US2211496A - Injector nozzle - Google Patents

Injector nozzle Download PDF

Info

Publication number
US2211496A
US2211496A US279292A US27929239A US2211496A US 2211496 A US2211496 A US 2211496A US 279292 A US279292 A US 279292A US 27929239 A US27929239 A US 27929239A US 2211496 A US2211496 A US 2211496A
Authority
US
United States
Prior art keywords
plunger
fuel
engine
compression
passage
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
US279292A
Inventor
Jr Andrew J Davidson
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 US279292A priority Critical patent/US2211496A/en
Application granted granted Critical
Publication of US2211496A publication Critical patent/US2211496A/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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/023Injectors structurally combined with fuel-injection pumps characterised by the pump drive mechanical
    • 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
    • F02M59/10Pumps 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 the piston-drive
    • F02M59/102Mechanical drive, e.g. tappets or cams
    • 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
    • F02M59/243Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke caused by movement of cylinders relative to their pistons
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18992Reciprocating to reciprocating

Definitions

  • This invention relates to fuel injectors for internal combustion engines, and. has particular reference to an improved unitary injector, such as disclosed in my copending application, S. N.
  • the principal object of this invention is to generally improve fuel injectors of the characterv referred to.
  • Another object of the present invention is to provide a simplified control for the by-passing of fuel through the nozzle.
  • Another object of the invention is to simplify the structure described in my copending application, referred to above, so that the device may be '16 more easily assembled and taken apart for inview illistrates the relative position ofthe various par at the beginning of an injection stroke.
  • 25y Fig. 2 is a vertical section taken substantially on the line 2-2 of Fig. l.
  • Fig. 3 is a vertical section taken substantially on the line 3--3 of Fig. 1.
  • Fig. 4 is an enlarged fragmentary detail illus- 30 trating the roller and wedge assembly for moving the plunger.
  • Fig. 5 is an enlarged fragmentary detail in section, which illustrates the relation of the various parts upon the completion of the injectionstroke.
  • Fig. 6 is an enlarged fragmentary detail lof a portion of the plunger, illustrating the relation of the delivery valve assembly and the by-pass port.
  • the device embodying my present invention consists of a cylindrical body member 1, which may be made of any suitable material, and machined to tightly fit into a the cylinder blockl of an engine; a fragmentary portion of which is indicated by the' reference character I0.
  • the body 1 isA preferably secured 'in position by Ameans of bolts II, which extend through the end 50 plate I2, and vinto internally threaded recesses 'I3 that part of the passage-way 34, formed in the recess 8, bored in a boss 9 formed on the side of (ci. 10s- 41) body 1 is bored as at I8, and counter-bored, as as I9, in which bores are positioned the working parts of my device. 4 f
  • a plunger is mounted for reciprocation in the bore I8.
  • the plunger 20 is provided with an 5 internal bore 2l, which is adapted to accommodate thevflxed core I4.
  • the core I4 is provided with compression rings 22, and the plunger 20 is providedY with compression rings 23, to provide against leaks. y
  • is threaded, as at 24, and is arranged to receive a threaded plug'25, which in turn, is provided with an internal 'passage-way 26. Between the plug and the end of the bore 2
  • a delivery valve 28 mounted a delivery valve 28.
  • the valve 28 is provided with angularly positioned passage-ways 29, which are arranged to communicate with the passage-way 26 in the plug 25.
  • a compression spring 30 is arranged to normally maintain the 20 valve 28 in a closed position, as shown in Fig. l.l The compression of this spring must be sufficient to allow a predetermined pressure to be built up in chamber 3l, which is formed between the end of the core I4 and the plug 25. The greater 25 the pressure in chamber 3
  • a burner plate y32 is threadedly mounted in an internally threaded recess formed in the end of the plunger 20,
  • the compression chamber 3l communicates at one side with a passage-way 34, which extends through the plunger 2Il and the body 1, and whichl 35 in turn is connected to a fuel transfer pump (not shown) which moves the fuel'from the main fuel tank. That part of the passage-way 34, which is in the plunger 20, is in the form of an arcuate slot, so that there is always communication with body 1, no matter to what position the plunger 2U is rotated.
