US2603159A - Fuel injection system - Google Patents

Fuel injection system Download PDF

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Publication number
US2603159A
US2603159A US781605A US78160547A US2603159A US 2603159 A US2603159 A US 2603159A US 781605 A US781605 A US 781605A US 78160547 A US78160547 A US 78160547A US 2603159 A US2603159 A US 2603159A
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fuel
manifold
pumps
vent
engine
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US781605A
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Lloyd E Johnson
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Caterpillar Inc
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Caterpillar Tractor Co
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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
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/0047Layout or arrangement of systems for feeding fuel
    • F02M37/0052Details on the fuel return circuit; Arrangement of pressure regulators
    • 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
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/007Venting means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

  • This invention relates to fuel injection'systems and particularly to that portion of I a fuel injection system by means of which fuel is directed to injection pumps and any air entrained with the fuel is vented or returned to the source of fuel supply. 7
  • the present invention provides means for automatically and continuously relieving or venting air from fuel supplied to injection pumps and. is disclosed herein in association with an engine having pumps located in close; proximity to the engine cylinders and, therefore, spaced apart from each other a considerable distance. It will appear from an understanding of the present disclosure, however, that the invention is equally adaptable to injection systems wherein the pumps are all contained in a compact group and connected with the several cylinders of the en gine by longer conduits.
  • FIG. 1 is a vertical section'taken transversely through a portion of an engine equipped with a fuel injection system embodying the present invention and taken on the'plane indicated by the line 1-1 in Fig. 1; and v Fig. 2 is a fragmentary section taken on the line 11-11 of Fig. 1;
  • a portion of a combustion engine of the compression ignition type is illustrated as comprising a cylinder block 10 having cylinders within which pistons H are reciprocably mounted in theconventional manner.
  • a cylinder head casting l2 overlies the block and contains a fuel injection nozzle l3 for each of the cylinders in the'blo'ck.
  • 'A' conduit l4 connects this nozzle with a fuel injection pump generally indicated at "[5.
  • the pump herein shown is of the reciprocating plunger type having a cylinder [6 in which a plunger 11 is disposed.
  • a spring l8 normally retracts the plunger and a cam I9 on a cam shaft 20 acts through a cam follower 2
  • Fuel oil is supplied to the interior of the cylinder 16 upon retraction of the plunger through an inlet port 22.
  • the port 22 communicates with a bore 23 in the pump housing.
  • a pump assembly I5 is provided for each cylinder of the engine and the pump assemblies are preferably arranged in alignment, as illustrated in Fig. 2
  • fuel oil is distributed to the several pumps through a common manifold 24.
  • each of the pumps is provided with a fitting 25 secured in place thereon as by a nut 26.
  • Each of the fittings 251 has a bore for the reception of the manifold'pipe 24 and this pipe is preferably, as shown in Fig. 2, formed in separate sections with sufficientspace between'the ends of the sections to permit the flow of oil from the interior of the manifold downwardly through a bore 21, which, as shown in Fig. 1, communicates with the bore 23 in the pump housing.
  • Fuel oil is introduced to the manifold 24 through a fitting 28, which fitting communicates with a conduit 29 leading to a fuel transfer pump (not shown).
  • the fuel transfer pump operating at a relatively low pressure, withdraws fuel from a fuel tank or reservoir (not shown) and directs it into the manifold so therein to meet the requirements of the several fuel injection pumps associated with the manifold.
