[go: up one dir, main page]

US3682146A - System of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines - Google Patents

System of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines Download PDF

Info

Publication number
US3682146A
US3682146A US120844A US3682146DA US3682146A US 3682146 A US3682146 A US 3682146A US 120844 A US120844 A US 120844A US 3682146D A US3682146D A US 3682146DA US 3682146 A US3682146 A US 3682146A
Authority
US
United States
Prior art keywords
fuel
tank
pump
piston
valve
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
US120844A
Inventor
Nikolai G Mozokhin
Konstantin Mikhailo Maskenskov
Niyazi Abdulkasim Ogly Kerimov
Zuleikha Ismial Kyzy Guseinova
Rafik Isrofil Ogly Mekhtiev
Garri Voldemarovich Evart
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.)
GO AUTOMOBILNY Z
GORKOVSKY AUTOMOBILNY ZAVOD
Original Assignee
GO AUTOMOBILNY Z
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 GO AUTOMOBILNY Z filed Critical GO AUTOMOBILNY Z
Application granted granted Critical
Publication of US3682146A publication Critical patent/US3682146A/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
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00Engines characterised by precombustion chambers
    • F02B19/10Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
    • F02B19/1019Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber
    • F02B19/108Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber with fuel injection at least into pre-combustion chamber, i.e. injector mounted directly in the pre-combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3094Controlling fuel injection the fuel injection being effected by at least two different injectors, e.g. one in the intake manifold and one in the cylinder
    • 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
    • F02M67/00Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type
    • 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
    • F02B2720/25Supply of fuel in the cylinder
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • ABSTRACT A system of fuel injection and precombustionchamber spray ignition in piston and rotary-piston internal combustion engines is provided with a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a jet pump connected to a tank filled with fuel that is provided with a device for maintaining a preset level in it.
  • the tank and the jet pump are connected to the combustion chamber of the engine by a duct in which a shut-off valve is installed for tapping gas from the combustion chamber to the jet pump and tank, the valve having a drive functioning synchronously with the delivery of fuel by the fuel pump.
  • the present invention relates to systems of fuel delivery and controlling engine duty used in piston and rotary-piston internal combustion engines.
  • a system of fuel injection and precombustion-chamber spray injection in piston and rotary-piston internal combustion engines comprising a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a fuel atomizer arranged in the inlet pipe.
  • the known system of fuel injection does not make it possible to use increased compression ratios of the mixture in the combustion chamber, as such ratios could lead to detonation during combustion of the mixture, which limits the possibility of effective qualitative control of all the working duties of the engine.
  • An object of the present invention is to provide such a system of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines that would ensure qualitative control of all the engine working duties with the use of a high compression ratio of the mixture, with its following automatic reduction as the load on the engine grows.
  • a system of fuel injection and precombustion-chamber spray injection in piston and rotarypiston internal combustion engines comprising a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a fuel atomizer disposed in the inlet pipe of the engine, wherein, according to the invention, the atomizer is a jet pump connected to a tank filled with fuel that isprovided with a device for maintaining a preset level of the fuel in it, and the said tank is connected to the combustion chamber of the engine by means of a duct in which there is installed a shut-off valve equipped with a drive that operates synchronously with delivery of the fuel by the fuel pump, the valve being designed for tapping gas from the combustion chamber into the jet pump and tank and simultaneously for changing the compression ratio of the mixture depending on the engine duty.
  • the jet pump of the system is an atomizer whose inner fuel-feeding tube has one and end immersed in the fuel contained in the tank.
