US3608531A - Fuel injection - Google Patents

Fuel injection Download PDF

Info

Publication number
US3608531A
US3608531A US835620A US3608531DA US3608531A US 3608531 A US3608531 A US 3608531A US 835620 A US835620 A US 835620A US 3608531D A US3608531D A US 3608531DA US 3608531 A US3608531 A US 3608531A
Authority
US
United States
Prior art keywords
fuel
pressure
exhaust gas
supply
engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US835620A
Inventor
Albert E Baxendale
Brian H Croft
George E Fowle
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Federal Mogul Coventry Ltd
Original Assignee
Brico Engineering Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Brico Engineering Ltd filed Critical Brico Engineering Ltd
Application granted granted Critical
Publication of US3608531A publication Critical patent/US3608531A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02M69/08Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air

Definitions

  • the present invention relates to a fuel injection system for internal combustion engines.
  • the system comprises at least one electromagnetically operated fuel injector for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas from the engine to assist in atomization of the fuel.
  • the flow of the exhaust gas is caused by the pressure differential between the exhaust gas pressure and the depression in the induction pipe or manifold.
  • the fuel pressure to the injectors is adjusted as a function of the pressure of the exhaust gas to provide compen sation for variations in fuel flow arising from changes in the pressure of the exhaust gas supply.
  • SHEET- 2 OF 2 FUEL INJECTION This invention relates to fuel injection systems.
  • the invention provides a fuel injection system for an internal combustion engine comprising an electromagnetically operated fuel injector for the injection of fuel into the induction pipe or manifold of the engine, and means to provide a supply of exhaust gas from the engine to assist in atomization of said fuel, the flow of said exhaust gas being caused by the pressure difference between the exhaust gas pressure and the depression in the pipe or manifold.
  • the level of the oxides of nitrogen emitted may be reduced to an acceptable value by feeding an inert gas, namely engine exhaust gas into the engine cylinders.
  • the invention therefore also provides, an internal combustion engine having means for feeding an inert gas, namely engine exhaust gas into the engine cylinders.
  • FIG. I shows, somewhat diagrammatically, a part of one embodiment of fuel injection system in accordance with the invention
  • FIGS. 2 to 5 show respectively different modifications to the system of FIG. 1,
  • FIG. 6 illustrates a fuel supply arrangement to a plurality of fuel injectors
  • FIGS. 7 to 9 shows partly in section, views of three embodiments of fuel injector.
  • FIG. 1 there is shown diagrammatically the cylinder head 10 of an internal combustion engine, formed with an induction tract 11, an inlet valve 12 to a cylinder 9,
  • the engine will have a plurality of cylinders, e.g. four or six, each with its own inlet valve.
  • An electromagnetically operated fuel injector 8 of which there may be one provided for each cylinder, located in the region of the inlet valve 12, is formed with an outer sleeve 15, which is attached to the inlet manifold 13, from which sleeve the fuel injector body 16 is supported so that an annular passage 17 is formed around the body.
  • the fuel injector may, for example, be basically constructed as described in U.S. Pat. No. 3,247,833, and supplied with fuel through a fuel passage 18.
  • the fuel injector body 16 has a fuel nozzle 20 which is coaxial with an atomizing nozzle 21 formed in the inner end wall of the sleeve 15, the atomizing nozzle being large enough to allow the nonatomized jet of fuel to enter it, but sufficiently small that the exhaust gas drawn through it from annular passage 17 causes atomization of the fuel, while allowing the engine to idle at a slow speed. It will be seen that the flow of exhaust gas is caused by the difference between the pressure of the exhaust gas at the upstream end of passage I9 and the depression in the inlet manifold 13.
  • the control of exhaust emission is improved and atmospheric pollution, particularly by the oxides of nitrogen, is reduced to an acceptable value.
  • the exhaust gas serves both to assist in atomization of the fuel from the nozzle 20, and also to reduce to an acceptathe engine, since the exhaust gas passing through the atomizing nozzle 21 is inspired into the cylinder through the induction tract 11.
  • FIG. 2 there is shown a modification in which, instead of a plane wall closing off the inner end of sleeve 15, the wall 22 is inwardly-curved, in semitoroidal form, resulting in local reversal of the direction of exhaust gas flow.
