a larger flexible diaphragm 1l peripherally clamped between the parts I4 and It. The diaphragm 6l thus forms the top wall of the fuel chamber N and it is provided with a centrally disposed button 12 which engages the stem 14 of the fuel inlet valve 16. The valve is normally urged toward its seat 1l by means of a spring 80 disposed below the valve in the valve seat fitting BI.
The cast body element 44 together with the diaphragms tl and 10 defines a suction or vacuum chamber 82 which is maintained in communication with the air induction tube It of the engine by means of a pipe 44 having a terminal fitting l. which leads from a port Il located at the construction 2l of the venturi. The chamber I2 and the flexible diaphragm 1II are thus subject at all times to variations in suction produced at the Venturi throat by adjustment of the throttle 22 or the choke 24. Thus, in starting the engine with the choke substantially closed, a high vacuum is produced which pulls strongly against the diaphragm 1li drawing it downwardly in the chamber l2. A pin IB is clamped to the center of the diaphragm 10 and projects downwardly therefrom into engagement with a small hollow shell 92 secured to the upper side of the diaphragm 6l by the button 12. Thus the downward movement of the diaphragm 1l is transmitted by the pin ll to the button 12 and to the valve stem 14, forcing the valve open in opposition to its spring Il and permitting the liquid fuel supplied under pressure by the pump l2 to flow from the orifices I4 into the chamber It and thence by way of the the engine and as the choke is opened admit- .f ting air, a more correct mixture for continued operation is supplied. The diaphragm 1l is readily responsive to the suction produced at the Venturi throat 20 because the upper side of the diaphragm is exposed to atmospheric pressure through the constantly open vent $4 in the top wall Il of the fuel control device.
It will be noted that the suction applied to the chamber l2 will act upwardly upon the flexible wall or diaphragm Il as well as downwardly upon the diaphragm 1l, but that because of the larger area of the diaphragm 1l, the net result will be a force in the downward direction. This excess force of the suction applied through the diaphragm 10 is sufncient to overcome the force of the fuel pressure acting upwardly against the diaphragm Il in a direction to permit the fuel inlet valve 1l to close. If the fuel pressure increases, this valve 14 will move toward closed position reducing the rate of flow, and if the fuel pressure is lowered, the valve 1l will open wider, increasing the flow rate. The effects of pressure variations at the fuel pump are thus neutralized, and the final rate oi' fuel now is determined by the adjusted position of the diaphragm 10 in response to the suction created by air now in the induction tube II. Y
Fig. 4 shows a spring Illreacting between the diaphragm 10 and a flange disc |02 carried on the end of an adjusting screw Il4 which is threaded into a boss III formed in the top wall I4. The valve control mechanism would function as described without the spring Ill but this spring is supplied to counteract or balance the spring Il which urges the valve 1l toward its seat. The balancing pressure furnished by the spring Ill may then be varied by means of the screw ll4 so as to provide the desired adjustment in the effective strength of the spring I4 for seating the valve and this adjustment may be maintained by means of a lock nut III on the screw |44.
While there is shown and described herein certain structure embodying the invention, it is to be understood that the invention is not limited thereto or thereby but may assume numerous other forms and includes all modifications. variations and equivalents coming within the scope of the following claims:
I claim:
1. In a charge forming device of a multiple outlet type which mixes a metered quantity of fuel duces a temporarily rich mixture for starting with air immediately adjacent the several outlets, the combination comprising an intake air manifold having an atmospheric opening and a plurality of outlet openings, said air manifold having a Venturi section therein to form a flow meter, a throttle valve downstream of said venturi so that actuation of said throttle valve controls the air delivery rate from all of said outlets while the pressure at said venturi is a function of the flow rate through said manifold and is independent of the pressure prevailing in said manifold downstream of said throttle valve. said manifold having a plurality of openings through the wall thereof each disposed immediately adjacent one of said outlets, a plurality of fuel nozzles each disposed adjacent to and in axial alignment with one of said openings and so disposed as to project jets of fuel from said nozzles through the intervening free space and through said openings and into said manifold immediately adjacent each of said outlets, means forming a second manifold enclosing the separate spaces between each of said nozzles and its associated opening, said second manifold having a connection to said first manifold at a point upstream of said throttle valve, and means including control means responsive to the preslsure at said venturi to supply said nozzles with fuel at a pressure which is a function of thel Venturi pressure.
