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

US1361711A - Fuel-injector for high-compression internal-combustion engines - Google Patents

Fuel-injector for high-compression internal-combustion engines Download PDF

Info

Publication number
US1361711A
US1361711A US248257A US24825718A US1361711A US 1361711 A US1361711 A US 1361711A US 248257 A US248257 A US 248257A US 24825718 A US24825718 A US 24825718A US 1361711 A US1361711 A US 1361711A
Authority
US
United States
Prior art keywords
fuel
piston
passageway
valve
combustion chamber
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
US248257A
Inventor
Waldo G Gernandt
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.)
GERNANDT MOTOR Corp
Original Assignee
GERNANDT MOTOR CORP
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 GERNANDT MOTOR CORP filed Critical GERNANDT MOTOR CORP
Priority to US248257A priority Critical patent/US1361711A/en
Application granted granted Critical
Publication of US1361711A publication Critical patent/US1361711A/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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D1/00Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T1/00Details of spark gaps
    • H01T1/16Series resistor structurally associated with spark gap
    • 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
    • F02M2700/07Nozzles and injectors with controllable fuel supply
    • F02M2700/078Injectors combined with fuel injection pump

Definitions

  • This invention relates to fuel injectors adapted to be used in single or multiple cylinder high compression internal combustion engines'
  • One object of the invention is to obtain a fuel injector whereby the speed or work ofthe engine iscontrolled by the'manipulation thereof; and to accomplish said object, the fuel injectoris made so that by said manipulation the quantity of fuel discharged thereby, at timed intervals, into the combustion chamber of the engine is controlled, being lessened or increased as the exigency of the occasion demands.
  • Figure 1 is a vertical sectional view ofthe u per end of an engine cylinder, showin vertical section), a fuel injector embodying my invention mounted thereon;
  • Fig. 4c is a vertical section of a modification of the construction embodying the invention which is illustrated in Figs. 1 and 3, on line 44 of Fig. 5, and viewed in the dire'tion indicated by the arrows; and
  • Fig. 5 is a side elevation of camways forming elements of the construction which is illustrated in Fig. 4.-
  • A represents an engine cylinder provided with the water space a, combustion chamber B, piston C, connecting rod D, pivotally attached to piston C by pin d, and the ordi-- nary spring rings F, Fig. 2, represents the inlet valve and stem of the combustion chamber of the engine.
  • H represents the discharge end of the fuel injector embodying the invention, 72. being radial apertures thereto positioned in the combustion chamber B, in a plane adjacent to the plane of the end of the piston 0, when said piston is at the end of its extreme inward movement or travel.
  • 1, represents a fuel supply tank.
  • J represents a supply pipe or tube connecting the fuel supply tank I, as by union '3', to the inlet end of a fuel injector embodying this invention.
  • K represents a check valve which comprises a 'ball arranged to permit the flow from the pipe J to the passagewayL of the fuel injector.
  • the passageway L is illustrated in Fig. 1 as having two legs one thereof positioned at a right angle to the other, and M, represents a needle valve which is adapted, when closed, to obstruct the discharge end of said passageway L. 'lhe timing of the closing of needle valve M on its seat, relative to the piston C, and to the combustion which occurs in the combustion chamber B, is such that said valve is closed immediately after the ignition of fuel in said combustion (hamber, while said piston is in the pre-determined position to be actuated by said ignition.
  • N represents a pump cylinder and O. a longitudinally movable piston in said pump cylinder.
  • P represents a lever which is pivotally mounted on pin Q, and said pin Q, is illustrated as mounted on the eccentric g.
  • Q represents a standard, 100
  • standard Q and 9 represents 105 a handle which is attached to'eccentric g, to control the position thereof in said stan ard.
  • R represents a rotatably mounted shaft which, in the constructions illustrated, may no i P is provided with a roller, S, with which roller the cam runway r engages and by means of which said end of lever P 1s advanced and retracted.
  • the opgosite end of said lever P is forked, as at in Fig. 1.
  • valve M The upper end of the valve M is engaged by the forked end S of said lever P.
  • S" represents a spring which is mounted on valve M so that the lower end thereof abuts against the annular flange m on said valve M, and the upper end abuts against the lever P.
  • interposing of said spring S between the forked end S of lever P and the shoulder m on valve M is to obtain some compression of said spring on the seating of end m of said valve.
  • T represents a link which is pivotally mounted on one end of the lever P, and the pin or pivot which connects said link to said lever is illustrated in Fig. 1 as being the pivot t on which the roller S is rotatably mounted.
  • U, Fig. 1 represents a member which is mounted on the upper end of piston O, and at its upper end is attached to the link T by pin to.