  • the inner end of sleeve 15 has a conical tapered part 32, followed by a cylindrical part 33, to give a funnel shape resulting in acceleration of the gas flow towards the atomizing nozzle 21.
  • FIGS. 4 and 5 there are shown embodiments in which heat transfer is obtained from the hot exhaust gas to the fuel, so as to promote vaporization of the fuel.
  • the passage 19 is connected to the downstream end of a sleeve 45, which, with an inner sleeve 46, forms an annular passage 47 through which the heated air or hot exhaust gas flows towards the fuel nozzle 20, where it reverses direction and mixes with the injected fuel, flowing out through an atomizing nozzle 4I formed in the end wall of inner sleeve 46.
  • the atomized fuel passes through the passage 48 within sleeve 46 and the heat exchange through the wall of sleeve 46 increases the vaporization.
  • the arrangement is similar to a that of FIG. 1, except that an extension'tube 55 projects from ble level the emission of oxides of nitrogen from the exhaust of 75 the end of sleeve 15, downstream of nozzle 21, to prolong the time during which the fuel is mixed with the heated exhaust gas, and thus to increase the amount of vaporization.
  • FIG. 6 there is shown diagrammatically a'method of compensating for variations in fuel flow arising from changes in the pressure of the exhaust gas supply in the passage 19.
  • Four fuel injectors 8 are shown which are fed withfuel under pressure from a tank 60, through pump 61 and fuel supply line 62.
  • the pressure in the" supply line 62 is determined by the pressure control valve 63, and excess fuel is bypassed back to the tank through the return line 64.
  • the desired compensation is achieved by subjecting the valve 63 to a reference pressure, which is the same as the pressure in line 65 causing the flow of exhaust gas through passage 19 and the atomizing nozzle.
  • the reference pressure in pipe line 65 decreases, tending to cause change in the rate of fuel delivery, the reference pressure acts on the valve 63 to alter the pressure of the fuel supply to the injectors, in such a way as to provide the desired compensation.
  • the fuel injection systems of the present invention may incorporate other features as described and claimed in US. Pat. No. 3,272,187.
  • FIGS. 7 to 9 show, partly in section, three embodiments of fuel injector for use in the system of the present invention.
  • the injector is electromagnetically operated and is constructed generally in the manner described in US. Pat. No. 3,247,833.
  • the injector is similar to that shown diagrammatically in FIG. 3 and corresponding parts bear the same numerals.
  • Fuel is fed to the valve through the inlet l8and the energizing coil for the electromagnet is shown at 71.
  • the inlet 18 is contained withing a housing 72 which, together with the sleeve or mixing chamber 15, surrounds the injector.
  • the parts 72 and 15 are secured together and the latter serves to supportthe injector from the inlet manifold of the engine.
  • the sleeve 15 has a conical tapered part 32 leading to the atomization nozzle 21.
  • FIG. 8 has an inwardly-curved wall portion 22 similar to that shown in FIG. 2; while the embodiment of FIG. 9 has an extension tube 55 similar to that shown in FIG. 5.
  • the fuel nozzle 20 may have a diameter of 0.020 inches and the atomizing nozzle 21 may have a diameter of 0.052 inches.
  • fuel issuing from the fuel nozzle is entrained in the exhaust gas stream to pass through the atomization nozzle.
  • a fuel injection system for an internal combustion engine including a plurality of electromagnetic-ally operated fuel injectors for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas of the engine to assist in atomization of said fuel, the flow of said exhaust gas being caused by the pressure difference between the exhaust gas pressure and the depression in said induction pipe or manifold, the injectors being fed with fuel under pressure from a fuel supply through a common supply line and including a return line to the fuel supply fed LII

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The present invention relates to a fuel injection system for internal combustion engines. The system comprises at least one electromagnetically operated fuel injector for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas from the engine to assist in atomization of the fuel. The flow of the exhaust gas is caused by the pressure differential between the exhaust gas pressure and the depression in the induction pipe or manifold. The fuel pressure to the injectors is adjusted as a function of the pressure of the exhaust gas to provide compensation for variations in fuel flow arising from changes in the pressure of the exhaust gas supply.