  • the device for maintaining the preset level of the fuel in the tank is a float closing the outlet orifice of the pipe feeding the fuel at a preset level of the latter, a non-return valve being installed in the pipe.
  • the shut-off valve is spring-loaded and is operated by a piston valve pusher that moves under the pressure of the fuel fed to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.
  • the proposed system ensures qualitative control of all the working duties of the engine even when using low-octane fuels by providing the possibility of using a high compression ratio of the mixture with its following automatic reduction as the load on the engine grows.
  • the automatic reduction of the compression ratio of the mixture by partial removing of the gases from the combustion chamber while retaining a constant geometrical compression ratio of the engine excludes the possibility of detonation combustion at high load duties at which the composition of the mixture in the main combustion chamber is the most dangerous from the viewpoint of detonation.
  • the change in the supply of the part of the fuel fed into the main combustion chamber depending on engine operation is automatically set by using the jet pump, which functions under the action of the gas delivered to the tank from the combustion chamber.
  • the system shown in the drawing comprises fuel pump 1 connected by means of pipe 2 to nozzle 3 installed in precombustion chamber 4 of combustion chamber 5 of the engine, chamber 5 consisting of precombustion chamber 4 and main chamber 6.
  • Spark plug 7 is installed in precombustion chamber 4 for ignition of an enriched mixture.
  • jet pump 9 for atomization of the fuel that comprises an atomizer whose atomizing part 10 is disposed in inlet pipe 8.
  • Atomizer 9 is connected to tank 11 containing fuel by means of fuel delivery tube 12, one end of which is immersed in the fuel contained in tank 1 l.
  • the preset level of fuel is maintained in tank 1 l by means of a device comprising float 13 carrying closing needle 14 that shuts the outlet orifice of pipe 15 supplying the fuel.
  • Pipe 15 contains a non-return valve 16 for closing its outlet orifice when gas is being fed into tank 1 1.
  • Tank 11 and jet pump 9 are connected to combustion chamber 5 by means of duct 17 in which shutoff valve 18 is installed.
  • Valve 18 is actuated by drive 19 and is designed for tapping the gas from combustion chamber into jet pump 9 and tank 11.
  • Drive 19 comprises piston valve pusher 20 that moves under the action of the pressure of the fuel supplied from fuel pump loaded by spring 26.
  • Fuel from the fuel tank (not shown in the drawing) is supplied by a fuel-feed pump (not shown in the drawing) after filtration along pipes 15 and 24 into tank 11 and fuel pump 1, respectively.
  • pump 1 delivers the fuel along pipe 2 into nozzle 3, and also along pipes 2 and 21 to drive 19 of shut-off valve 18.
  • needle 14 of float 13 opens the inlet orifice of tank 11 and fills it with fuel to the preset level. When the fuel reaches the given level, needle 14 again closes the inlet orifice, stopping the supply of fuel into tank 11.
  • shut-off valve 18 grows.
  • a system of fuel injection and precombustionchamber spray ignition in piston and rotary-piston internal combustion engines comprising a fuel pump; a nozzle disposed in the precombustion chamber of the engine and connected to said fuel pump; a tank filled with fuel and connected by means of a duct to said engine combustion chamber; a device for maintaining a preset level of fuel in said tank; a jet pump installed in the inlet pipe of said engine and connected to said tank, designed for injecting fuel into said inlet pipe; a shut-off valve disposed in said duct connecting the tank to the combustion chamber and designed for tapping gas from the combustion chamber into the tank and simultaneously for changing the compression ratio of the mixture depending on the engine duty; the gas, flowing into said tank under pressure, facilitates the suction of fuel into said jet pump and its injection into the combustion chamber; means for actuating said shut-off valve functioning synchronously with the delivery of fuel by the said fuel pump.
  • jet pump comprises an atomizer whose inner fuel delivery tube has one end immersed in the fuel contained in the tank.
  • a system as claimed in claim 1, wherein the device for maintaining the preset level of the fuel in the tank comprises a float closing the outlet orifice of the pipe supplying fuel at its preset level, a non-retum valve being installed in the pipe.
  • shutoff valve is spring-loaded and is'actuated by a piston valve pusher moving under the action of the fuel delivered to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