  • vent manifold 30 conventional internal ably also supported by and passing through the fittings.
  • the vent manifold communicates with the fuel manifold 24 only at its opposite ends and through restricted orifices 3! formed in the endmost fittings 25.
  • the vent manifold 30 also communicates as through a fitting 32 shown in Fig. 2 with a return line 33 preferably leading to the fuel tank or other source of supply from whichithe fuel is withdrawn by the transfer pump.
  • which communicate between the extreme ends of the fuel manifold and, the ends of the vent manifold 30,, insure a constant return of a limited amount of fuel;oil to the source of supply.
  • These orifices are preferably restricted or small in diameter so that the quantity of fuel returned is very limited and an excess or unnecessary burden is not placed upon vfuel manifold with the vent manifold, means for directing fuel from a source to the fuel manifold, and means connecting the vent manifold the fuel transfer pump.
  • These orifices are, how-- ever, sufficiently large to insure return to the source of supply of any air that might be included in the fuel delivered by the fuel transfer pump to the fuel oil manifold 24.
  • vent manifold 30 is disposedabove the fuel manifold 24, any air deliveredto the rally find its way into the vent manifold.
  • : adjacent the opposite ends of the fuel manifold is toinsure that air which occupies the uppermost position in the manifold will always be able to escapeinto the vent manifold regardless of whether the engine is tilted forwardly or rearwardly, as would occur if a vehicle in which the engine was carried were travelingup'or down grade.
  • the capacity of the fueltransfer pump is. sufli cient to fulfill the requirements of, all of the fuel injection pumps on the engine and to pro vide sufficient extra fuelto insure a constant return through the vent manifold back to they source of supply. Consequently, the fuel injection pumps which withdraw -oil from the lower portion of the fuel manifold 24 will never receive any of the air which occupies the upper portion of said manifold, and-is delivered back with the excess oil to the source of supply.
  • the fuel oil manifold 24, herein-shown as sep-- arate pieces of pipe entering the fittings 25 and the fitting 28, is preferably brazed or otherwise securely sealed at its several points of connection with these fittings, though it may, of course, be a single pipe with bored openings communieating with the bored passages in the fittings.
  • the invention as herein disclosed is applied to an engine wherein the fuel injection pumps are spaced according to the spacing of cylindersin the engine and are inalignment with each other. It is apparent, however, that the manifold pipes may be curved for adaptation to other arrangements of fuel injection pumps or may be considerably shorter where all of the pumps are contained in a group within a single fuel injection housing.
  • a fuel injection system for an engine comprising a plurality of aligned fuel pumps, a fuel manifold disposed above and connecting the intakes of said pumps, a vent manifold parallel to and above the fuel manifold, vent openings connecting said manifolds adjacent their extreme ends, and means for exhausting fluid from the vent manifold.
  • a fuel injection system for an engine comprising a plurality of injectionfpumps to which fuel is supplied from a source, a fuel supply manifold disposed above said pumps, means for directing fuel downwardly from said manifold to each of said pumps, and vent'opening'in the upper portion of said manifold.
  • a fuel injection system for an engine comprising a plurality of injection pumps to which fuel is supplied from a source, a fuel supply manifold disposed above said; pumps,
  • a fuel injection system forlane'ngine comprising a plurality of injection pumps to which fuel is supplied from a source, a fuel supply manifold disposed above said pumps, means for directing fuel downwardly from said manifold to each of said pumps, restricted vent openings in the upper portion of said manifold, and means communicating between said vent openings and said fuel source.