Description

ties Patent [72] Inventors Albert E. lBaxendale Coventry; Brian ll. Croft, Coventry; George E. Fowle, Nuneaton, all of England [21] Appl. No. 835,620 [22] Filed June 23, 1969 [45] Patented Sept. 28, 19711 [73] Assignee Brico Engineering Limited Coventry, England [32] Priority July 4, 1968 [33] Great Britain [31] 32060/68 [54] FUEL INJECTION 1 Claim, 9 Drawing Figs.
[52] 11.5. Cl 1123/1119 A, 123/35, 123/52, 123/133, 123/139 [51] 1111. C1 ..lF02m 25/66 [50] Field otsenrcli 123/1 19 A, 119,119 B, 119 D, 139.17, 139.18, 52 M, 52 MV, 124,127, 35,133
[56] References Cited UNITED STATES PATENTS 2,511,213 6/1950 Leslie ..l23/l39.18UX
W m 15 n Primary Examiner-Wendell E. Burns Art0rneyl-lo1combe, Wetherill & Brisebois ABT1RACT: The present invention relates to a fuel injection system for internal combustion engines. The system comprises at least one electromagnetically operated fuel injector for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas from the engine to assist in atomization of the fuel. The flow of the exhaust gas is caused by the pressure differential between the exhaust gas pressure and the depression in the induction pipe or manifold. The fuel pressure to the injectors is adjusted as a function of the pressure of the exhaust gas to provide compen sation for variations in fuel flow arising from changes in the pressure of the exhaust gas supply.
PATENTED was 197: 3508.531
SHEET- 2 OF 2 FUEL INJECTION This invention relates to fuel injection systems.
The invention provides a fuel injection system for an internal combustion engine comprising an electromagnetically operated fuel injector for the injection of fuel into the induction pipe or manifold of the engine, and means to provide a supply of exhaust gas from the engine to assist in atomization of said fuel, the flow of said exhaust gas being caused by the pressure difference between the exhaust gas pressure and the depression in the pipe or manifold.
One problem, which is encountered at present in the design of fuel metering systems for internal combustion engines of motor vehicles, is to ensure that the composition of the exhaust gas does not produce unacceptable atmospheric pollution.
It has been possible to design fuel metering systems which give acceptable levels of unbumt hydrocarbons and of carbon monoxide in the exhaust gas, without the necessity to resort to catalytic or combustion processes in the exhaust system. 7
However such fuel metering systems tend to operate successfully by metering a fuel quantity which gives a weak fuel/air ratio, and this in turn may result in the emission of an unacceptable quantity of the oxides of nitrogen in the exhaust gas.
We have found that the level of the oxides of nitrogen emitted may be reduced to an acceptable value by feeding an inert gas, namely engine exhaust gas into the engine cylinders.
The invention therefore also provides, an internal combustion engine having means for feeding an inert gas, namely engine exhaust gas into the engine cylinders.
The invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. I shows, somewhat diagrammatically, a part of one embodiment of fuel injection system in accordance with the invention,
FIGS. 2 to 5 show respectively different modifications to the system of FIG. 1,
FIG. 6 illustrates a fuel supply arrangement to a plurality of fuel injectors; and
FIGS. 7 to 9, shows partly in section, views of three embodiments of fuel injector.
Referring to FIG. 1, there is shown diagrammatically the cylinder head 10 of an internal combustion engine, formed with an induction tract 11, an inlet valve 12 to a cylinder 9,
and an inlet manifold 13, in well-known fashion. It will be understood that generally the engine will have a plurality of cylinders, e.g. four or six, each with its own inlet valve.
An electromagnetically operated fuel injector 8, of which there may be one provided for each cylinder, located in the region of the inlet valve 12, is formed with an outer sleeve 15, which is attached to the inlet manifold 13, from which sleeve the fuel injector body 16 is supported so that an annular passage 17 is formed around the body. The fuel injector may, for example, be basically constructed as described in U.S. Pat. No. 3,247,833, and supplied with fuel through a fuel passage 18.
A supply of inert gas, namely exhaust gas, is led from the exhaust system of the engine (not shown) through passage 19 to the annular passage 17. The fuel injector body 16 has a fuel nozzle 20 which is coaxial with an atomizing nozzle 21 formed in the inner end wall of the sleeve 15, the atomizing nozzle being large enough to allow the nonatomized jet of fuel to enter it, but sufficiently small that the exhaust gas drawn through it from annular passage 17 causes atomization of the fuel, while allowing the engine to idle at a slow speed. It will be seen that the flow of exhaust gas is caused by the difference between the pressure of the exhaust gas at the upstream end of passage I9 and the depression in the inlet manifold 13. By injecting inert exhaust gas as just described, the control of exhaust emission is improved and atmospheric pollution, particularly by the oxides of nitrogen, is reduced to an acceptable value. The exhaust gas serves both to assist in atomization of the fuel from the nozzle 20, and also to reduce to an acceptathe engine, since the exhaust gas passing through the atomizing nozzle 21 is inspired into the cylinder through the induction tract 11.
