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US1289716A - Fuel-pump for internal-combustion engines. - Google Patents

Fuel-pump for internal-combustion engines. Download PDF

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Publication number
US1289716A
US1289716A US24052718A US24052718A US1289716A US 1289716 A US1289716 A US 1289716A US 24052718 A US24052718 A US 24052718A US 24052718 A US24052718 A US 24052718A US 1289716 A US1289716 A US 1289716A
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United States
Prior art keywords
pump
fuel
plunger
stroke
port
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Expired - Lifetime
Application number
US24052718A
Inventor
Hugh Emile Fenchelle
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WILLIAM L KANN
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WILLIAM L KANN
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Publication date
Application filed by WILLIAM L KANN filed Critical WILLIAM L KANN
Priority to US24052718A priority Critical patent/US1289716A/en
Application granted granted Critical
Publication of US1289716A publication Critical patent/US1289716A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/20Varying fuel delivery in quantity or timing
    • F02M59/24Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke
    • F02M59/26Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke caused by movements of pistons relative to their cylinders

Definitions

  • This invention relates to n improved con struction of fuel pump for internal combustion engines of the kind employing ignition on Diesel lines and especially engines in which the fuel is sprayed into the cylinder mechanically without the aid of an air injector, the chief object of the invention being to provide simple means by which a pump plunger having no valve attachment may deliver varying quantities of fuel without altering the time at which injection begins.
  • the pump plunger is formed with a fuel relief passage which at a variable predetermined point in the delivery stroke registers with a relief port in the pump casing and thus makes communication between the pump chamber and the said port, so that the pressure in the chamber is relieved and the delivery of fuel to the engine stopped.
  • the amount of fuel supplied to the engine will therefore vary according to the point in the pump stroke at which release of the fuel occurs and in the construction preferred the plunger is rotatable by means of connections from the engine governor or regulator and the pump casing is formed with a relief port, preferably leading to the suction side of the pump, the-rear edge of which poi-t is inclined along the axis of the pump so that the moment at which the fuel pressure is relieved varies according to the angular adjustment of the plunger.
  • Fig. 2 is a detail view illustrating the operation of the pump.
  • A is the pump casing, within which works I J the plunger B provided with the relief passage b.
  • C is the suction valve and D the delivery valve of the pump.
  • E is a cam operating the pump through the intermediate member F havin the cam roller
  • the suction stroke 0 the plunger B 1s effected by means of the spring G mounted on the end of the plunger extension 6' which passes through the casing A. This spring G keeps the opposite end of the plunger up against the member F, maintaining the cam roller f against the cam E.
  • the cam E Assuming the pump chamber a to be filled with fuel at the end of the suction stroke of the pump, the cam E as it turns to meet the roller f drives in the plunger B against the pressure of the spring G, causing the annular shoulder bof the pump plunger to compress the fuel in the pump chamber a and to force it at high pressure through the delivery valve D, from which it passes to a suitable spraying nozzle or atomizer in the engine cylinder.
  • the delivery of the fuel continues until the outer end I) of the relief passage 6 reaches the relief outlet a in the casing A, when the pressure on the fuel is instantly relieved, permitting. the delivery valve D to close, while the fuel during the remainder of the compression stroke escapes through the outlet port a, whence it may pass to the suction side of the pump.
  • FIG. 2 shows the form of therelief aperture or port a which permits the amount of fuel delivered by the pump to be regulated by rotation of-the plunger B through its regulating arm I)".
  • a pump casing provided with a fuel relief port, a plunger moving in the said casing havin a passage adapted to make communication etween the said port and the pump chamber and means for varying the point m the plunger stroke at which such communication is made.
  • a pump casing provided with a fuel relief port in its wall, which port is formed with a slanting edge, a plunger having a passa e adapted during the delivery stroke to ma e communication between the said port and the pumpchamber and-means for angularly adjustin the plunger to vary the point in the stroke at which such communication is made.
  • a pump casing provided with a fuel relief port, a plunger position of the plunger,- an
  • a pump casing provided with a fuel relief port, a plunger having a fuel relief passage adapted to registerwith the said port at a predetermined point in the pump stroke, a. cam. effecting the delivery stroke of the plunger and a spring adapted to return the plunger on the suction stroke 5.
  • a liquid fuel pump having a relief passage arranged to dischar e fluid from the pump chamber independent y of the regular delivery of the pump and t0 the exclusion thereof, and means whereby said relief passage may be brought into action at any one of a number of different predetermined points in the deliver stroke of the pump.