2. The combination called for in claim 1 in which said openings are so proportioned as to supply a ilxed minimum flow of air from said outlets.
3. A charge forming device having the combination called for in claim 1 and an air filter connected to the atmospheric opening of said air intake manifold whereby said air cleaner serves to remove dust particles and the like from the air stream passing through said air intake manifold and through said second manifold.
4. In a charge forming device for a multiple cylinder combustion engine of the type which mixes a metered quantity of fuel with air immediately adjacent the several engine intake ports, the combination comprising an intake air manifold having an atmospheric opening at one end and a plurality of outlet openings adapted to communicate with the individual engine ports, said air manifold having a Venturi section therein to form a flow meter, a throttle valve downstream of said venturi so that actuation of said throttle valve controls the air delivery rate from all of said outlet openings while the pressure at said venturi is -a function of the flow rate through said manifold and is independent of the pressure prevailing in said manifold downstream of said throttle valve, said manifold having a plurality of openings through the side wall thereof each disposed immediately adjacent one of said outlet openings, a plurality of fuel noze zles each disposed adjacent to and in axial alignment with one of said openings and so disposed as to project jets of fuel from said nozzles through the intervening free space and through said openings and into said manifold immediately adjacent each of said outlet openings, said openings being so proportioned as to supply an appropriate flow of air to said ports under idling conditions of said engine, means forming a second manifold enclosing the separate spaces between each of said nozzles and its associated opening, said second manifold having a connection to said first manifold at a point upstream of said throttle valve, and means including control means responsive to the pressure at said venturi to supply said nozzles with fuel at a pressure which is a function of the Venturi pressure.
JOI-IN H. LESLIE, II.
REFERENCES crrnn The following references are of record in the le of this patent:
UNITED STATES PATENTS Mennesson Jan. 1. 1946
US590379A 1945-04-26 1945-04-26 Carbureting apparatus Expired - Lifetime US2511213A (en)

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Cited By (38)

* Cited by examiner, † Cited by third party
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US2654995A (en) * 1947-11-01 1953-10-13 Mcdonnell Aircraft Corp Maximum-minimum fuel flow regulator responsive to ram jet engine ram pressure
US2688845A (en) * 1948-07-13 1954-09-14 Mcdonnell Aircraft Corp Two-stage fuel regulator for pulse jet engines
US2706885A (en) * 1948-01-15 1955-04-26 Mcdonnell Aircraft Corp Fuel regulator responsive to speed and atmospheric pressure
US2833260A (en) * 1955-05-31 1958-05-06 Gen Motors Corp Atmospheric vent for fuel injection nozzle
US2843096A (en) * 1956-06-29 1958-07-15 Gen Motors Corp Fuel distribution means
US2860859A (en) * 1956-09-10 1958-11-18 Gen Motors Corp Fuel injection nozzle