  • the piston O is provided with slot, V and the member U is provided with a pin, which is positioned in slot V. sents a spring which is interposed between the upper end of piston O and member U.
  • the movement of the lever P is communicated to piston 0 when the pressure in pum cylinder N (and passageway L) is not su cient to overcome the resiliency of the spring W; and when said pressure in said pump cylinder N is suflicient to overcome the resiliency of said spring, the member U advancing on the upper end of said spring W compresses said spring without producing corresponding advancing movement of piston O; the pin V, at such time, moving in slot V.
  • the camway 7' is timed relative to the W reprev piston C, to retract piston 0 when piston C is advanced to near the position where a low pressure is obtained in the engine cylinder and combustion chamber, and at said time the pressure in the pump cylinder N and passageway L between check valve K and the seated valve M is less than the pressure at the discharge end of the fuel discharge pipe J; and at said time fuel flows from said supply pipe through check valve K into passageway L.
  • Said camway 1' is also so constructed and timed relative to said piston C that when said piston C moves toward the combustion chamber to its point of maximum travel, thereby producing the greatest pressure which is obtained in said combustion chamber prior to ignition, piston O is advanced. This is effected as piston C approaches the end of its compression travel, by lever P, which is moved by cam runway 1- so that the forked end S thereof is brought into contact with shoulder m, and continued movement of said lever unseats valve M. The travel of forked end S before said end contacts with shoulder m is varied by the position of pivot Q, and said variation, as hereinbefore stated, is obtained by mov-- ing the eccentric g by means of handle g.
  • the camways 1*, 1'" are so constructed that there is quick retraction of the pistons O, O", at timed intervals, an advancing movement of one of said pistons at all times, and advancing movement of both of said pistons most of the time.
  • the compression of the contents of pump cylinders O, O and the discharge thereof into passageways 'X, L and L, is, therefore, practically continuous, and the pressure so obtained is greater than the pressure in the combustion chamber B prior to the ignition therein.
  • the passageway L extends to a plurality of passageways L, said passageways L forming branches of the passageway L, respectively communicating at the discharge ends thereof with a corresponding combustion chamber of the engine; and each of said branches is provided With apvalve M, which is in timed relation to the correspond- Said modiing engine piston, as the construction illustrated in Figs, 1, 2 and 3.
  • a fuel injector comprising, in combination, a passageway provided with branches, the discharge ends whereof communicate with the combustion chambers of an engine provided with a plurality of cylinders and movable pistons, means to obstruct said branches, means to supply fuel to said passageway, yielding means to obtain a pre-determined maximum pressure in said passageway and branches, and means to remove said obstructions in timed relation to said pistons.
  • A- fuel injector comprising, in combination, a passageway provided with branches, the discharge ends whereof communicate with the combustion chamber of an engine provided with a plurality of cylinders and movable pistons, means to obstruct said branches, means to supply fuel to said passageway, yielding means to obing means to vary the timed relation the duration and the extent of said removal.
  • a fuel injector comprising, in combination, a passageway the discharge end whereof communicates with the combustion chamber of an engine provided with a cyl-' inder and movable piston therein, means to obstruct said passageway, means to supply fuel to said passageway, yielding means to obtain a predetermined maximum pressure in said passageway, said means'comprising a longitudinally movable piston, means to actuate said piston and a resilient member interposed between said actuating means.
  • a fuel injector comprising, in combination, a passageway the discharge end whereof communicates with the combustion chamber of an engine provided with a cylinder and movable piston therein, means to obstruct said passageway, means tosupply fuel to said passageway, yielding means to obtain a predetermined maximum pressure in said passageway, said means comprising a longitudinally movable piston, means to actuate said piston and a resilient member interposed between said actuating means, independent of said means to establish maximum pressure, and said piston and means to remove.
  • said obstruction in timed relation to saidpiston, said removing means comprising means to vary the timed relation, the duration and the extent of said removal.
  • a fuel injector comprising, in combination, a passageway provided with branches the discharge ends whereof communicate with the combustion chambers of an engine provided with a plurality of chambers and movable pistons, means to obstruct said branches of said passageway, means to supply fuel to said passageway, yielding means to obtain a pre-determined maximum pressure in said passageway, said yielding means comprising longitudinally movable pistons, means to actuate said pistons, and resilient members interposed between said actuating means and said pistons, said actuating means arranged so that one thereof is at all times advancing, and means to remove said obstruction in timed relation to said piston.