  • the other side of the compression chamber 3l communicates with a triangular shapedport 35 (Fig. 6) formedin the plunger 45 barrel 20, which is adapted to communicate with the passage-way 36 which extends through the 4 body 1 and is connected, to the fuel tank, as hereinafter described.
  • the plunger 2U is normally held in the position illustrated in Fig. 1, by means of the compression spring 40, which is mounted around the core I4 and abuts at either end against the retaining elements 4
  • a yoke 44 upon the end of each arm of which is a Wedge shaped member 45 adapted to be inserted between two sets of rollers 46 and 41, arranged as shown' in Figs. 1 and 4.
  • the rollers 46 are mounted on axles 48, which are journaled in bearing .members 49, which are secured to the body member 1 by suitable screws 5D.
  • rollers 41 are supported on axles 5
  • L 'I'he ring 52 is retained on one side by the shoulder 53, and on the other side by a retainer 54, the latter being grooved to accommodate ball bearings55.
  • is held in predetermined position by means of the lock member 56.
  • the yoke 44 is mounted at the end of a push rod, which is adapted to be actuated by a suitable timed cam (not shown), which is mounted on the engine to which vthe device is attached.
  • the wedge shaped elements 45 when moved by the push rod,.cause the rollers 41 to separate from the rollers 46, thereby causing the plunger 28 to be moved against the compression of the spring 40.
  • the cam accommodating the wedge 45 is timed to operate, and causes the plunger 20 to start to move away from the combustion chamber of the engine as the compression reaches its maximum in the cylinder of the engine.
  • the compression in the spring 40 will lbe adjusted so that it will just overcome the maximum compression pressure in the combustion chamber of the engine cylinder, so'as to normally hold the plunger 20 in the position as shown in Fig. 1. f
  • the operating cycle of my device is as :follows: Fuel is pumped to the device by means of the usual transfer pump (not shown) where it enters the passageway 34 and through which it travels to the compression chamber 3
  • the by-pass clearance between the port 35 and the by-pass outlet 36 is Veither increased or diminished.
  • the by-pass clearance is decreased, there is an increased amount of fuel injected through the valve 28 into the engine; and as the by-pass clearance is increased, there is a decreased amount of fuel forced through the valve 28 into the engine.
  • a 1 in a device of the character described, including a body member having a plunger reciprocable therein, and a compression chamber in said plunger, the combination of an intake passage-way in said body member and said plunger, in communication with the compression chamber in said plunger, and a by-pass port in said plunger communicating with said compression chamber and an outlet line, said by-pass port being arranged to be opened and closed upon the radial movement of said plunger, and means for moving said plunger axially and means for moving said plunger radially, at least a portion of each of said means, being housed within an extension of said body member.
  • a device of the character described including a body member having a plunger reciprocable therein, and a compression chamber in said plunger, the combination of an intake passage-way in said body member and said plunger, in communication with the compression chamber in said plunger, and a by-pass port in said plunger communicating with said compression chamber and an outlet, line, said by-pass port being arranged to be opened and closed upon the radial movement' oi said plunger, means for' moving said plunger axially and means for moving said plunger radially, at least a portion of each of said means, being housed within an extension of said body member, and another portion oi each of said means extending through the Walls of said body member.
  • a device of the'character described including a body member having a plunger reciprocable therein,A and a compression chamber in said plunger, the combination of a fuel intake communicating with said compression chamber, a by-pass port in said plunger arranged to be opened and closed by the radial movement of said plunger, a counter-bore in said body vmemr ber, and a rack and pinion in said counter-bore,
  • said rack extending through the walls of said body member and said pinion being secured to said plunger.
  • wedge shaped elements arranged to be driven betweenA the said pairs'of rollers,'and means extending through -the walls of said body member and arranged to move said wedge shaped elements.