A system of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines is provided with a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a jet pump connected to a tank filled with fuel that is provided with a device for maintaining a preset level in it. The tank and the jet pump are connected to the combustion chamber of the engine by a duct in which a shut-off valve is installed for tapping gas from the combustion chamber to the jet pump and tank, the valve having a drive functioning synchronously with the delivery of fuel by the fuel pump.

Description

United States Patent Mozokhin et al.
[ 51 Aug. 8, 1972 [54]v SYSTEM OF FUEL INJECTION AND PRECOMBUSTION-CHANEER SPRAY IGNITION IN PISTON AND ROTARY- PISTON INTERNAL COMBUSTION ENGINES U.S.S.R.
[73] Assignee: Gorkovsky Automobilny Zavod,
' Gorky, U.S.S.R.
[22] Filed: March 4,1971
[21] Appl. No.: 120,844
[52] US. Cl. ..123/32 SP, 123/32 ST, 123/119 A, 123/139 AJ, 123/139 AW [58] Field of Search ..F02b/3/00; 123/8.l3, 32 SP, 123/32 ST, 139 AJ, 139 AW, 119 A;
[56] References Cited UNITED STATES PATENTS 1,588,885 6/1926 Hart ..60/39.48
1,737,813 12/1929 Tice 123/32 SP 1,953,808 4/1934 Kenneweg ..60/39.48 2,766,582 10/1956 Smith ..123/32 SP 2,816,533 12/1957 Reggio ..123/l39 AL 2,849,992 9/ 1958 Stillebroer et a1. 123/32 SP 2,914,043 11/1959 Mallinger ..123/32 SP 3,443,552 5/1969 Von Seggem et al. .123/32 ST Primary Examiner -C. J. l-lusar Attorney-Waters, Roditi, Schwartz & Nissen [5 7] ABSTRACT A system of fuel injection and precombustionchamber spray ignition in piston and rotary-piston internal combustion engines is provided with a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a jet pump connected to a tank filled with fuel that is provided with a device for maintaining a preset level in it.'The tank and the jet pump are connected to the combustion chamber of the engine by a duct in which a shut-off valve is installed for tapping gas from the combustion chamber to the jet pump and tank, the valve having a drive functioning synchronously with the delivery of fuel by the fuel pump.
4 Claims, 1 Drawing figure The present invention relates to systems of fuel delivery and controlling engine duty used in piston and rotary-piston internal combustion engines.
Known in the art is a system of fuel injection and precombustion-chamber spray injection in piston and rotary-piston internal combustion engines comprising a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a fuel atomizer arranged in the inlet pipe.
The known system of fuel injection does not make it possible to use increased compression ratios of the mixture in the combustion chamber, as such ratios could lead to detonation during combustion of the mixture, which limits the possibility of effective qualitative control of all the working duties of the engine.
No provision is made in the known systems for automatic reduction of the amount of fuel fed into the precombustion chamber as the load on the engine grows. This may lead to too great overenrichment of the mixture in the precombustion chamber and reduce to zero the effect of precombustion-chamber spray igmtion.
In the known systems, economical operation of the engine is ensured when the load drops by using a rich mixture at the expense of quantitative control of the working duties, which leads to a poorer performance of the engine working cycle and a growth of the toxicity of the exhaust gases, and also to a more intricate system of controlling the engine working duties, namely, to the installation of an additional automatic device for controlling the quality of the mixture.
An object of the present invention is to provide such a system of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines that would ensure qualitative control of all the engine working duties with the use of a high compression ratio of the mixture, with its following automatic reduction as the load on the engine grows.
It is proposed a system of fuel injection and precombustion-chamber spray injection in piston and rotarypiston internal combustion engines comprising a nozzle disposed in the precombustion chamber of the engine and connected to a fuel pump, and a fuel atomizer disposed in the inlet pipe of the engine, wherein, according to the invention, the atomizer is a jet pump connected to a tank filled with fuel that isprovided with a device for maintaining a preset level of the fuel in it, and the said tank is connected to the combustion chamber of the engine by means of a duct in which there is installed a shut-off valve equipped with a drive that operates synchronously with delivery of the fuel by the fuel pump, the valve being designed for tapping gas from the combustion chamber into the jet pump and tank and simultaneously for changing the compression ratio of the mixture depending on the engine duty.