Description

y 15, 1952 1.. E. JOHNSON 2,603,159
FUEL INJECTION SYSTEM Filed Oct. 23, 1947 2 SHEETS SHEET 1 El E -l- AI IV A! IV /7 ,J IV I E A! IV INVENTOR. [A n 5 1124M ATTORNEY Jufly 15, 1952 L. E. JOHNSON 2,603,159
FUEL INJECTION SYSTEM Filed Oct. 25, 1947 2 SHEETS-SHEET 2 Q INVENTOR.
A TTORNEY Patented July 15, 19 52 UNITED [STATES PATENT OFFICE" Q I a 2, 03,159 x q ruin) INJECTION SYSTEM Lloyd E. Johnson, Peoria, 111., assignor't o" cater pillar Tractor ('30., San Leandro, Calif.,- a corporation of California 7 V Application October 2a, 1947, Serial No. 781.605
5 Claims.
This invention relates to fuel injection'systems and particularly to that portion of I a fuel injection system by means of which fuel is directed to injection pumps and any air entrained with the fuel is vented or returned to the source of fuel supply. 7
It is conventional practice in injecting fuel to internal combustion engines to employ a set .of pumps corresponding in number to the number of cylinders in the engine. Fuel is supplied to these pumps from the fuel tank by a low pressure transfer pump and the fuelinjection pumps are operated by cam action in the order and timing desired. Because of the high pressure and small volume operation of the injection pumps, any gas or air included with the fuel delivered to them will interfere with their proper functioning and failure of fuel delivery to the engine cylinder results. One method of eliminating air fromthe injection pumps is to provide a vent valve in association with each pump so that upon the presence of air in any pump the valve may be temporarily opened. This method requires the attention of an operator. It is costly because of the necessity of the vent valves and it is undesirable when the injection pumps are exposed in an inaccessible position or obstructed by other engine parts.
The present invention provides means for automatically and continuously relieving or venting air from fuel supplied to injection pumps and. is disclosed herein in association with an engine having pumps located in close; proximity to the engine cylinders and, therefore, spaced apart from each other a considerable distance. It will appear from an understanding of the present disclosure, however, that the invention is equally adaptable to injection systems wherein the pumps are all contained in a compact group and connected with the several cylinders of the en gine by longer conduits.
It is an object of this invention to provide a fuel injection system for engines having means to continuously vent air from the system just before it reaches the injection pumps. Another object is to provide an arrangement for venting air or gas from such a system that will operate regardless of variations in the position of the engine such as might be caused by a vehicle carrying the engine traveling up or down grade. Still further and more specific objects and advantages of the invention are made apparent in the following specification wherein a preferred form of the invention is described in detail by reference to the accompanying drawings.
' that a constant supply of fuel is always present 7 Fig. 1 is a vertical section'taken transversely through a portion of an engine equipped with a fuel injection system embodying the present invention and taken on the'plane indicated by the line 1-1 in Fig. 1; and v Fig. 2 is a fragmentary section taken on the line 11-11 of Fig. 1;
In Fig. 1 a portion of a combustion engine of the compression ignition type is illustrated as comprising a cylinder block 10 having cylinders within which pistons H are reciprocably mounted in theconventional manner. A cylinder head casting l2 overlies the block and contains a fuel injection nozzle l3 for each of the cylinders in the'blo'ck. 'A' conduit l4connects this nozzle with a fuel injection pump generally indicated at "[5. The pump herein shown is of the reciprocating plunger type having a cylinder [6 in which a plunger 11 is disposed. A spring l8 normally retracts the plunger and a cam I9 on a cam shaft 20 acts through a cam follower 2| to advance the'plunger'in opposition to the action of the spring l8. Fuel oil is supplied to the interior of the cylinder 16 upon retraction of the plunger through an inlet port 22. The port 22 communicates with a bore 23 in the pump housing. A pump assembly I5 is provided for each cylinder of the engine and the pump assemblies are preferably arranged in alignment, as illustrated in Fig. 2
According to the present invention fuel oil is distributed to the several pumps through a common manifold 24. To support thismanifold each of the pumps is provided with a fitting 25 secured in place thereon as by a nut 26. Each of the fittings 251has a bore for the reception of the manifold'pipe 24 and this pipe is preferably, as shown in Fig. 2, formed in separate sections with sufficientspace between'the ends of the sections to permit the flow of oil from the interior of the manifold downwardly through a bore 21, which, as shown in Fig. 1, communicates with the bore 23 in the pump housing. Fuel oil is introduced to the manifold 24 through a fitting 28, which fitting communicates with a conduit 29 leading to a fuel transfer pump (not shown). The fuel transfer pump, operating at a relatively low pressure, withdraws fuel from a fuel tank or reservoir (not shown) and directs it into the manifold so therein to meet the requirements of the several fuel injection pumps associated with the manifold.