Description

Aug 13, 1940- A. J. DAVIDSON, JR 2,211,496
' INJECTOR NOZZLE I Filed June l5, 1939 4 Za J0 Vig@ 6 /4 f .28,30 t '25 Patented Aug. 13, 1940 UNITED STATES PATENT oEFlcE INJEo'rolt NozzLE Andrew J. Davidson, Jr., Detroit-.Mich n Application June is, 1939, serial No. 279,292
e claims.
This invention relates to fuel injectors for internal combustion engines, and. has particular reference to an improved unitary injector, such as disclosed in my copending application, S. N.
162,185, filed Sept. 2, 1937.-
The principal object of this invention is to generally improve fuel injectors of the characterv referred to.
Another object of the present invention is to provide a simplified control for the by-passing of fuel through the nozzle.
Another object of the invention is to simplify the structure described in my copending application, referred to above, so that the device may be '16 more easily assembled and taken apart for inview illistrates the relative position ofthe various par at the beginning of an injection stroke. 25y Fig. 2 is a vertical section taken substantially on the line 2-2 of Fig. l.
Fig. 3 is a vertical section taken substantially on the line 3--3 of Fig. 1.
Fig. 4 is an enlarged fragmentary detail illus- 30 trating the roller and wedge assembly for moving the plunger.
Fig. 5 is an enlarged fragmentary detail in section, which illustrates the relation of the various parts upon the completion of the injectionstroke.
Fig. 6 is an enlarged fragmentary detail lof a portion of the plunger, illustrating the relation of the delivery valve assembly and the by-pass port. A
Referring now more particularly to the drawing, it will be understood that the device embodying my present invention consists of a cylindrical body member 1, which may be made of any suitable material, and machined to tightly fit into a the cylinder blockl of an engine; a fragmentary portion of which is indicated by the' reference character I0.
The body 1 isA preferably secured 'in position by Ameans of bolts II, which extend through the end 50 plate I2, and vinto internally threaded recesses 'I3 that part of the passage-way 34, formed in the recess 8, bored in a boss 9 formed on the side of (ci. 10s- 41) body 1 is bored as at I8, and counter-bored, as as I9, in which bores are positioned the working parts of my device. 4 f
A plunger is mounted for reciprocation in the bore I8. The plunger 20 is provided with an 5 internal bore 2l, which is adapted to accommodate thevflxed core I4. The core I4 is provided with compression rings 22, and the plunger 20 is providedY with compression rings 23, to provide against leaks. y
The internal bore 2| .is threaded, as at 24, and is arranged to receive a threaded plug'25, which in turn, is provided with an internal 'passage-way 26. Between the plug and the end of the bore 2| is a restricted area 21, in which is slidably 15.
mounted a delivery valve 28. The valve 28 is provided with angularly positioned passage-ways 29, which are arranged to communicate with the passage-way 26 in the plug 25. A compression spring 30 is arranged to normally maintain the 20 valve 28 in a closed position, as shown in Fig. l.l The compression of this spring must be sufficient to allow a predetermined pressure to be built up in chamber 3l, which is formed between the end of the core I4 and the plug 25. The greater 25 the pressure in chamber 3|, the better 'the fuel will be atomized during delivery. A burner plate y32 is threadedly mounted in an internally threaded recess formed in the end of the plunger 20,
and has a small axial passage-way 33, arranged 30 to communicate with a similar, -but larger in diameter, axial passage-way formed in the plunger 20. The compression chamber 3l communicates at one side with a passage-way 34, which extends through the plunger 2Il and the body 1, and whichl 35 in turn is connected to a fuel transfer pump (not shown) which moves the fuel'from the main fuel tank. That part of the passage-way 34, which is in the plunger 20, is in the form of an arcuate slot, so that there is always communication with body 1, no matter to what position the plunger 2U is rotated. The other side of the compression chamber 3l communicates with a triangular shapedport 35 (Fig. 6) formedin the plunger 45 barrel 20, which is adapted to communicate with the passage-way 36 which extends through the 4 body 1 and is connected, to the fuel tank, as hereinafter described.