US2863433A (en) * 1954-10-06 1958-12-09 Chrysler Corp Low pressure fuel injection system
US2871841A (en) * 1954-10-04 1959-02-03 Laurence M Goodridge Pressure injection type carburetor
DE1052170B (en) * 1957-05-31 1959-03-05 Gen Motors Corp Fuel injection system for internal combustion engines
US2888912A (en) * 1955-05-13 1959-06-02 Citroen Sa Andre Fuel-injection system for spark-ignition engine
US2893365A (en) * 1956-05-31 1959-07-07 Gen Motors Corp Fuel injection means
US2894735A (en) * 1957-02-25 1959-07-14 Gen Motors Corp Fuel metering system
US2902016A (en) * 1957-06-10 1959-09-01 Continental Motors Corp Fuel injection system
US2913235A (en) * 1957-07-11 1959-11-17 Gen Motors Corp Atmospheric nozzle for fuel injection system
US2913233A (en) * 1957-01-16 1959-11-17 Continental Motors Corp Fuel injector
DE1083595B (en) * 1956-09-10 1960-06-15 Gen Motors Corp Internal combustion engine with valveless injection nozzles
DE1085376B (en) * 1958-03-05 1960-07-14 Gen Motors Corp Fuel injection system for internal combustion engines
DE1085377B (en) * 1957-12-21 1960-07-14 Sibe Device for injecting fuel into the intake line of an engine
US2957464A (en) * 1956-06-18 1960-10-25 Gen Motors Corp Fuel injection system
US2957682A (en) * 1957-05-13 1960-10-25 Holley Carburetor Co Fuel system
US2963282A (en) * 1957-05-02 1960-12-06 Gen Motors Corp Fuel nozzle
US2980090A (en) * 1956-02-24 1961-04-18 Bendix Corp Fuel injection system
US2983491A (en) * 1958-11-13 1961-05-09 Continental Motors Corp Fuel injection system
US3005448A (en) * 1958-08-13 1961-10-24 Chrysler Corp Fuel injection system
US3174732A (en) * 1962-09-28 1965-03-23 Acf Ind Inc Carburetor
US3181843A (en) * 1962-12-17 1965-05-04 Acf Ind Inc Carburetor
US3181519A (en) * 1956-06-14 1965-05-04 Gen Motors Corp Fuel control
US3232284A (en) * 1963-07-30 1966-02-01 Carl F High Internal combustion engine
US3234926A (en) * 1963-04-19 1966-02-15 William H Mashinter Method and apparatus for supplying fuel
DE1270881B (en) * 1962-07-13 1968-06-20 Bosch Gmbh Robert Device for the introduction of fuel in a multi-cylinder, mixture-compressing internal combustion engine
US3519407A (en) * 1966-06-27 1970-07-07 Fuel Injection Eng Co Fuel injection nozzle
US3608531A (en) * 1968-07-04 1971-09-28 Brico Eng Fuel injection
US3620511A (en) * 1968-10-22 1971-11-16 Audi Ag Carburetor system for combustion engines
US3643635A (en) * 1970-04-24 1972-02-22 William T Milam Electronic fuel injection system
US3783844A (en) * 1972-02-18 1974-01-08 Gen Motors Corp Fuel injection system
US3788287A (en) * 1972-02-18 1974-01-29 Gen Motors Corp Fuel injection system
US4445473A (en) * 1978-04-13 1984-05-01 Yamaha Hatsudoki Kabushiki Kaisha Control of carburetor-supplied induction system
US4513700A (en) * 1978-05-17 1985-04-30 Yamaha Hatsudoki Kabushiki Kaisha Induction system for spark ignition engine of fuel injection type

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US1795319A (en) * 1926-10-14 1931-03-10 Curtis B Camp Carburetor
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US996110A (en) * 1910-01-25 1911-06-27 Miller Automatic Safety Gas Valve Co Automatic shut-off valve and fire-alarm combined.