The jet pump of the system is an atomizer whose inner fuel-feeding tube has one and end immersed in the fuel contained in the tank.
The device for maintaining the preset level of the fuel in the tank is a float closing the outlet orifice of the pipe feeding the fuel at a preset level of the latter, a non-return valve being installed in the pipe.
The shut-off valveis spring-loaded and is operated by a piston valve pusher that moves under the pressure of the fuel fed to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.
The proposed system ensures qualitative control of all the working duties of the engine even when using low-octane fuels by providing the possibility of using a high compression ratio of the mixture with its following automatic reduction as the load on the engine grows.
The possibility of using effective qualitative control ensures high fuel economy in the engine, appreciably reduces the toxicity of the exhaust gases and simplifies the system of controlling the engine duties, eliminating the use of an automatic device for controlling the quality of the mixture.
As the engine load grows, the automatic reduction of the compression ratio of the mixture by partial removing of the gases from the combustion chamber while retaining a constant geometrical compression ratio of the engine excludes the possibility of detonation combustion at high load duties at which the composition of the mixture in the main combustion chamber is the most dangerous from the viewpoint of detonation.
In the proposed system, provision is made for automatic reduction of the supply of the precombustion chamber part of the fuel by bypassing part of it with the aid of the piston valve pusher into the inlet system of the fuel pump, thus ensuring an almost constant easily flammable enriched composition of the mixture in the precombustion chamber and retaining the precombustion-chamber and spray effect at any engine duties.
In addition, the change in the supply of the part of the fuel fed into the main combustion chamber depending on engine operation is automatically set by using the jet pump, which functions under the action of the gas delivered to the tank from the combustion chamber.
The nature of the present invention will become more fully apparent from a consideration of the following detailed description of an exemplary embodiment thereof, taken in conjunction with the accompanying drawing.
The system shown in the drawing comprises fuel pump 1 connected by means of pipe 2 to nozzle 3 installed in precombustion chamber 4 of combustion chamber 5 of the engine, chamber 5 consisting of precombustion chamber 4 and main chamber 6.
Spark plug 7 is installed in precombustion chamber 4 for ignition of an enriched mixture.
At inlet pipe 8 of the engine there is installed jet pump 9 for atomization of the fuel that comprises an atomizer whose atomizing part 10 is disposed in inlet pipe 8. Atomizer 9 is connected to tank 11 containing fuel by means of fuel delivery tube 12, one end of which is immersed in the fuel contained in tank 1 l. The preset level of fuel is maintained in tank 1 l by means of a device comprising float 13 carrying closing needle 14 that shuts the outlet orifice of pipe 15 supplying the fuel.
Pipe 15 contains a non-return valve 16 for closing its outlet orifice when gas is being fed into tank 1 1.
Tank 11 and jet pump 9 are connected to combustion chamber 5 by means of duct 17 in which shutoff valve 18 is installed. Valve 18 is actuated by drive 19 and is designed for tapping the gas from combustion chamber into jet pump 9 and tank 11. Drive 19 comprises piston valve pusher 20 that moves under the action of the pressure of the fuel supplied from fuel pump loaded by spring 26.
The system functions as follows;
Fuel from the fuel tank (not shown in the drawing) is supplied by a fuel-feed pump (not shown in the drawing) after filtration along pipes 15 and 24 into tank 11 and fuel pump 1, respectively.
