[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US3233550A - High pressure fuel pumps - Google Patents

High pressure fuel pumps Download PDF

Info

Publication number
US3233550A
US3233550A US275340A US27534063A US3233550A US 3233550 A US3233550 A US 3233550A US 275340 A US275340 A US 275340A US 27534063 A US27534063 A US 27534063A US 3233550 A US3233550 A US 3233550A
Authority
US
United States
Prior art keywords
fuel
cam
cylinder
plunger
ring
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
US275340A
Inventor
Sidney T Smith
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US275340A priority Critical patent/US3233550A/en
Application granted granted Critical
Publication of US3233550A publication Critical patent/US3233550A/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
    • F02M69/46Details, component parts or accessories not provided for in, or of interest apart from, the apparatus covered by groups F02M69/02 - F02M69/44
    • F02M69/50Arrangement of fuel distributors, e.g. with means for supplying equal portion of metered fuel to injectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R17/00Arrangements or adaptations of lubricating systems or devices
    • B60R17/02Systems, e.g. central lubrication systems
    • 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
    • F02M41/00Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/08Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
    • 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
    • F02M59/02Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
    • F02M59/04Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by special arrangement of cylinders with respect to piston-driving shaft, e.g. arranged parallel to that shaft or swash-plate type pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B9/00Piston machines or pumps characterised by the driving or driven means to or from their working members
    • F04B9/02Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical
    • F04B9/04Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical the means being cams, eccentrics or pin-and-slot mechanisms
    • 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
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/05Miscellaneous constructional elements; Leakage detection
    • F02M2700/055Fuel distribution among injection nozzles
    • 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
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/13Special devices for making an explosive mixture; Fuel pumps
    • F02M2700/1317Fuel pumpo for internal combustion engines
    • F02M2700/1329Controlled rotary fuel pump with parallel pistons or with a single piston in the extension of the driving shaft