Referring now to FIG. 2, there is shown a modification in which, instead of a plane wall closing off the inner end of sleeve 15, the wall 22 is inwardly-curved, in semitoroidal form, resulting in local reversal of the direction of exhaust gas flow.
In the modification shown in FIG. 3, instead of a plane wall, the inner end of sleeve 15 has a conical tapered part 32, followed by a cylindrical part 33, to give a funnel shape resulting in acceleration of the gas flow towards the atomizing nozzle 21.
In FIGS. 4 and 5 there are shown embodiments in which heat transfer is obtained from the hot exhaust gas to the fuel, so as to promote vaporization of the fuel. In FIG. 4, the passage 19 is connected to the downstream end of a sleeve 45, which, with an inner sleeve 46, forms an annular passage 47 through which the heated air or hot exhaust gas flows towards the fuel nozzle 20, where it reverses direction and mixes with the injected fuel, flowing out through an atomizing nozzle 4I formed in the end wall of inner sleeve 46.
The atomized fuel passes through the passage 48 within sleeve 46 and the heat exchange through the wall of sleeve 46 increases the vaporization.
In the embodiment of FIG. 5, the arrangement is similar to a that of FIG. 1, except that an extension'tube 55 projects from ble level the emission of oxides of nitrogen from the exhaust of 75 the end of sleeve 15, downstream of nozzle 21, to prolong the time during which the fuel is mixed with the heated exhaust gas, and thus to increase the amount of vaporization.
In FIG. 6 there is shown diagrammatically a'method of compensating for variations in fuel flow arising from changes in the pressure of the exhaust gas supply in the passage 19. Four fuel injectors 8 are shown which are fed withfuel under pressure from a tank 60, through pump 61 and fuel supply line 62. The pressure in the" supply line 62 is determined by the pressure control valve 63, and excess fuel is bypassed back to the tank through the return line 64. The desired compensation is achieved by subjecting the valve 63 to a reference pressure, which is the same as the pressure in line 65 causing the flow of exhaust gas through passage 19 and the atomizing nozzle. Thus, as the reference pressure in pipe line 65 decreases, tending to cause change in the rate of fuel delivery, the reference pressure acts on the valve 63 to alter the pressure of the fuel supply to the injectors, in such a way as to provide the desired compensation.
The fuel injection systems of the present invention may incorporate other features as described and claimed in US. Pat. No. 3,272,187.
FIGS. 7 to 9 show, partly in section, three embodiments of fuel injector for use in the system of the present invention. In each case, the injector is electromagnetically operated and is constructed generally in the manner described in US. Pat. No. 3,247,833. a
In the embodiment of FIG. 7, the injector is similar to that shown diagrammatically in FIG. 3 and corresponding parts bear the same numerals. Fuel is fed to the valve through the inlet l8and the energizing coil for the electromagnet is shown at 71. The inlet 18 is contained withing a housing 72 which, together with the sleeve or mixing chamber 15, surrounds the injector. The parts 72 and 15 are secured together and the latter serves to supportthe injector from the inlet manifold of the engine. The sleeve 15 has a conical tapered part 32 leading to the atomization nozzle 21.
The embodiment of FIG. 8 has an inwardly-curved wall portion 22 similar to that shown in FIG. 2; while the embodiment of FIG. 9 has an extension tube 55 similar to that shown in FIG. 5.
In each embodiment of injector, the fuel nozzle 20 may have a diameter of 0.020 inches and the atomizing nozzle 21 may have a diameter of 0.052 inches. Thus fuel issuing from the fuel nozzle is entrained in the exhaust gas stream to pass through the atomization nozzle.
We claim:
l. A fuel injection system for an internal combustion engine, including a plurality of electromagnetic-ally operated fuel injectors for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas of the engine to assist in atomization of said fuel, the flow of said exhaust gas being caused by the pressure difference between the exhaust gas pressure and the depression in said induction pipe or manifold, the injectors being fed with fuel under pressure from a fuel supply through a common supply line and including a return line to the fuel supply fed LII