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

Description

H. E. FENCHELLE.
FUEL PUMP FOR INTERNAL COMBUSTION ENGINES. APPLICATION FILED DEC-6.1917- RENEWED JUNE I7, I918,
11. 289;? 1 6 Patented Dec. 31, 191&
Inventor.
sir-are rarest @FFEQE.
HUGH EMILE FENCHELLE, OF GENOA, ITALY, ASSIGNOR T0 WILLIAM L. KANN,
TRUSTEE, OF PITTSBURGH, PENNSYLVANIA.
FUEL-PUMP FOR INTEBNAL-COMBUSTION ENGINES.
Specification of Letters Patent,
Patented Dec; 31*, 1918.
Application filed December 6, 1817, Serial No. 205,885. Renewed June 17, 1918. Serial No. 240,527.
To all whom it may concern:
Be it known that I, HUGH EMILE FEN- CHELLE, a British subject, residing at Via XX Settembre 34/4, Genoa, in the Kingdom of Italy, have invented certain new and useful Improvements in Fuel-Pumps for Internal-Combustion Engines, of which the following is a specification.
This invention relates to n improved con struction of fuel pump for internal combustion engines of the kind employing ignition on Diesel lines and especially engines in which the fuel is sprayed into the cylinder mechanically without the aid of an air injector, the chief object of the invention being to provide simple means by which a pump plunger having no valve attachment may deliver varying quantities of fuel without altering the time at which injection begins. I
According to this invention the pump plunger is formed with a fuel relief passage which at a variable predetermined point in the delivery stroke registers with a relief port in the pump casing and thus makes communication between the pump chamber and the said port, so that the pressure in the chamber is relieved and the delivery of fuel to the engine stopped. The amount of fuel supplied to the engine will therefore vary according to the point in the pump stroke at which release of the fuel occurs and in the construction preferred the plunger is rotatable by means of connections from the engine governor or regulator and the pump casing is formed with a relief port, preferably leading to the suction side of the pump, the-rear edge of which poi-t is inclined along the axis of the pump so that the moment at which the fuel pressure is relieved varies according to the angular adjustment of the plunger.
In order that-the said invention may be clearly understood and readily carried into effect I will describe the same more fully with reference to the accompanying drawings, in which Figure 1 is a longitudinal section of a pump constructed in accordance with this inventlon, showing also the cam mechanism for operating the pump; and
Fig. 2 is a detail view illustrating the operation of the pump.
' A is the pump casing, within which works I J the plunger B provided with the relief passage b. C is the suction valve and D the delivery valve of the pump. E is a cam operating the pump through the intermediate member F havin the cam roller The suction stroke 0 the plunger B 1s effected by means of the spring G mounted on the end of the plunger extension 6' which passes through the casing A. This spring G keeps the opposite end of the plunger up against the member F, maintaining the cam roller f against the cam E.
Assuming the pump chamber a to be filled with fuel at the end of the suction stroke of the pump, the cam E as it turns to meet the roller f drives in the plunger B against the pressure of the spring G, causing the annular shoulder bof the pump plunger to compress the fuel in the pump chamber a and to force it at high pressure through the delivery valve D, from which it passes to a suitable spraying nozzle or atomizer in the engine cylinder. The delivery of the fuel continues until the outer end I) of the relief passage 6 reaches the relief outlet a in the casing A, when the pressure on the fuel is instantly relieved, permitting. the delivery valve D to close, while the fuel during the remainder of the compression stroke escapes through the outlet port a, whence it may pass to the suction side of the pump.
- Fig. 2 shows the form of therelief aperture or port a which permits the amount of fuel delivered by the pump to be regulated by rotation of-the plunger B through its regulating arm I)". As will be noted in Fig.
lar displacement of the pump plunger. which is free to turn in the casing. By turning the plunger through the lever arm I), operated automatically or otherwise through any suitable gear, the end of the effective stroke of the pump is timed in a very simple manner by bringing the end 6 of the passage 6 v in line with the desired point on the sloping port edge a When the cam has completed its delivery stroke the spring G returns the plunger and 4 fresh fuel is drawn throu h the suction valve G into the pump cham er a ready for the next delivery stroke.
What I claim and desire to secure by Letters Patent of the United States is 1. In a liquidtfuel pump, a pump casing provided with a fuel relief port, a plunger moving in the said casing havin a passage adapted to make communication etween the said port and the pump chamber and means for varying the point m the plunger stroke at which such communication is made.
2. In a liquid fuel pump, a pump casing provided with a fuel relief port in its wall, which port is formed with a slanting edge, a plunger having a passa e adapted during the delivery stroke to ma e communication between the said port and the pumpchamber and-means for angularly adjustin the plunger to vary the point in the stroke at which such communication is made.
3. In a liquid fuel pump, a pump casing provided with a fuel relief port, a plunger position of the plunger,- an
moving in the said casing having a passage adapted to make communication between the said port and the pump chamber at a point in the stroke dependir. on the angular means for angularly adjusting the plunger.
4. In a liquid fuel pump, a pump casing provided with a fuel relief port, a plunger having a fuel relief passage adapted to registerwith the said port at a predetermined point in the pump stroke, a. cam. effecting the delivery stroke of the plunger and a spring adapted to return the plunger on the suction stroke 5. A liquid fuel pump having a relief passage arranged to dischar e fluid from the pump chamber independent y of the regular delivery of the pump and t0 the exclusion thereof, and means whereby said relief passage may be brought into action at any one of a number of different predetermined points in the deliver stroke of the pump.
HUGH E ILE FENCHELLE.
US24052718A 1918-06-17 1918-06-17 Fuel-pump for internal-combustion engines. Expired - Lifetime US1289716A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US24052718A US1289716A (en) 1918-06-17 1918-06-17 Fuel-pump for internal-combustion engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US24052718A US1289716A (en) 1918-06-17 1918-06-17 Fuel-pump for internal-combustion engines.

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US1289716A true US1289716A (en) 1918-12-31

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421844A (en) * 1944-01-28 1947-06-10 United Aircraft Corp Fuel injection system
US2441259A (en) * 1943-12-06 1948-05-11 William H Cook Ratio control comprising a chamber for a first liquid passing therethrough and a member therein having a port for feeding a second liquid into the first liquid
US2482733A (en) * 1946-07-13 1949-09-20 Injector Company Aktiebolag Fuel injection pump
US2540755A (en) * 1947-06-25 1951-02-06 United Aireraft Corp Fuel injection system and apparatus

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2441259A (en) * 1943-12-06 1948-05-11 William H Cook Ratio control comprising a chamber for a first liquid passing therethrough and a member therein having a port for feeding a second liquid into the first liquid
US2421844A (en) * 1944-01-28 1947-06-10 United Aircraft Corp Fuel injection system
US2482733A (en) * 1946-07-13 1949-09-20 Injector Company Aktiebolag Fuel injection pump
US2540755A (en) * 1947-06-25 1951-02-06 United Aireraft Corp Fuel injection system and apparatus

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