conventional internal ably also supported by and passing through the fittings is a vent manifold 30. The vent manifold communicates with the fuel manifold 24 only at its opposite ends and through restricted orifices 3! formed in the endmost fittings 25. The vent manifold 30 also communicates as through a fitting 32 shown in Fig. 2 with a return line 33 preferably leading to the fuel tank or other source of supply from whichithe fuel is withdrawn by the transfer pump. The
orifices 3|, which communicate between the extreme ends of the fuel manifold and, the ends of the vent manifold 30,, insure a constant return of a limited amount of fuel;oil to the source of supply. These orifices are preferably restricted or small in diameter so that the quantity of fuel returned is very limited and an excess or unnecessary burden is not placed upon vfuel manifold with the vent manifold, means for directing fuel from a source to the fuel manifold, and means connecting the vent manifold the fuel transfer pump. These orifices are, how-- ever, sufficiently large to insure return to the source of supply of any air that might be included in the fuel delivered by the fuel transfer pump to the fuel oil manifold 24.
Because the vent manifold 30 is disposedabove the fuel manifold 24, any air deliveredto the rally find its way into the vent manifold. The reason for placing the orifices: 3|: adjacent the opposite ends of the fuel manifold is toinsure that air which occupies the uppermost position in the manifold will always be able to escapeinto the vent manifold regardless of whether the engine is tilted forwardly or rearwardly, as would occur if a vehicle in which the engine was carried were travelingup'or down grade. The capacity of the fueltransfer pump is. sufli cient to fulfill the requirements of, all of the fuel injection pumps on the engine and to pro vide sufficient extra fuelto insure a constant return through the vent manifold back to they source of supply. Consequently, the fuel injection pumps which withdraw -oil from the lower portion of the fuel manifold 24 will never receive any of the air which occupies the upper portion of said manifold, and-is delivered back with the excess oil to the source of supply.
The fuel oil manifold 24, herein-shown as sep-- arate pieces of pipe entering the fittings 25 and the fitting 28, is preferably brazed or otherwise securely sealed at its several points of connection with these fittings, though it may, of course, be a single pipe with bored openings communieating with the bored passages in the fittings. The invention as herein disclosed is applied to an engine wherein the fuel injection pumps are spaced according to the spacing of cylindersin the engine and are inalignment with each other. It is apparent, however, that the manifold pipes may be curved for adaptation to other arrangements of fuel injection pumps or may be considerably shorter where all of the pumps are contained in a group within a single fuel injection housing.
.25 fuel manifold by the transfer pump will natuwith said source.
2. In a fuel injection system for an engine comprising a plurality of aligned fuel pumps, a fuel manifold disposed above and connecting the intakes of said pumps, a vent manifold parallel to and above the fuel manifold, vent openings connecting said manifolds adjacent their extreme ends, and means for exhausting fluid from the vent manifold.
3. In a fuel injection system for an engine comprising a plurality of injectionfpumps to which fuel is supplied from a source, a fuel supply manifold disposed above said pumps, means for directing fuel downwardly from said manifold to each of said pumps, and vent'opening'in the upper portion of said manifold.- i
4. In a fuel injection system for an engine comprising a plurality of injection pumps to which fuel is supplied from a source, a fuel supply manifold disposed above said; pumps,
means for directing fueldownwardly from said manifold to each of said pumps, vent openings in the upper portion of said manifold, and {means communicating between said vent openings and said fuel source.
5. In a fuel injection system forlane'ngine comprising a plurality of injection pumps to which fuel is supplied from a source, a fuel supply manifold disposed above said pumps, means for directing fuel downwardly from said manifold to each of said pumps, restricted vent openings in the upper portion of said manifold, and means communicating between said vent openings and said fuel source.
LLOYD E. JOHNSONQ REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,096,711 Fielden Oct. 26, 1937 2,185,144 Edwards Dec. 26, 1989 2,192,387 Schlaupitz 1 1 Mar. 5, 1940 2,357,870 Beeh -1- Sept; 12, 1944 2,412,316 Campbell 1 Dec. 10, '1946 2,414,261 Kalitinsky Jan. 14, 194! 2,426,319 Meitzler Aug. 26, '1947 2,458,377
Hennings Jan. 4, 1949
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3100449A (en) * 1959-02-04 1963-08-13 Borg Warner Fuel injection pump
US3242913A (en) * 1963-04-24 1966-03-29 Max G Fiedler Compression ignition engine
DE1254907B (en) * 1959-02-04 1967-11-23 Borg Warner Fuel injection pump
US3624823A (en) * 1969-03-18 1971-11-30 Bosch Gmbh Robert Multicylinder fuel injection pump for internal combustion engines
US3651756A (en) * 1969-08-11 1972-03-28 Roy R Smith Jr Spray dampening system with individual metering pumps for offset press
EP0638719A1 (en) * 1993-08-09 1995-02-15 WOODWARD GOVERNOR GERMANY GmbH Fuel pipe connection for fuel injection pumps
US20030188481A1 (en) * 2000-05-02 2003-10-09 Weder Donald E. Liquid impermeable decorative sleeve for flower pot