Claims (1)

1. A fuel injection system for an internal combustion engine, including a plurality of electromagnetically operated fuel injectors for the injection of fuel into the induction pipe or manifold of the engine and means to provide a supply of exhaust gas of the engine to assist in atomization of said fuel, the flow of said exhaust gas being caused by the pressure difference between the exhaust gas pressure and the depression in said induction pipe or manifold, the injectors being fed with fuel under pressure from a fuel supply through a common supply line and including a return line to the fuel supply fed through a pressure control valve which determines the fuel pressure in said supply line, wherein the pressure control valve is also subjected to a reference pressure which is the same as the pressure of the exhaust gas fed to the injectors, whereby the reference pressure acts on the pressure control valve to alter the pressure of the fuel supply to the injectors in such a way as to provide compensation for variations in fuel flow arising from changes in the pressure of the exhaust gas supply.
US835620A 1968-07-04 1969-06-23 Fuel injection Expired - Lifetime US3608531A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3206068 1968-07-04
GB38743/68A GB1270945A (en) 1968-07-04 1968-07-04 Improvements in fuel injection systems for internal combustion engines

Publications (1)

Publication Number Publication Date
US3608531A true US3608531A (en) 1971-09-28

Family

ID=26261191

Family Applications (1)

Application Number Title Priority Date Filing Date
US835620A Expired - Lifetime US3608531A (en) 1968-07-04 1969-06-23 Fuel injection

Country Status (5)

Country Link
US (1) US3608531A (en)
DE (1) DE1933514A1 (en)
FR (1) FR2012294A1 (en)
GB (1) GB1270945A (en)
SE (1) SE349846B (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3789819A (en) * 1972-01-28 1974-02-05 Gen Motors Corp Fuel rail vapor bleed
US3868936A (en) * 1971-03-19 1975-03-04 Renault Fuel injection systems
US3894520A (en) * 1974-03-13 1975-07-15 Thermo Electron Corp Charge forming device with fuel vaporization
US3977374A (en) * 1972-05-02 1976-08-31 Paul August Arrangement for the preparation of the fuel-air mixture for an internal combustion engine
JPS51147822U (en) * 1975-05-21 1976-11-27
US4159703A (en) * 1976-12-10 1979-07-03 The Bendix Corporation Air assisted fuel atomizer
US4257376A (en) * 1978-08-17 1981-03-24 The Bendix Corporation Single injector, single point fuel injection system
US4787343A (en) * 1986-11-07 1988-11-29 Walbro Corporation Combustion enhancer for internal combustion engines
US5044339A (en) * 1989-03-11 1991-09-03 Robert Bosch Gmbh Fuel injection system for internal combustion engines
US5082184A (en) * 1986-05-02 1992-01-21 General Motors Corporation Fuel injection
US20050081833A1 (en) * 2002-03-22 2005-04-21 Pellizzari Roberto O. Capillary fuel injector with metering valve for an internal combustion engine
US20220042484A1 (en) * 2020-08-10 2022-02-10 Ford Global Technologies, Llc Methods and systems for a ducted injector