In order to control the amount of fuel to be by-passed from the compression chamber 3l, I provide an improved control means, which I will now describe. In order to more effectively control the by-passing of the fuel from the: compression chamber 3l, I'provide for the ro- 55 tation, on its longitudinal axis, of the plunger 20 through an arc suicient to open and close the port 35. This rotation is accomplished by means of the rack and pinion illustrated in Fig. 3. The rack 31 is slidably supported by suitable apertures 38, formed in the enlarged portion |1 of the body member 1. The pinion 39 is presstted on to the plunger barrel 28. 'I'he rack 31 is connected to manually operable means (not shown), and as the rack 31 is moved, it causes the rotation of the plunger 20, corresponding to the degree of the movement.
The plunger 2U is normally held in the position illustrated in Fig. 1, by means of the compression spring 40, which is mounted around the core I4 and abuts at either end against the retaining elements 4| and 42. Adjustment is made in the compression of the spring 40 by means of the adjusting screw 43, and threadedly engages a suitable boss formed on the inside of the end plate l2.
'I'he movement of the plunger 20 away from the engine block is accomplished by the means which are now described. I provide a yoke 44 (Fig. 3), upon the end of each arm of which is a Wedge shaped member 45 adapted to be inserted between two sets of rollers 46 and 41, arranged as shown' in Figs. 1 and 4. The rollers 46 are mounted on axles 48, which are journaled in bearing .members 49, which are secured to the body member 1 by suitable screws 5D. The rollers 41 are supported on axles 5| formed on the ring 52, which is freely mounted on a reduced section of the plunger 2|).L 'I'he ring 52 is retained on one side by the shoulder 53, and on the other side by a retainer 54, the latter being grooved to accommodate ball bearings55. The retaining element 4| is held in predetermined position by means of the lock member 56.
The yoke 44 is mounted at the end of a push rod, which is adapted to be actuated by a suitable timed cam (not shown), which is mounted on the engine to which vthe device is attached. The wedge shaped elements 45, when moved by the push rod,.cause the rollers 41 to separate from the rollers 46, thereby causing the plunger 28 to be moved against the compression of the spring 40. It will be understood that the cam accommodating the wedge 45, is timed to operate, and causes the plunger 20 to start to move away from the combustion chamber of the engine as the compression reaches its maximum in the cylinder of the engine. The compression in the spring 40 will lbe adjusted so that it will just overcome the maximum compression pressure in the combustion chamber of the engine cylinder, so'as to normally hold the plunger 20 in the position as shown in Fig. 1. f
The operating cycle of my device is as :follows: Fuel is pumped to the device by means of the usual transfer pump (not shown) where it enters the passageway 34 and through which it travels to the compression chamber 3|. y As the plunger 20 is moved away from the engine, under the influence of the properly timed cam operated wedges 45,- the fuel in the compression chamber 3| can only escape in two directions; either through thefby-pass port 35 into the passage-way 36 and hence to the fuel tank or supply line, ory through the axialpassage-way 26, formed in the plug 25 and through the angular passage-ways 29, formed in the valve 28 and into the space betweenthe valve 28 and the end of the bore 2|, and hence through the axial passage-Way in the plunger 20, and the burner plate 32 and into the combustion chamber of the engine. By rotating the plunger 20, the by-pass clearance between the port 35 and the by-pass outlet 36, is Veither increased or diminished. As the by-pass clearance is decreased, there is an increased amount of fuel injected through the valve 28 into the engine; and as the by-pass clearance is increased, there is a decreased amount of fuel forced through the valve 28 into the engine. As illustrated in Fig. -5, I prefer, at all times, to maintain a slight by-pass between the port 35 into the passage-way 36, so as to release the pressure back of the discharge valve 28 at the iinish of an injection stroke.