Definitions

  • the metering is accomplished by rotating One ring with inclined planed surfaces coaxially disposed around the pump axis against another ring of similar design but having the inclined planed surfaces slanted in the opposite direction and held stationary so as to force the two rings farther apart. This action raises the rotor and cam which when the motor is operating, produces a longer stroke in the pump barrel and results in a heavier charge of fuel to the engine cylinder being served.
  • This pump if built in sufficiently substantial proportions and of proper materials, should endure the high pressures generated in a high pressure pump over long periods of service. Furthermore, the simplicity of design and low number of working parts should make for economy in manufacture.
  • FIG. 1 is a vertical sectional View of a fuel pump in accordance with this invention.
  • FIG. 2 is an inverted view of the ring 20.
  • FIG. 3 is a side view of the rings showing the outer edges of the inclined planed surfaces.
  • FIG. 4 is a top view of the rotor and cam assembly.
  • FIG. 5 is a side View of the rotor.
  • this pump comprises a main body 1 of generally cylindrical form, such body including at the bottom, a collar for bolting on the lower body 2 which holds the driving and metering equipment.
  • These include a drive shaft 2 3, splined at the upper end, the rotor 16 with a slot in its center, splined to lit on the upper end of the drive shaft, and the two rings and 21 with the inclined planed surfaces opposed.
  • the main body 1 is formed with a prescribed number of bores coaxially disposed and evenly spaced, which hold the pump barrels 4, and the tappets 13.
  • the barrels 4 are threaded at the upper ends to receive the plugs which hold the fuel lines 10 in place, which conduct fuel to engine cylinders.
  • Cam advanced and spring retracted plungers 9 work in the barrels 4, forced up by the tappets 13 and the cam 15.
  • Helical springs v12 surround the plungers 9 at their lower ends and, working between the lower end of the barrel and the guidehead 11 on the lower end of the plungers, serve to retract the plungers after the pressure stroke.
  • Each pump barrel 4 together with its enclosed plunger 9 and the related working parts form what may be termed a fuel metering and distributing unit.
  • One of these units is allotted to each of the cylinders in the engine being served.
  • the body 1 contains in its center a fuel reservoir 5 fed by a constant delivery pump 27 of about twenty-five pounds pressure. From this reservoir the fuel is fed to the surrounding pump barrels thru check valves 7 and canals 6 and 8. When the plunger 9 is retracted the low pressure fuel from the reservoir 5 is fed into the pump barrels 4 and on the succeding pressure stroke, when the motor is in operation, a charge of fuel is forced thru the fuel line 10 into the engine cylinder being served.
  • the check valves 7 are not indispensible to the working efii- United States Patent 0 ciency of the pump. They serve only to make a shorter plunger stroke adequate.
  • the rings 20 and 21 with the inclined planed surfaces opposed constitute the basis of this device for which a patent is sought.
  • the ring 20 is held from turning by the lugs 19 on its sides which are held by ribs 18 in the inside of the lower body 2.
  • lever 22 is moved in a clockwise direction, as seen from its upper side, ring 21 moves with it and, by the action of the opposed inclined planed surfaces working against each other, forces ring 20, which cannot turn, to a higher position.
  • Rotor 16 and cam 15, supported by ring 20 are moved up with it and, when the pump is in operation, the tappet 1-3 and-the plunger 9 are given a longer pressure stroke, resulting in a heavier charge of fuel to the engine cylinder being served.
  • the pump is mounted at its base to the motor and has a drive gear (not shown) secured on the outer end of the drive shaft 23.
  • the drive gear is properly meshed and timed in the timing gear train so that the charges of fuel are delivered to the respective engine cylinders at the most eflicient time.
  • the described fuel pump while being relatively simple in its structure, is also quite rugged and provides a practical and efficient machine for the injection of high pressure fuels into engine cylinders.
  • a fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage checkval've controlled outwardly, leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder means to reciprocate the plunger thru a stroke of variable length, such latter means including a driven shaft, a rotary cam mounted in driving relation on the shaft and shi ftable axially thereof, one end of the plunger riding a .tappet which rides a cam, and applied to the cam means to shift the cam axially along the shaft in one direction whereby to alter the length of reciprocation of the plunger, said last named means comprising .a non-rotatable ring movable axially on the shaft and on which the cam is rotatably mounted, the face of the ring opposite the cam being provided with inclined planed surfaces, coaxially disposed, riding another ring of similar design with the
  • a fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder,
  • means to reciprocate the plunger thru a stroke of variable length such latter means including a driven shaft, a rotary cam mounted in driving relation on the sharft and shittab le axially thereof, one end of the plunger riding said cam, and applied to the cam means to shift the cam axially along the shaft in one direction, whereby to alter the length of reciprocation of the plunger, said last named means comprising a non-rotatable rin-g, movable axially on the shaft and on which the cam is rotatably mounted, the face of ring opposite the cam being provided with inclined planed sunfaces, coaxially disposed riding another ring of corresponding design with the planed surfaces opposed and means to turn the opposed ring.
  • a fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder, means to reciprocate the plunger thru a stroke of constant length from below the inlet passage to a point beyond the passage, such latter means including a driven shaft, a rotary cam mounted in driving relation on the shaft and shiftable axially thereof, one end of the plunger riding said cam, and applied to the cam means to shift the cam axially (along the shaft in one direction, whereby to alter the range of reciprocation of the plunger, said last named means comprising a non-rotatable ring, movable axially on the shaft and on which the cam is rotatably mounted, the face of ring opposite the cam being provided with inclined planed surfaces, coaxially disposed, riding another ring of corresponding design with the planed surfaces opposed and means