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5440915A (en) * 1977-09-07 1979-03-31 Toyota Motor Corp Internal combution engine
DE2930737C2 (en) * 1979-07-28 1983-10-20 Bosch und Pierburg System oHG, 4040 Neuss Constant pressure carburettor
DE2936426A1 (en) * 1979-09-08 1981-04-02 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION VALVE
US4601275A (en) * 1982-08-23 1986-07-22 General Motors Corporation Fuel rail
DE3240554C2 (en) * 1982-11-03 1993-10-07 Bosch Gmbh Robert Fuel injection valve for an internal combustion engine
US4570598A (en) * 1985-04-15 1986-02-18 Ford Motor Company Air assist fuel distributor type fuel injection system
CA1292651C (en) * 1986-05-02 1991-12-03 Ernest R. Stettner Fuel injection
SE8604448D0 (en) * 1986-10-20 1986-10-20 John Olsson DEVICE FOR COMBUSTION ENGINES
DE3841088A1 (en) * 1988-12-07 1990-06-21 Mesenich Gerhard FUEL INJECTION DEVICE WITH AIR SUPPORTED FUEL SPRAYING
US5241938A (en) * 1990-03-14 1993-09-07 Aisan Kogyo Kabushiki Kaisha Injector with assist air passage for atomizing fuel
US5255658A (en) * 1990-10-12 1993-10-26 Coltec Industries Inc. System and apparatus to improve atomization of injected fuel
SE502371C2 (en) * 1991-07-10 1995-10-09 Volvo Ab Device for suction engine combustion systems
GB2263309A (en) * 1992-01-16 1993-07-21 Ford Motor Co Mixing injected fuel with air in an ic engine intake.
DE4422331B4 (en) * 1993-07-08 2005-12-08 Volkswagen Ag Device for air-assisted fuel injection into a suction pipe
KR20020081526A (en) * 2001-04-18 2002-10-28 한국기계연구원 Exhaust gas assisted fuel injection system of internal combustion engine

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511213A (en) * 1945-04-26 1950-06-13 Stewart Warner Corp Carbureting apparatus
US2833260A (en) * 1955-05-31 1958-05-06 Gen Motors Corp Atmospheric vent for fuel injection nozzle
US2860617A (en) * 1957-06-21 1958-11-18 Gen Motors Corp Enrichment device for fuel injection system
US2874944A (en) * 1957-06-05 1959-02-24 Gen Motors Corp Charge forming means
US2893365A (en) * 1956-05-31 1959-07-07 Gen Motors Corp Fuel injection means
US2969784A (en) * 1958-03-13 1961-01-31 Borg Warner Fuel injection mechanism
US3182646A (en) * 1961-06-15 1965-05-11 Kuechenmeister Craig Alfred Air-bled coaxial injector
US3247833A (en) * 1962-12-03 1966-04-26 Ass Eng Ltd Fuel injection valves
US3330541A (en) * 1964-02-25 1967-07-11 Petrol Injection Ltd Fuel injector devices and systems
US3416503A (en) * 1967-10-27 1968-12-17 Carl F. High Engine fume discharge reduction systems

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511213A (en) * 1945-04-26 1950-06-13 Stewart Warner Corp Carbureting apparatus
US2833260A (en) * 1955-05-31 1958-05-06 Gen Motors Corp Atmospheric vent for fuel injection nozzle
US2893365A (en) * 1956-05-31 1959-07-07 Gen Motors Corp Fuel injection means
US2874944A (en) * 1957-06-05 1959-02-24 Gen Motors Corp Charge forming means
US2860617A (en) * 1957-06-21 1958-11-18 Gen Motors Corp Enrichment device for fuel injection system
US2969784A (en) * 1958-03-13 1961-01-31 Borg Warner Fuel injection mechanism
US3182646A (en) * 1961-06-15 1965-05-11 Kuechenmeister Craig Alfred Air-bled coaxial injector
US3247833A (en) * 1962-12-03 1966-04-26 Ass Eng Ltd Fuel injection valves
US3330541A (en) * 1964-02-25 1967-07-11 Petrol Injection Ltd Fuel injector devices and systems
US3416503A (en) * 1967-10-27 1968-12-17 Carl F. High Engine fume discharge reduction systems