Landscapes

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

Description

W. G. GERNANDT. FUEL INJECTOR FOR HIGH COMPRESSION INTERNAL COMBUSTION ENGINES.
APPLICATION FILED AUG.5. 1918.
. [N VENTOR) mzm 03,
Patented Dec. 7, 1920.
1 A TTORNE Y.
.ing
UNITED" STATES PATENT OFFICE.
WALDO G. GERNANDT, OF CHICAGO, ILLINOIS, ASSIGNOR TO GERNAND'I' MOTOR I CORPORATION, OF CHICAGO, ILLINOIS, A CORPORATION OF ILLINOIS.
' FUEL-INJECTOR FOB. HIGH-COMPRESSION INTERNAL-COMBUSTION'ENGINES.
Specification of Letters Patent.
Application filed August 5, 1918. Serial No. 248,257.
To all whom it may concern:
Be it known that I, WALDO G. GERNANDT, a citizen of the United States, and a resident of Chicago, in the county of Cook and State of Illinois, have invented certain new and useful Improvements in Fuel-Injectors for High-Compression Internal-Combustion Engines, of which the following is a specificatlon.
.This invention relates to fuel injectors adapted to be used in single or multiple cylinder high compression internal combustion engines' One object of the invention is to obtain a fuel injector whereby the speed or work ofthe engine iscontrolled by the'manipulation thereof; and to accomplish said object, the fuel injectoris made so that by said manipulation the quantity of fuel discharged thereby, at timed intervals, into the combustion chamber of the engine is controlled, being lessened or increased as the exigency of the occasion demands.
A further object of the invention is to obtain a device whereof the operation is continuous and the determined maximum pressure at which fuel is inje ted into said combustion chamber, or chambers, is not increased by said continuous operation.
Additional objects are disclosed in the specification and claims.
I have illustrated devices embodying this invention in the drawing accompanying and forming a part hereof in which,
Figure 1, is a vertical sectional view ofthe u per end of an engine cylinder, showin vertical section), a fuel injector embodying my invention mounted thereon;
Fig. 2 a like section of an engine 'cylinder, at an angle of ninety degrees from the illustration in Fig. 1, showing the discharge end of the fuel injector in elevation and Fig. 3, a vertical section of the upper end of the construction embodying the invention which is illustrated in Fig. 1.
Fig. 4c is a vertical section of a modification of the construction embodying the invention which is illustrated in Figs. 1 and 3, on line 44 of Fig. 5, and viewed in the dire'tion indicated by the arrows; and
Fig. 5 is a side elevation of camways forming elements of the construction which is illustrated in Fig. 4.-
A reference character applied to designate agiven part indicates saldpart throughout the several figures of the drawing, whereever the same appears.
A, represents an engine cylinder provided with the water space a, combustion chamber B, piston C, connecting rod D, pivotally attached to piston C by pin d, and the ordi-- nary spring rings F, Fig. 2, represents the inlet valve and stem of the combustion chamber of the engine. H, represents the discharge end of the fuel injector embodying the invention, 72. being radial apertures thereto positioned in the combustion chamber B, in a plane adjacent to the plane of the end of the piston 0, when said piston is at the end of its extreme inward movement or travel. 1, represents a fuel supply tank. J represents a supply pipe or tube connecting the fuel supply tank I, as by union '3', to the inlet end of a fuel injector embodying this invention. K, represents a check valve which comprises a 'ball arranged to permit the flow from the pipe J to the passagewayL of the fuel injector. The passageway L, is illustrated in Fig. 1 as having two legs one thereof positioned at a right angle to the other, and M, represents a needle valve which is adapted, when closed, to obstruct the discharge end of said passageway L. 'lhe timing of the closing of needle valve M on its seat, relative to the piston C, and to the combustion which occurs in the combustion chamber B, is such that said valve is closed immediately after the ignition of fuel in said combustion (hamber, while said piston is in the pre-determined position to be actuated by said ignition. Said position-ofthe pi ton may be when it is substantially on what is termed its dead center and it is so illustrated in the drawing. N, Fig. 1,represents a pump cylinder and O. a longitudinally movable piston in said pump cylinder. P, represents a a lever which is pivotally mounted on pin Q, and said pin Q, is illustrated as mounted on the eccentric g. Q represents a standard, 100
upper end of standard Q and 9 represents 105 a handle which is attached to'eccentric g, to control the position thereof in said stan ard.
R, represents a rotatably mounted shaft which, in the constructions illustrated, may no i P is provided with a roller, S, with which roller the cam runway r engages and by means of which said end of lever P 1s advanced and retracted. The opgosite end of said lever P is forked, as at in Fig. 1.
The upper end of the valve M is engaged by the forked end S of said lever P. S" represents a spring which is mounted on valve M so that the lower end thereof abuts against the annular flange m on said valve M, and the upper end abuts against the lever P. By this construction the valve M is advanced and retracted by the pivotal movement of lever P, the advancing movement of said valve being imparted thereto through the said spring S", and said retracting movement being applied directly to shoulder m by the forked end S. The