During the compression stroke, pump 1 delivers the fuel along pipe 2 into nozzle 3, and also along pipes 2 and 21 to drive 19 of shut-off valve 18.
During starting, idle running and low loads of the engine, the entire cycle portion of fuel supplied by pump 1 is injected by means of nozzle 3 into precombustion chamber 4, where in all duties there is formed an enriched mixture that is easily ignited by spark plug 7,
Upon an increase in the amount of fuel delivered by pump 1, the pressure in pipes 2 and 21 will grow owing to the limited capacity of nozzle 3. As a result piston valve pusher 20, overcoming the resistance of spring 26 and the pressure of the gases in combustion chamber 5, opens shut-off valve 18 and bypass port 22. Compressed gas from combustion chamber 5 through duct 17 flows into atomizer 9 and tank 11 and exerts pressure on the fuel in it. Non-return valve 16 closes pipe 15.
Under the pressure of the gas flowing into jet pump 9 and tank 11, the fuel rising along tube 12 into atomizer 9, sucked into it-by the stream of gases, is injected by atomizing part of the atomizer into inlet pipe 8 of the engine.
As the fuel is consumed from tank 11, needle 14 of float 13 opens the inlet orifice of tank 11 and fills it with fuel to the preset level. When the fuel reaches the given level, needle 14 again closes the inlet orifice, stopping the supply of fuel into tank 11.
As the amount of fuel supplied by pump 1 increases, the excess fuel through port 22 and pipe 23 is discharged into the pipe 24 feeding fuel to fuel pipe 1. With an increase in the duration of fuel delivery by pump 1 the"time-section of shut-off valve 18 grows.
With a growth. in the load on the engine, the amount of fuel passing through atomizer 9 increases, and through nozzle 3 decreases, retaining the optimal enriched composition of the mixture in precombustion chamber 4, and it is this that ensures the precomloads on the engine at which a too lean mixture in main combustion chamber 6 prevents any possibility of detonation appearing during combustion of the mixture.
When pump 1 stops delivering fuel, the pressure of the fuel in pipes 2 and 21 decreases, nozzle 3 stops injecting fuel into precombustion chamber 4, and piston valve pusher 20 and shut-off valve 18 under the action ttsra asta saa mattresses ing the entrance to duct 17 and part 22. As a result operation of atomizer 9 stops.
Thus, by changing only the position of the control I member (not shown in the drawing) of pump l,-the optimal compositions of the mixture in combustion chamber 5 are ensured, and also the required compression ratio of the mixture. The above underlies the achievement of qualitative control of all the engine working duties.
What we claim is:
l. A system of fuel injection and precombustionchamber spray ignition in piston and rotary-piston internal combustion engines, comprising a fuel pump; a nozzle disposed in the precombustion chamber of the engine and connected to said fuel pump; a tank filled with fuel and connected by means of a duct to said engine combustion chamber; a device for maintaining a preset level of fuel in said tank; a jet pump installed in the inlet pipe of said engine and connected to said tank, designed for injecting fuel into said inlet pipe; a shut-off valve disposed in said duct connecting the tank to the combustion chamber and designed for tapping gas from the combustion chamber into the tank and simultaneously for changing the compression ratio of the mixture depending on the engine duty; the gas, flowing into said tank under pressure, facilitates the suction of fuel into said jet pump and its injection into the combustion chamber; means for actuating said shut-off valve functioning synchronously with the delivery of fuel by the said fuel pump.
2. A system as claimed in claim 1, wherein the jet pump comprises an atomizer whose inner fuel delivery tube has one end immersed in the fuel contained in the tank.
3. A system as claimed in claim 1, wherein the device for maintaining the preset level of the fuel in the tank comprises a float closing the outlet orifice of the pipe supplying fuel at its preset level, a non-retum valve being installed in the pipe.
4. A system as claimed in claim 1, wherein the shutoff valve is spring-loaded and is'actuated by a piston valve pusher moving under the action of the fuel delivered to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.