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3868936A (en) * 1971-03-19 1975-03-04 Renault Fuel injection systems
US3789819A (en) * 1972-01-28 1974-02-05 Gen Motors Corp Fuel rail vapor bleed
US3977374A (en) * 1972-05-02 1976-08-31 Paul August Arrangement for the preparation of the fuel-air mixture for an internal combustion engine
US3894520A (en) * 1974-03-13 1975-07-15 Thermo Electron Corp Charge forming device with fuel vaporization
JPS51147822U (en) * 1975-05-21 1976-11-27
US4159703A (en) * 1976-12-10 1979-07-03 The Bendix Corporation Air assisted fuel atomizer
US4257376A (en) * 1978-08-17 1981-03-24 The Bendix Corporation Single injector, single point fuel injection system
US5082184A (en) * 1986-05-02 1992-01-21 General Motors Corporation Fuel injection
US4787343A (en) * 1986-11-07 1988-11-29 Walbro Corporation Combustion enhancer for internal combustion engines
US5044339A (en) * 1989-03-11 1991-09-03 Robert Bosch Gmbh Fuel injection system for internal combustion engines
US20050081833A1 (en) * 2002-03-22 2005-04-21 Pellizzari Roberto O. Capillary fuel injector with metering valve for an internal combustion engine
US7137383B2 (en) * 2002-03-22 2006-11-21 Philip Morris Usa Inc. Capillary fuel injector with metering valve for an internal combustion engine
US20220042484A1 (en) * 2020-08-10 2022-02-10 Ford Global Technologies, Llc Methods and systems for a ducted injector
US11480143B2 (en) * 2020-08-10 2022-10-25 Ford Global Technologies, Llc Methods and systems for a ducted injector

Also Published As

Publication number Publication date
FR2012294A1 (en) 1970-03-20
DE1933514A1 (en) 1970-01-08
GB1270945A (en) 1972-04-19
SE349846B (en) 1972-10-09

Similar Documents

Publication Publication Date Title
US3608531A (en) Fuel injection
US3782639A (en) Fuel injection apparatus
US3868936A (en) Fuel injection systems
US4361126A (en) Fuel injection valve
US5323966A (en) Apparatus for injecting a fuel-air mixture
US3680534A (en) Device for the injection of gases into the feed system of an internal combustion engine
US3931814A (en) Cylinder-induction responsive electronic fuel feed control carburetors
US4532906A (en) Fuel supply system
US4194474A (en) EGR Recirculation at low load in internal combustion engines
US3610213A (en) Fuel injection system
JPS6056908B2 (en) Fuel control device for fuel injection system
US3944634A (en) Carburetor idling system
JPS61237882A (en) Internal combustion engine fuel supply system
JP2002531743A (en) A device for feeding a reducing agent into an exhaust pipe section of an internal combustion engine
US4351304A (en) Fuel injection valve
US4387695A (en) Fuel injection apparatus
US3680794A (en) Electromagnetically operated fuel injection valve
US4292945A (en) Fuel injection apparatus and system
US4235210A (en) Fuel supply apparatus for internal combustion engines
US5255658A (en) System and apparatus to improve atomization of injected fuel
US3656464A (en) Fuel injection nozzle and system
US3498274A (en) Fuel injector for internal combustion engines
US5197672A (en) Fuel injection valve and adjustable gas sleeve forming an annular metering gas gap
US3587541A (en) Engine exhaust recirculation
US4406266A (en) Fuel metering and discharging apparatus for a combustion engine