Landscapes

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

Description

? Feb. 8,1966 5. r. SMITH I 3,
HIGH PRESSURE FUEL PUMPS Filed April 24, 1963 2 Sheets-Sheet 1 INVENTOR WTW 1966 s. T. SMITH 3,233,550
. HIGH PRESSURE FUEL PUMPS Filed April 24, 1965 3 Sheets-Sheet z 3,233,550 HIGH PRESSURE FUEL PUMPS Sidney T. Smith, Box 50, Rte. 1, Grafton, W. Va. Filed Apr. 24, 1963, Ser. No. 275,340 3 Claims. (Cl. 10338) This invention relates to improvements in high pressure \fuel pumps such as are used on diesel motors. Several pumps of this type have been patented, differing mainly in their means of metering the fuel. This pump follows that pattern. In this device, the metering is accomplished by rotating One ring with inclined planed surfaces coaxially disposed around the pump axis against another ring of similar design but having the inclined planed surfaces slanted in the opposite direction and held stationary so as to force the two rings farther apart. This action raises the rotor and cam which when the motor is operating, produces a longer stroke in the pump barrel and results in a heavier charge of fuel to the engine cylinder being served.
This pump, if built in sufficiently substantial proportions and of proper materials, should endure the high pressures generated in a high pressure pump over long periods of service. Furthermore, the simplicity of design and low number of working parts should make for economy in manufacture.
In the drawings;
FIG. 1 is a vertical sectional View of a fuel pump in accordance with this invention.
FIG. 2 is an inverted view of the ring 20.
FIG. 3 is a side view of the rings showing the outer edges of the inclined planed surfaces.
FIG. 4 is a top view of the rotor and cam assembly.
FIG. 5 is a side View of the rotor.
Referring now more particularly to the characters of reference in the drawings; this pump comprises a main body 1 of generally cylindrical form, such body including at the bottom, a collar for bolting on the lower body 2 which holds the driving and metering equipment. These include a drive shaft 2 3, splined at the upper end, the rotor 16 with a slot in its center, splined to lit on the upper end of the drive shaft, and the two rings and 21 with the inclined planed surfaces opposed.
The main body 1 is formed with a prescribed number of bores coaxially disposed and evenly spaced, which hold the pump barrels 4, and the tappets 13. The barrels 4 are threaded at the upper ends to receive the plugs which hold the fuel lines 10 in place, which conduct fuel to engine cylinders. Cam advanced and spring retracted plungers 9 work in the barrels 4, forced up by the tappets 13 and the cam 15. Helical springs v12 surround the plungers 9 at their lower ends and, working between the lower end of the barrel and the guidehead 11 on the lower end of the plungers, serve to retract the plungers after the pressure stroke.
Each pump barrel 4 together with its enclosed plunger 9 and the related working parts form what may be termed a fuel metering and distributing unit. One of these units is allotted to each of the cylinders in the engine being served.
The body 1 contains in its center a fuel reservoir 5 fed by a constant delivery pump 27 of about twenty-five pounds pressure. From this reservoir the fuel is fed to the surrounding pump barrels thru check valves 7 and canals 6 and 8. When the plunger 9 is retracted the low pressure fuel from the reservoir 5 is fed into the pump barrels 4 and on the succeding pressure stroke, when the motor is in operation, a charge of fuel is forced thru the fuel line 10 into the engine cylinder being served. The check valves 7 are not indispensible to the working efii- United States Patent 0 ciency of the pump. They serve only to make a shorter plunger stroke adequate.
The rings 20 and 21 with the inclined planed surfaces opposed constitute the basis of this device for which a patent is sought. The ring 20 is held from turning by the lugs 19 on its sides which are held by ribs 18 in the inside of the lower body 2. When lever 22 is moved in a clockwise direction, as seen from its upper side, ring 21 moves with it and, by the action of the opposed inclined planed surfaces working against each other, forces ring 20, which cannot turn, to a higher position. Rotor 16 and cam 15, supported by ring 20, are moved up with it and, when the pump is in operation, the tappet 1-3 and-the plunger 9 are given a longer pressure stroke, resulting in a heavier charge of fuel to the engine cylinder being served. When the cam 15 passes the nub 14 the tappet 13 and the plunger 9 are pushed back to their lowest point by the spring 12 between the lower end of the pump barrel 4 and the guidehead 1 1. The tappet 13 rests on the retainer plate 24 which limits the return stroke of the plunger 9 to a point just below canal '8. When the lever 22 is moved counterclockwise, moving ring 21 with it, some pressure is taken off ring 20 and the spring 17 moves the rotor 16 and the ring 20 down against ring 2 1 which reduces the pressure stroke of the plunger 9.
The pump is mounted at its base to the motor and has a drive gear (not shown) secured on the outer end of the drive shaft 23. The drive gear is properly meshed and timed in the timing gear train so that the charges of fuel are delivered to the respective engine cylinders at the most eflicient time.
The described fuel pump, while being relatively simple in its structure, is also quite rugged and provides a practical and efficient machine for the injection of high pressure fuels into engine cylinders.
From the foregoing description it should be evident that there has been produced such a device as substantially fulfills the objects of the invention as set forth herein.
While this specification sets forth in detail the preferred construction of the device, in practice deviations from such detail may be resorted to as do not form a departure from the basic elements of the invention as defined by the appended claims.
Having thus described the invention, the following is claimed as new and useful, and upon which Letters Patent is sought:
-1. A fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage checkval've controlled outwardly, leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder means to reciprocate the plunger thru a stroke of variable length, such latter means including a driven shaft, a rotary cam mounted in driving relation on the shaft and shi ftable axially thereof, one end of the plunger riding a .tappet which rides a cam, and applied to the cam means to shift the cam axially along the shaft in one direction whereby to alter the length of reciprocation of the plunger, said last named means comprising .a non-rotatable ring movable axially on the shaft and on which the cam is rotatably mounted, the face of the ring opposite the cam being provided with inclined planed surfaces, coaxially disposed, riding another ring of similar design with the planed surfaces opposed, and means to turn the opposed ring.
2. A fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder,
means to reciprocate the plunger thru a stroke of variable length, such latter means including a driven shaft, a rotary cam mounted in driving relation on the sharft and shittab le axially thereof, one end of the plunger riding said cam, and applied to the cam means to shift the cam axially along the shaft in one direction, whereby to alter the length of reciprocation of the plunger, said last named means comprising a non-rotatable rin-g, movable axially on the shaft and on which the cam is rotatably mounted, the face of ring opposite the cam being provided with inclined planed sunfaces, coaxially disposed riding another ring of corresponding design with the planed surfaces opposed and means to turn the opposed ring.
3. A fuel pump comprising a body having a cylinder therein, the cylinder having a head, a fuel outlet passage from said head, a fuel inlet passage leading to the cylinder a distance from said head, a fuel pressure line leading to said inlet passage, a plunger slidable in the cylinder, means to reciprocate the plunger thru a stroke of constant length from below the inlet passage to a point beyond the passage, such latter means including a driven shaft, a rotary cam mounted in driving relation on the shaft and shiftable axially thereof, one end of the plunger riding said cam, and applied to the cam means to shift the cam axially (along the shaft in one direction, whereby to alter the range of reciprocation of the plunger, said last named means comprising a non-rotatable ring, movable axially on the shaft and on which the cam is rotatably mounted, the face of ring opposite the cam being provided with inclined planed surfaces, coaxially disposed, riding another ring of corresponding design with the planed surfaces opposed and means to turn the opposed ring.
References Cited by the Examiner UNITED STATES PATENTS 2,031,346 2/1936 Wahlmark 10338 2,251,552 8/1941 Purdy 10341.2 2,381,585 8/1945 Gambrell 10337 2,459,303 1/ 1949 Baker 10337 2,534,153 12/1950 Widrner 10337 2,645,182 7/1953 Tucker 10337 LAURENCE V. EFNER, Primary Examiner.