. interposing of said spring S between the forked end S of lever P and the shoulder m on valve M is to obtain some compression of said spring on the seating of end m of said valve.
T, represents a link which is pivotally mounted on one end of the lever P, and the pin or pivot which connects said link to said lever is illustrated in Fig. 1 as being the pivot t on which the roller S is rotatably mounted. U, Fig. 1, represents a member which is mounted on the upper end of piston O, and at its upper end is attached to the link T by pin to.
The piston O, is provided with slot, V and the member U is provided with a pin, which is positioned in slot V. sents a spring which is interposed between the upper end of piston O and member U.
By the construction last above described, the movement of the lever P is communicated to piston 0 when the pressure in pum cylinder N (and passageway L) is not su cient to overcome the resiliency of the spring W; and when said pressure in said pump cylinder N is suflicient to overcome the resiliency of said spring, the member U advancing on the upper end of said spring W compresses said spring without producing corresponding advancing movement of piston O; the pin V, at such time, moving in slot V.
It will be observed that the pressure in the pump cylinder N and in the passa eway L between check valve K and valve lVI, said valve being seated, is at all times equal, and that when said pressure is greater than the pressure in the' fuel supply pipe J it will close the check valve K, to prevent said pressure being communicated to said fuel supply pipe. v
The camway 7' is timed relative to the W reprev piston C, to retract piston 0 when piston C is advanced to near the position where a low pressure is obtained in the engine cylinder and combustion chamber, and at said time the pressure in the pump cylinder N and passageway L between check valve K and the seated valve M is less than the pressure at the discharge end of the fuel discharge pipe J; and at said time fuel flows from said supply pipe through check valve K into passageway L.
Said camway 1' is also so constructed and timed relative to said piston C that when said piston C moves toward the combustion chamber to its point of maximum travel, thereby producing the greatest pressure which is obtained in said combustion chamber prior to ignition, piston O is advanced. This is effected as piston C approaches the end of its compression travel, by lever P, which is moved by cam runway 1- so that the forked end S thereof is brought into contact with shoulder m, and continued movement of said lever unseats valve M. The travel of forked end S before said end contacts with shoulder m is varied by the position of pivot Q, and said variation, as hereinbefore stated, is obtained by mov-- ing the eccentric g by means of handle g. In the movement of the eccentric q and lever q in a contra'ry clock-wise direction, as viewed in Figs. 1 and 3, the timing of the opening of the valve M relative to piston C is changed, it being opened earlier; the extent of the said opening is changed, it being opened wider; and the duration of said opening is also changed, it being opened for a longer time. Said changes do not destroy the timed relation of the opening of valve M relative to the position of piston C, nor does said change of position of pivot Q destroy the timed relation of the advancing movement of piston 0, but the length of travel of said piston is increased, (see member U) correspondingly with the increased aperture through the valve seat of end m, and the longer period of time during which the valve M is unseated, so that the variation in the quantity of fuel supplied to the combustion chamber B varies with the above named variations in the movement of valve M.
Upon the advance of the piston O, by camway 1", the pressure in passageway L is increased sufficiently to force the contents thereof, (including the fuel therein) into said combustion chamber B through passageway h: and ignition of the fuel mixture obtained thereby will occur in said com bustion chamber because of the high temperature of the contents of said combustion chamber; and said temperature is produced by the quick compression of the air contents of an engine cylinder of large capacity into a combustion chamber of relatively small capacity, on the compression travel of the piston.
Where my invention is embodied in a con- I struction suchas is illustrated in Figs. 1
and 3 and hereinbefore described, and said constructlon is used in an engine having a plurality of piston cylinders and pistons, a"
comprising rollers 'S, 3"", members U,
U", pins V", V in slots V, and springs, W, W. Said modification is provided with the passageway X and check valves X, X interposed between the discharge end of cylinders N, N and the passageway L. Y represents fuel inlets to the cylinders N, N".
The camways 1*, 1'" are so constructed that there is quick retraction of the pistons O, O", at timed intervals, an advancing movement of one of said pistons at all times, and advancing movement of both of said pistons most of the time. The compression of the contents of pump cylinders O, O and the discharge thereof into passageways 'X, L and L, is, therefore, practically continuous, and the pressure so obtained is greater than the pressure in the combustion chamber B prior to the ignition therein.