US1622010A (en) * 1922-09-26 1927-03-22 Frank S Summer External-combustion engine
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US2216422A (en) * 1936-06-25 1940-10-01 Schimanek Emil Charge former
US2215597A (en) * 1937-09-28 1940-09-24 Charles F Semon Fluid pressure regulating device
US2392055A (en) * 1940-05-24 1946-01-01 Mennesson Marcel Louis Carburetor of the fuel injection type
US2314580A (en) * 1941-09-16 1943-03-23 Phillips Petroleum Co Carburetor
US2364330A (en) * 1942-03-16 1944-12-05 Weigel Daniel Michael Internal-combustion engine
US2382625A (en) * 1942-03-19 1945-08-14 Phillips Petroleum Co Manifold injection carburetor

Cited By (38)

* Cited by examiner, † Cited by third party
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US2654995A (en) * 1947-11-01 1953-10-13 Mcdonnell Aircraft Corp Maximum-minimum fuel flow regulator responsive to ram jet engine ram pressure
US2706885A (en) * 1948-01-15 1955-04-26 Mcdonnell Aircraft Corp Fuel regulator responsive to speed and atmospheric pressure
US2688845A (en) * 1948-07-13 1954-09-14 Mcdonnell Aircraft Corp Two-stage fuel regulator for pulse jet engines
US2871841A (en) * 1954-10-04 1959-02-03 Laurence M Goodridge Pressure injection type carburetor
US2863433A (en) * 1954-10-06 1958-12-09 Chrysler Corp Low pressure fuel injection system
US2888912A (en) * 1955-05-13 1959-06-02 Citroen Sa Andre Fuel-injection system for spark-ignition engine
US2833260A (en) * 1955-05-31 1958-05-06 Gen Motors Corp Atmospheric vent for fuel injection nozzle
US2980090A (en) * 1956-02-24 1961-04-18 Bendix Corp Fuel injection system
US2893365A (en) * 1956-05-31 1959-07-07 Gen Motors Corp Fuel injection means
US3181519A (en) * 1956-06-14 1965-05-04 Gen Motors Corp Fuel control
US2957464A (en) * 1956-06-18 1960-10-25 Gen Motors Corp Fuel injection system
US2843096A (en) * 1956-06-29 1958-07-15 Gen Motors Corp Fuel distribution means
DE1083595B (en) * 1956-09-10 1960-06-15 Gen Motors Corp Internal combustion engine with valveless injection nozzles
US2860859A (en) * 1956-09-10 1958-11-18 Gen Motors Corp Fuel injection nozzle
US2913233A (en) * 1957-01-16 1959-11-17 Continental Motors Corp Fuel injector
US2894735A (en) * 1957-02-25 1959-07-14 Gen Motors Corp Fuel metering system
US2963282A (en) * 1957-05-02 1960-12-06 Gen Motors Corp Fuel nozzle
US2957682A (en) * 1957-05-13 1960-10-25 Holley Carburetor Co Fuel system
DE1052170B (en) * 1957-05-31 1959-03-05 Gen Motors Corp Fuel injection system for internal combustion engines
US2902016A (en) * 1957-06-10 1959-09-01 Continental Motors Corp Fuel injection system
US2913235A (en) * 1957-07-11 1959-11-17 Gen Motors Corp Atmospheric nozzle for fuel injection system
DE1085377B (en) * 1957-12-21 1960-07-14 Sibe Device for injecting fuel into the intake line of an engine
DE1085376B (en) * 1958-03-05 1960-07-14 Gen Motors Corp Fuel injection system for internal combustion engines
US3005448A (en) * 1958-08-13 1961-10-24 Chrysler Corp Fuel injection system
US2983491A (en) * 1958-11-13 1961-05-09 Continental Motors Corp Fuel injection system
DE1270881B (en) * 1962-07-13 1968-06-20 Bosch Gmbh Robert Device for the introduction of fuel in a multi-cylinder, mixture-compressing internal combustion engine
US3174732A (en) * 1962-09-28 1965-03-23 Acf Ind Inc Carburetor
US3181843A (en) * 1962-12-17 1965-05-04 Acf Ind Inc Carburetor
US3234926A (en) * 1963-04-19 1966-02-15 William H Mashinter Method and apparatus for supplying fuel
US3232284A (en) * 1963-07-30 1966-02-01 Carl F High Internal combustion engine
US3519407A (en) * 1966-06-27 1970-07-07 Fuel Injection Eng Co Fuel injection nozzle
US3608531A (en) * 1968-07-04 1971-09-28 Brico Eng Fuel injection
US3620511A (en) * 1968-10-22 1971-11-16 Audi Ag Carburetor system for combustion engines
US3643635A (en) * 1970-04-24 1972-02-22 William T Milam Electronic fuel injection system
US3783844A (en) * 1972-02-18 1974-01-08 Gen Motors Corp Fuel injection system
US3788287A (en) * 1972-02-18 1974-01-29 Gen Motors Corp Fuel injection system
US4445473A (en) * 1978-04-13 1984-05-01 Yamaha Hatsudoki Kabushiki Kaisha Control of carburetor-supplied induction system
US4513700A (en) * 1978-05-17 1985-04-30 Yamaha Hatsudoki Kabushiki Kaisha Induction system for spark ignition engine of fuel injection type

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