Claims (1)

1. A FUEL PUMP COMPRISING A BODY HAVING A CYLINDER THEREIN, THE CYLINDER HAVING A HEAD, A FUEL OUTLET PASSAGE FROM SAID HEAD, A FUEL INLET PASSAGE CHECKVALVE CONTROLLED OUTWARDLY, LEADING TO THE CYLINDER, A DISTANCE FROM SAID HEAD, A FUEL PRESSURE LINE LEADING TO SAID INLET PASSAGE, A PLUNGER SLIDABLE IN THE CYLINDER MEANS TO RECIPROCATE THE PLUNGER SLIDABLE IN THE CYLINDER MEANS TO RECIPROCATE THE INCLUDING A DRIVEN SHAFT, A ROTARY CAM MOUNTED IN DRIVING RELATION ON THE SHAFT AND SHIFTABLE AXIALLY THEREOF, ONE END OF THE PLUNGER RIDING A TAPPET WHICH RIDES A CAM, AND APPLIED TO THE CAM MEANS TO SHIFT THE CAM AXIALLY ALONG
US275340A 1963-04-24 1963-04-24 High pressure fuel pumps Expired - Lifetime US3233550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US275340A US3233550A (en) 1963-04-24 1963-04-24 High pressure fuel pumps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US275340A US3233550A (en) 1963-04-24 1963-04-24 High pressure fuel pumps

Publications (1)

Publication Number Publication Date
US3233550A true US3233550A (en) 1966-02-08

Family

ID=23051871

Family Applications (1)

Application Number Title Priority Date Filing Date
US275340A Expired - Lifetime US3233550A (en) 1963-04-24 1963-04-24 High pressure fuel pumps

Country Status (1)

Country Link
US (1) US3233550A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3461990A (en) * 1966-01-17 1969-08-19 Tecalemit Engineering Trailer lubrication systems
US3841803A (en) * 1973-05-03 1974-10-15 Gen Motors Corp Rotary engine oil metering pump
JPS5125763Y1 (en) * 1974-10-28 1976-07-01
DE2840897A1 (en) * 1977-09-23 1979-03-29 Semt METHOD AND DEVICE FOR STOPPING AN COMBUSTION ENGINE WITH FUEL INJECTION IN THE EVENT OF OVER SPEED
US5724879A (en) * 1996-02-08 1998-03-10 White Moss, Inc. Method and apparatus for controlled axial pump
US5979294A (en) * 1996-02-08 1999-11-09 Whitemoss, Inc. Method and apparatus for controlling axial pump
US6237465B1 (en) * 1998-06-29 2001-05-29 Linde Aktiengesellschaft Axial piston machine with curved bearing surface on the drive plate
US20060002801A1 (en) * 2004-07-01 2006-01-05 Kosco John S Rocker compressor mechanism