As the plunger 20 is moved away from the engine, the rst part df the stroke is ineffective to discharge oil past the valve 28, for in this position the by-pass port 35 is open and the fuel will be by-passed through the passage-way 36. As the plunger 20 continues its movement away from the engine, the by-pass will be reduced. thereby building up pressure in the chamber 3|. While the by-pass port 35 remains open, the outlet ports of the angular passage-ways 29 in the valve 28 are still covered by the Walls of the restricted area 21.' As the plunger 20 continues to move away from the engine, the opening in the by-pass port 35 will be reduced and almost closed, thereby building up pressure in the chamber 3|, at which time therunrestricted area of the internal bore of the plunger 20 communicates with the outlet ports of the valve 28, thus permitting the fuel to pass around the end of the valve 28 and hence into the axial passageway 33, -formed in the plunger 20, and hence into the combustion chamber of the engine.
When the plunger 20 reaches the end of its travel away from the engine, which position is shown in Fig. 5, the compression in the chamber 3|' is reduced to a minimum, thereby permitting the delivery valve 28 to be returned to its normal position under the influence of the spring 3B. In this position it is evident that no more fuel will be discharged into the combustion chamber of the engine, as the walls of the restricted area of the bore 2|, close the angular passageways 29, in the valve 28. When the plunger 20 reaches the position shown in Fig. 5, it will be returned to `the position shown in Fig. 1, by means of the spring 40, and the cycle is completed.
Having described my invention, what I claim and desire to secure by Letters Patent is:
A 1. In a device of the character described, including a body member having a plunger reciprocable therein, and a compression chamber in said plunger, the combination of an intake passage-way in said body member and said plunger, in communication with the compression chamber in said plunger, and a by-pass port in said plunger communicating with said compression chamber and an outlet line, said by-pass port being arranged to be opened and closed upon the radial movement of said plunger, and means for moving said plunger axially and means for moving said plunger radially, at least a portion of each of said means, being housed within an extension of said body member.
,2. In a device of the character described, including a body member having a plunger reciprocable therein, and a compression chamber in said plunger, the combination of an intake passage-way in said body member and said plunger, in communication with the compression chamber in said plunger, and a by-pass port in said plunger communicating with said compression chamber and an outlet, line, said by-pass port being arranged to be opened and closed upon the radial movement' oi said plunger, means for' moving said plunger axially and means for moving said plunger radially, at least a portion of each of said means, being housed within an extension of said body member, and another portion oi each of said means extending through the Walls of said body member.
3. In a device of the'character described, including a body member having a plunger reciprocable therein,A and a compression chamber in said plunger, the combination of a fuel intake communicating with said compression chamber, a by-pass port in said plunger arranged to be opened and closed by the radial movement of said plunger, a counter-bore in said body vmemr ber, and a rack and pinion in said counter-bore,
said rack extending through the walls of said body member and said pinion being secured to said plunger.
4. The combination dened in claim 3, including two pairs of rollers within said counter-bore,
one pair being secured to said body- 1 member and-one pair being secured to said plunger, wedge shaped elements arranged to be driven betweenA the said pairs'of rollers,'and means extending through -the walls of said body member and arranged to move said wedge shaped elements.
5. In a device of the character described. in-
cluding a body member having a cylindricalI plungerreciprocable therein, a fixed core telesooped by said plunger, and a compression chamber between the core and one end of said plunger,
the combination of a fuel intake communicating -to engage a' control rack, which is directly actuated from without the said body member.l
'i ANDREW J. DAVIDSON, an.
with said compression chamber, an angular byv
US279292A 1939-06-15 1939-06-15 Injector nozzle Expired - Lifetime US2211496A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US279292A US2211496A (en) 1939-06-15 1939-06-15 Injector nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US279292A US2211496A (en) 1939-06-15 1939-06-15 Injector nozzle