In the constructions which are illustrated and described, the shaft R, camway 'r', and said shaft and camways 1", 1'" continuously rotate, and the maximum pressure in the pump cylinders N, N and N" which is obtainable by pistons O, O, O", is determined by the resiliency of the several springs W,
W and W".
In the constructions herein describedand illustrated fuel from the fuel receptacle I flows into the passageway L on the retraction of the pistons O, O, O and on the simultaneous advance of said pistons and retraction of valve M a quantity of said fuel corresponding with the advance of said pistons is injected from said passageway into the combustion chamber.
In the construction which is illustrated in Figs. 4 and 5, and herein before described, the passageway L extends to a plurality of passageways L, said passageways L forming branches of the passageway L, respectively communicating at the discharge ends thereof with a corresponding combustion chamber of the engine; and each of said branches is provided With apvalve M, which is in timed relation to the correspond- Said modiing engine piston, as the construction illustrated in Figs, 1, 2 and 3.
I claim 7 1. A fuel injector comprising, in combination, a passageway provided with branches, the discharge ends whereof communicate with the combustion chambers of an engine provided with a plurality of cylinders and movable pistons, means to obstruct said branches, means to supply fuel to said passageway, yielding means to obtain a pre-determined maximum pressure in said passageway and branches, and means to remove said obstructions in timed relation to said pistons.
2. A- fuel injector comprising, in combination, a passageway provided with branches, the discharge ends whereof communicate with the combustion chamber of an engine provided with a plurality of cylinders and movable pistons, means to obstruct said branches, means to supply fuel to said passageway, yielding means to obing means to vary the timed relation the duration and the extent of said removal.
3. A fuel injector comprising, in combination, a passageway the discharge end whereof communicates with the combustion chamber of an engine provided with a cyl-' inder and movable piston therein, means to obstruct said passageway, means to supply fuel to said passageway, yielding means to obtain a predetermined maximum pressure in said passageway, said means'comprising a longitudinally movable piston, means to actuate said piston and a resilient member interposed between said actuating means.
independent of said means to establish I maximum pressure, and said piston and means to remove said obstruction in timed relation to said piston actuating means.
4. A fuel injector comprising, in combination, a passageway the discharge end whereof communicates with the combustion chamber of an engine provided with a cylinder and movable piston therein, means to obstruct said passageway, means tosupply fuel to said passageway, yielding means to obtain a predetermined maximum pressure in said passageway, said means comprising a longitudinally movable piston, means to actuate said piston and a resilient member interposed between said actuating means, independent of said means to establish maximum pressure, and said piston and means to remove. said obstruction in timed relation to saidpiston, said removing means comprising means to vary the timed relation, the duration and the extent of said removal.
5. A fuel injector comprising, in combination, a passageway provided with branches the discharge ends whereof communicate with the combustion chambers of an engine provided with a plurality of chambers and movable pistons, means to obstruct said branches of said passageway, means to supply fuel to said passageway, yielding means to obtain a pre-determined maximum pressure in said passageway, said yielding means comprising longitudinally movable pistons, means to actuate said pistons, and resilient members interposed between said actuating means and said pistons, said actuating means arranged so that one thereof is at all times advancing, and means to remove said obstruction in timed relation to said piston.
6. A fuel injector comprising a passage way the discharge end whereof is communicable with the combustion chamber of an engine, and means to supply fuel to the receiving end of said passage way, in combination with a fulcrumed lever, means to vary the position of said fulcrum, and means to rock said lever on said fulcrum, a cylindrical member in communication with said passage way between said receiving and discharge ends, a plunger in said cylindrical member, said lever arranged to retract and to yieldingly advance said plunger,
and a valve arranged to normally obstruct the communicable end of said passage way, said lever arranged to retract and to yieldingly advance said valve.
WALDO G. GERNANDT.
In the presence of- CHARLES TURNER BROWN, J. SGUDDER.
US248257A 1918-08-05 1918-08-05 Fuel-injector for high-compression internal-combustion engines Expired - Lifetime US1361711A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US248257A US1361711A (en) 1918-08-05 1918-08-05 Fuel-injector for high-compression internal-combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US248257A US1361711A (en) 1918-08-05 1918-08-05 Fuel-injector for high-compression internal-combustion engines