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2031346A (en) * 1932-10-17 1936-02-18 Rystrom Charles H Fuel injection pump
US2251552A (en) * 1935-11-07 1941-08-05 Eisemann Magneto Corp Fuel injection pump
US2381585A (en) * 1943-02-13 1945-08-07 Ernest C Gambrell Fuel injection pump
US2459303A (en) * 1942-05-12 1949-01-18 Thomas A Baker Fluid metering system
US2534153A (en) * 1946-03-11 1950-12-12 Schweizerische Lokomotiv Axial cylinder pump especially intended for moving liquids
US2645182A (en) * 1948-04-16 1953-07-14 Boine W Fuller Fuel injector

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2031346A (en) * 1932-10-17 1936-02-18 Rystrom Charles H Fuel injection pump
US2251552A (en) * 1935-11-07 1941-08-05 Eisemann Magneto Corp Fuel injection pump
US2459303A (en) * 1942-05-12 1949-01-18 Thomas A Baker Fluid metering system
US2381585A (en) * 1943-02-13 1945-08-07 Ernest C Gambrell Fuel injection pump
US2534153A (en) * 1946-03-11 1950-12-12 Schweizerische Lokomotiv Axial cylinder pump especially intended for moving liquids
US2645182A (en) * 1948-04-16 1953-07-14 Boine W Fuller Fuel injector

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3461990A (en) * 1966-01-17 1969-08-19 Tecalemit Engineering Trailer lubrication systems
US3841803A (en) * 1973-05-03 1974-10-15 Gen Motors Corp Rotary engine oil metering pump
JPS5125763Y1 (en) * 1974-10-28 1976-07-01
DE2840897A1 (en) * 1977-09-23 1979-03-29 Semt METHOD AND DEVICE FOR STOPPING AN COMBUSTION ENGINE WITH FUEL INJECTION IN THE EVENT OF OVER SPEED
US5724879A (en) * 1996-02-08 1998-03-10 White Moss, Inc. Method and apparatus for controlled axial pump
US5979294A (en) * 1996-02-08 1999-11-09 Whitemoss, Inc. Method and apparatus for controlling axial pump
US6237465B1 (en) * 1998-06-29 2001-05-29 Linde Aktiengesellschaft Axial piston machine with curved bearing surface on the drive plate
US20060002801A1 (en) * 2004-07-01 2006-01-05 Kosco John S Rocker compressor mechanism

Similar Documents

Publication Publication Date Title
US3233550A (en) High pressure fuel pumps
US2292125A (en) Rotary fluid pump
US2130299A (en) Radial pump
US2405938A (en) Multiple injection pump
DE2511365A1 (en) FUEL PUMP
US2341203A (en) Rotary engine
US2372559A (en) Fuel injection pump
US3168042A (en) Pumps, and in particular fuel injection pumps having opposed pistons and a rotary distributing valve element
US3058425A (en) Liquid fuel pumps for internal combustion engines
US1307282A (en) Internal-combustion engine
US2052737A (en) Fuel feed mechanism for internal combustion engines
US2759422A (en) Fuel injection apparatus
US2351908A (en) High-pressure pump
US4889096A (en) Fuel injection pump for internal combustion engines
US2445266A (en) Fuel pumping and distributing device
ES8103268A1 (en) Oil pump for small two=stroke engines - has reciprocating piston in cylinder offset in rotating distributor driven by worm gear
US3215080A (en) Multiple delivery pump apparatus
US6205980B1 (en) High-pressure delivery pump
US2813485A (en) Inking mechanisms for printing machines
US2053027A (en) Pump
US2901974A (en) Liquid fuel injection pumps for internal combustion engines
DE1601806A1 (en) Internal combustion engine with internal combustion and rotary piston
US3768929A (en) Liquid fuel injection pumping apparatus
EP0372238B1 (en) Fuel injection pump for internal-combustion engines
US1236275A (en) Rotary engine.