Publications (1)

Publication Number Publication Date
US2211496A true US2211496A (en) 1940-08-13

Family

ID=23068368

Family Applications (1)

Application Number Title Priority Date Filing Date
US279292A Expired - Lifetime US2211496A (en) 1939-06-15 1939-06-15 Injector nozzle

Country Status (1)

Country Link
US (1) US2211496A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2464288A (en) * 1945-04-21 1949-03-15 Vernon C Belt Fuel injection means for combustion engines
US2516692A (en) * 1946-09-23 1950-07-25 Louis O French Fuel injector
US2518901A (en) * 1945-01-15 1950-08-15 Edward H King Engine pressure actuated injector
US2547174A (en) * 1946-07-03 1951-04-03 Gardiner M Rogers Fuel injector mechanism
US2588481A (en) * 1942-07-22 1952-03-11 Niles Bement Pond Co Fuel injector pump mechanism
US2599018A (en) * 1946-07-26 1952-06-03 Gardiner M Rogers Fuel injector
US2759770A (en) * 1952-04-17 1956-08-21 Gen Motors Corp Fuel injector
US2821926A (en) * 1954-06-28 1958-02-04 Cessna Aircraft Co Variable volume reciprocating pump
WO2017144987A1 (en) 2016-02-26 2017-08-31 Rpartner S.R.O. A way of person transportation and facilities for providing this way of transport

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2588481A (en) * 1942-07-22 1952-03-11 Niles Bement Pond Co Fuel injector pump mechanism
US2518901A (en) * 1945-01-15 1950-08-15 Edward H King Engine pressure actuated injector
US2464288A (en) * 1945-04-21 1949-03-15 Vernon C Belt Fuel injection means for combustion engines
US2547174A (en) * 1946-07-03 1951-04-03 Gardiner M Rogers Fuel injector mechanism
US2599018A (en) * 1946-07-26 1952-06-03 Gardiner M Rogers Fuel injector
US2516692A (en) * 1946-09-23 1950-07-25 Louis O French Fuel injector
US2759770A (en) * 1952-04-17 1956-08-21 Gen Motors Corp Fuel injector
US2821926A (en) * 1954-06-28 1958-02-04 Cessna Aircraft Co Variable volume reciprocating pump
WO2017144987A1 (en) 2016-02-26 2017-08-31 Rpartner S.R.O. A way of person transportation and facilities for providing this way of transport

Similar Documents

Publication Publication Date Title
US2282562A (en) Diesel engine fuel pump
GB1366048A (en) Fuel injection pump for multi-cylinder internal combustion engines
US2211496A (en) Injector nozzle
US2863438A (en) Timing of fuel injection pumps
US2576451A (en) Fuel injection pump
US2410947A (en) Fuel injection pum mechanism
US2590575A (en) Fuel injector
US3319616A (en) Liquid fuel pumps for use with internal combustion engines
KR890701896A (en) Fuel injection pump
US3023705A (en) Injection pump
US2424943A (en) Fuel pump
US2251783A (en) Fuel pump for engines
US2547174A (en) Fuel injector mechanism
US4458643A (en) Lubricating oil feeding device for fuel injection pumps
DE3843467A1 (en) FUEL INJECTION DEVICE FOR INTERNAL COMBUSTION ENGINES
US2989003A (en) Liquid fuel pumps for internal combustion engines
US2670684A (en) Fuel injection device for internalcombustion engines
US2912935A (en) Fuel injection pump
US3237568A (en) Fuel injection pump with pneumatic damper
US3101079A (en) Liquid fuel pumps for internal combustion engines
US3138103A (en) Fuel supplying mechanism
US3309024A (en) Fuel delivery valve and injection apparatus employing same
US4594988A (en) Method for building or repairing rotary injection fuel pump piston cylinders
US2398834A (en) Fuel injection in internalcombustion engines
US2251552A (en) Fuel injection pump