Publications (1)

Publication Number Publication Date
US1361711A true US1361711A (en) 1920-12-07

Family

ID=22938327

Family Applications (1)

Application Number Title Priority Date Filing Date
US248257A Expired - Lifetime US1361711A (en) 1918-08-05 1918-08-05 Fuel-injector for high-compression internal-combustion engines

Country Status (1)

Country Link
US (1) US1361711A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2725863A (en) * 1951-12-07 1955-12-06 Sanders Arthur Freeman Drive for the fuel pump to a compression ignition engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2725863A (en) * 1951-12-07 1955-12-06 Sanders Arthur Freeman Drive for the fuel pump to a compression ignition engine

Similar Documents

Publication Publication Date Title
US2898051A (en) Fluid injection device
US3409225A (en) Mechanical injector having needleseating spring
US2625141A (en) Fuel injection method
US2980092A (en) Fuel injection pump
US1361711A (en) Fuel-injector for high-compression internal-combustion engines
US1890702A (en) Fuel injection device for internal combustion engines
US3104817A (en) Fuel injector with pilot injection
US2005008A (en) Fuel injection pump
GB1474961A (en) Fuel nozzle assembly for a compression ignition internal combustion engine and a' engine incorporating such a fuel nozzle assembly
US2588481A (en) Fuel injector pump mechanism
US2645182A (en) Fuel injector
US2548342A (en) Fuel injection pump for internalcombustion engines
US1668919A (en) Fuel-oil pump
US1497258A (en) Internal-combustion engine
US1451228A (en) Fuel-feeding device for internal-combustion engines
US2516690A (en) Automatic fuel injector
US1610997A (en) Fuel pump for internal-combustion engines
US2684571A (en) Jet motor
US2225796A (en) Fuel injector for diesel motors
US3146769A (en) Fuel injection system
US2474419A (en) Fuel injection apparatus
US2676061A (en) Fuel injector for internalcombustion engines
US2929371A (en) Fuel injector for an internal combustion engine
US1705665A (en) Fuel-injection system
US1967970A (en) System for supplying fuel to internal combustion engines