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2096711A (en) * 1934-11-28 1937-10-26 Gen Motors Corp Fuel pump for injectors
US2185144A (en) * 1937-05-27 1939-12-26 Timken Roller Bearing Co Fuel injection pump
US2192387A (en) * 1937-11-08 1940-03-05 Timken Roller Bearing Co Fuel injection pump
US2357870A (en) * 1941-11-29 1944-09-12 Beeh Louis Fuel injection pump for internal-combustion engines
US2412316A (en) * 1942-01-16 1946-12-10 George M Holley Fuel injection system
US2414261A (en) * 1943-07-23 1947-01-14 United Aircraft Corp Accumulator pump
US2426319A (en) * 1943-05-11 1947-08-26 United Aircraft Corp Injection system
US2458377A (en) * 1944-06-03 1949-01-04 Hennings William Earl Light fuel injector

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2096711A (en) * 1934-11-28 1937-10-26 Gen Motors Corp Fuel pump for injectors
US2185144A (en) * 1937-05-27 1939-12-26 Timken Roller Bearing Co Fuel injection pump
US2192387A (en) * 1937-11-08 1940-03-05 Timken Roller Bearing Co Fuel injection pump
US2357870A (en) * 1941-11-29 1944-09-12 Beeh Louis Fuel injection pump for internal-combustion engines
US2412316A (en) * 1942-01-16 1946-12-10 George M Holley Fuel injection system
US2426319A (en) * 1943-05-11 1947-08-26 United Aircraft Corp Injection system
US2414261A (en) * 1943-07-23 1947-01-14 United Aircraft Corp Accumulator pump
US2458377A (en) * 1944-06-03 1949-01-04 Hennings William Earl Light fuel injector

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3100449A (en) * 1959-02-04 1963-08-13 Borg Warner Fuel injection pump
DE1254907B (en) * 1959-02-04 1967-11-23 Borg Warner Fuel injection pump
US3242913A (en) * 1963-04-24 1966-03-29 Max G Fiedler Compression ignition engine
US3624823A (en) * 1969-03-18 1971-11-30 Bosch Gmbh Robert Multicylinder fuel injection pump for internal combustion engines
US3651756A (en) * 1969-08-11 1972-03-28 Roy R Smith Jr Spray dampening system with individual metering pumps for offset press
EP0638719A1 (en) * 1993-08-09 1995-02-15 WOODWARD GOVERNOR GERMANY GmbH Fuel pipe connection for fuel injection pumps
US20030188481A1 (en) * 2000-05-02 2003-10-09 Weder Donald E. Liquid impermeable decorative sleeve for flower pot

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