Claims (7)

1. A system of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines, comprising a fuel pump; a nozzle disposed in the precombustion chamber of the engine and connected to said fuel pump; a tank filled with fuel and connected by means of a duct to said engine combustion chamber; a device for maintaining a preset level of fuel in said tank; a jet pump installed in the inlet pipe of said engine and connected to said tank, designed for injecting fuel into said inlet pipe; a shut-off valve disposed in said duct connecting the tank to the combustion chamber and designed for tapping gas from the combustion chamber into the tank and simultaneously for changing the compression ratio of the mixture depending on the engine duty; the gas, flowing into said tank under pressure, facilitates the suction of fuel into said jet pump and its injection into the combustion chamber; means for actuating said shut-off valve functioning synchronously with the delivery of fuel by the said fuel pump.
2. A system as claimed in claim 1, wherein the jet pump comprises an atomizer whose inner fuel delivery tube has one end immersed in the fuel contained in the tank.
2. A system as claimed in claim 1, wherein the jet pump comprises an atomizer whose inner fuel delivery tube has one end immersed in the fuel contained in the tank.
3. A system as claimed in claim 1, wherein the device for maintaining the preset level of the fuel in the tank comprises a float closing the outlet orifice of the pipe supplying fuel at its preset level, a non-return valve being installed in the pipe.
3. A system as claimed in claim 1, wherein the device for maintaining the preset level of the fuel in the tank comprises a float closing the outlet orifice of the pipe supplying fuel at its preset level, a non-return valve being installed in the pipe.
4. A system as claimed in claim 1, wherein the shut-off valve is spring-loaded and is actuated by a piston valve pusher moving under the action of the fuel delivered to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.
4. A system as claimed in claim 1, wherein the shut-off valve is spring-loaded and is actuated by a piston valve pusher moving under the action of the fuel delivered to it from the fuel pump, the excess fuel being discharged by the piston valve pusher along a pipe into the inlet system of the fuel pump.
US120844A 1971-03-04 1971-03-04 System of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines Expired - Lifetime US3682146A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12084471A 1971-03-04 1971-03-04

Publications (1)

Publication Number Publication Date
US3682146A true US3682146A (en) 1972-08-08

Family

ID=22392875

Family Applications (1)

Application Number Title Priority Date Filing Date
US120844A Expired - Lifetime US3682146A (en) 1971-03-04 1971-03-04 System of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines

Country Status (1)

Country Link
US (1) US3682146A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3983849A (en) * 1974-07-25 1976-10-05 Robert Bosch G.M.B.H. Fuel injection system
US4140088A (en) * 1977-08-15 1979-02-20 The Bendix Corporation Precision fuel injection apparatus
US4258681A (en) * 1977-11-26 1981-03-31 Dr. Ing. H.C.F. Porsche Aktiengesellschaft Fuel system for a mixture-compressing, spark ignited four cycle internal combustion engine with charge stratification
US4865002A (en) * 1988-02-24 1989-09-12 Outboard Marine Corporation Fuel supply system for internal combustion engine
US5447142A (en) * 1994-12-06 1995-09-05 Caterpillar Inc. Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel
US20100319655A1 (en) * 2008-03-12 2010-12-23 Cameron International Corporation Internal combustion engine with shrouded injection valve and pre-combustion chamber system
US9670827B2 (en) 2008-03-12 2017-06-06 Ge Oil & Gas Compression Systems, Llc Pre-chamber

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1588885A (en) * 1924-11-24 1926-06-15 Hart Russell Combustion-pressure apparatus
US1737813A (en) * 1920-10-21 1929-12-03 Percival S Tice Carbureting system for internal-combustion engines
US1953808A (en) * 1931-04-21 1934-04-03 Christian H Kenneweg Liquid-fuel storage and supply system
US2766582A (en) * 1951-10-06 1956-10-16 Lester H Smith Apparatus for creating electric space charges in combustion engines
US2816533A (en) * 1943-01-20 1957-12-17 Reggio Ferdinando Carlo Fluid pump system
US2849992A (en) * 1954-12-24 1958-09-02 Shell Dev Stratified charge internal combustion engine
US2914043A (en) * 1954-12-16 1959-11-24 Daimler Benz Ag Method and apparatus for operating fuel injection engines
US3443552A (en) * 1966-12-13 1969-05-13 Ernest A Von Seggern Internal combustion engine,fuel supply system and process

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1737813A (en) * 1920-10-21 1929-12-03 Percival S Tice Carbureting system for internal-combustion engines
US1588885A (en) * 1924-11-24 1926-06-15 Hart Russell Combustion-pressure apparatus
US1953808A (en) * 1931-04-21 1934-04-03 Christian H Kenneweg Liquid-fuel storage and supply system
US2816533A (en) * 1943-01-20 1957-12-17 Reggio Ferdinando Carlo Fluid pump system
US2766582A (en) * 1951-10-06 1956-10-16 Lester H Smith Apparatus for creating electric space charges in combustion engines
US2914043A (en) * 1954-12-16 1959-11-24 Daimler Benz Ag Method and apparatus for operating fuel injection engines
US2849992A (en) * 1954-12-24 1958-09-02 Shell Dev Stratified charge internal combustion engine
US3443552A (en) * 1966-12-13 1969-05-13 Ernest A Von Seggern Internal combustion engine,fuel supply system and process

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3983849A (en) * 1974-07-25 1976-10-05 Robert Bosch G.M.B.H. Fuel injection system
US4140088A (en) * 1977-08-15 1979-02-20 The Bendix Corporation Precision fuel injection apparatus
US4258681A (en) * 1977-11-26 1981-03-31 Dr. Ing. H.C.F. Porsche Aktiengesellschaft Fuel system for a mixture-compressing, spark ignited four cycle internal combustion engine with charge stratification
US4865002A (en) * 1988-02-24 1989-09-12 Outboard Marine Corporation Fuel supply system for internal combustion engine
US5447142A (en) * 1994-12-06 1995-09-05 Caterpillar Inc. Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel
EP0716224A1 (en) 1994-12-06 1996-06-12 Caterpillar Inc. Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel
US20100319655A1 (en) * 2008-03-12 2010-12-23 Cameron International Corporation Internal combustion engine with shrouded injection valve and pre-combustion chamber system
US9670827B2 (en) 2008-03-12 2017-06-06 Ge Oil & Gas Compression Systems, Llc Pre-chamber
US9677459B2 (en) 2008-03-12 2017-06-13 Ge Oil & Gas Compression Systems, Llc Internal combustion engine with shrouded injection valve and precombustion chamber system
US9745891B2 (en) 2008-03-12 2017-08-29 Ge Oil & Gas Compression Systems, Llc Internal combustion engine with shrouded injection valve and precombustion chamber system
US9938886B2 (en) * 2008-03-12 2018-04-10 Ge Oil & Gas Compression Systems, Llc Internal combustion engine with shrouded injection valve and pre-combustion chamber system
US10662864B2 (en) 2008-03-12 2020-05-26 Ge Oil & Gas Compression Systems, Llc Internal combustion engine with shrouded injection valve and precombustion chamber system

Similar Documents

Publication Publication Date Title
US4022165A (en) Fuel injection system for successively introducing multiple fuel quantities in an engine cylinder
CN1069381C (en) Forming method of fuel air mixture of I.C engine and fuel feeding attachment
US3824965A (en) Fuel system
KR870004224A (en) Fuel delivery method
GB909867A (en) Improvements in or relating to internal combustion engines
GB2126650A (en) I c engine injection system providing a stratified charge of two fuels
GB2073320A (en) Exhaust gas recirculation in an internal combustion engine
US4068629A (en) Stepped piston two stroke engines
US3826234A (en) Fuel injection apparatus in an internal combustion engine
US3987774A (en) Supplementary fuel injection apparatus for the internal combustion engine
US3682146A (en) System of fuel injection and precombustion-chamber spray ignition in piston and rotary-piston internal combustion engines
GB1172067A (en) Improvements in or relating to a Fuel Feed System for a Fuel Injection Internal Combustion Engine
US3980058A (en) Fuel feed control system of internal combustion engine
US4078535A (en) Modification to an internal combustion engine to reduce both fuel consumption and air pollutants
US2319773A (en) Control device
US4369747A (en) Method of and apparatus for preparation of a combustion mixture for engines with divided combustion space
GB1417703A (en) Fuel injection apparatus for internal combustion engines
RU2260144C2 (en) Device to deliver water into internal combustion engine
US3895618A (en) Differential fuel supply system for internal combustion engines
US3604405A (en) Fuel injectors
SU990087A3 (en) Device for heating intake air in internal combustion compression-inflammation engine
SU803868A3 (en) Fuel system of internal combustion engine
US3664318A (en) Fuel injection system
SU1080755A3 (en) Internal combustion engine
US1737813A (en) Carbureting system for internal-combustion engines