US3412718A - Precision fuel metering system - Google Patents

Precision fuel metering system Download PDF

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US3412718A
US3412718A US650563A US65056367A US3412718A US 3412718 A US3412718 A US 3412718A US 650563 A US650563 A US 650563A US 65056367 A US65056367 A US 65056367A US 3412718 A US3412718 A US 3412718A
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fuel
fuel metering
engine
transducer
flapper valve
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US650563A
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Long Emile David
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Gillett Tool Co Inc
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Gillett Tool Co Inc
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Priority to US650563A priority Critical patent/US3412718A/en
Priority claimed from GB40984/68A external-priority patent/GB1236062A/en
Priority to GB40984/68A priority patent/GB1236062A/en
Priority to DE19681776012 priority patent/DE1776012B2/de
Priority to FR166361 priority
Publication of US3412718A publication Critical patent/US3412718A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/3809Common rail control 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/005Arrangement of electrical wires and connections, e.g. wire harness, sockets, plugs; Arrangement of electronic control circuits in or on fuel injection apparatus
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0635Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding
    • F02M51/0639Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding the armature acting as a valve
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/08Injectors peculiar thereto with means directly operating the valve needle specially for low-pressure fuel-injection
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/14Arrangements of injectors with respect to engines; Mounting of injectors
    • F02M61/145Arrangements of injectors with respect to engines; Mounting of injectors the injection nozzle opening into the air intake conduit
    • 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
    • F02M69/04Injectors peculiar thereto
    • F02M69/042Positioning of injectors with respect to engine, e.g. in the air intake conduit
    • F02M69/044Positioning of injectors with respect to engine, e.g. in the air intake conduit for injecting into the intake conduit downstream of an air throttle valve
    • 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
    • F02M69/462Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down
    • F02M69/465Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down of fuel rails

Description

Nov. 26, 1968 E. D. LONG 3,412,718
PRECISION FUEL METERING SYSTEM FUEL PUMP W/ACCUMULATOR ACCUMULATOR ENGINE HEAD"\ -ts ELECTRONIC FROMfiTO E MODULATOR SUPPLY I ELEC. TRIGGER POWER UNIT CAMSHAFT INVENTOR E. DAVID LONG BY (97.5 ab
ATTORNEY Nov. 26, 1968 E. D. LONG 3,412,718
PRECISION FUEL METERING SYSTEM Filed June 15, 1967 2 Sheets-Sheet 2 1 INVENTOR E. DAVID LONG ATTORNEY United States Patent 3,412,718 PRECISION FUEL METERING SYSTEM Emile David Long, Elmira, N.Y., assignor to Gillett Tool Co., Inc., Buffalo, N.Y. Filed lane 13, 1967, Ser. No. 650,563 8 Claims. (Cl. 123-32) ABSTRACT OF THE DISCLOSURE A plurality of fuel metering transducers are employed for simultaneously delivering measured amounts of fuel to the cylinders of an internal combustion engine, once per engine cycle, and in response to an electronic modulator which senses various engine operational and environmental parameters, such as, engine manifold air temperature and vacuum, engine temperature, engine speed, throttle position and barometric pressure. Each of the fuel metering transducers is mounted entirely within the engine air manifold and adjustably positioned adjacent the respective inlet valve for each cylinder, the fuel fed to each transducer being at constant pressure, whereby the measured amount of fuel being admitted to each cylinder depends upon the length of time the transducer is held in open position.
Background of the invention Heretofore it has been the customary practice to supply the proper fuel-air mixture to the cylinders of spark ignition internal combustion engines through carburetion wherein the liquid fuel is vaporized and mixed with air in the correct proportion. The use of carburetion in these engines has been nearly the universal practice for economy and reliability in general day-to-day performance. While carburetor systems have been satisfactory for their intended purpose, they have been subject to certain disadvantages inherent in their design. For instance, while trying to maintain the proper volume and velocity of air flow to insure an adequate ratio of the fuel-air mixture, the fuel becomes deposited on the wall of the manifold resulting in a reduction of fuel economy. Furthermore, in view of the fact that the heat of the manifold is utilized to facilitate the vaporization of the fuel, hot spots are formed in the manifold which have a tendency to cause backfiring and vapor lock.
In order to overcome the disadvantages experienced with carburetion systems and in an attempt to provide a proper fuel-air mixture for complete combustion in the engine cylinder with a concomitant reduction of exhaust gases, it has been proposed to employ various types of fuel injection systems. However, it has been found that designing a fuel injection system for spark-ignition engines involves much more than merely substituting an injector valve for a carburetor. In both mechanical and electrically controlled injection systems, the proper calibration and control of the fuel-air mixture through the full dynamic range of the engine is most difiicult and sometimes impossible to achieve since the bellows, diaphragms and associated control linkage commonly employed in these systems are frequently subject to binding, hysteresis and frequent malfunction.
While the shortcomings of known fuel injection systems have been recognized, the advantages of fuel injection over carburetion in spark ignition engines have equally been recognized by those skilled in the art. For instance, by eliminating the carburetor, the improved engine volumetric efficiency and colder air charges results in an increase of power output at high engine speeds. Furthermore, the fuel-air mixture more closely approaches a stoichiometric composition to thereby reduce the amount of unburned hydrocarbons and carbon monoxide in the exhaust.
Patented Nov. 26, 1968 Summary After considerable research and experimentation, the fuel metering system of the present invention has been devised to overcome the disadvantages experienced in fuel injection systems and comprises, essentially, a plurality of fuel metering transducers mounted entirely within an air chamber such as an engine air manifold. Each of the transducers is adjustably positioned adjacent the respective inlet valve for each cylinder and includes an orifice of fixed area which is opened and closed by an electromagnetically actuated member of fixed travel. The fuel metering transducers communicate with a fuel rail which supplies fuel at constant pressure to the transducers, whereby the quantity of fuel admitted to the cylinders depends upon the length of time the magnetically actuated members are held in open position, the energization of the electro-magnet for each movable member being controlled by an electronic modulator which senses various engine operational and environmental parameters.
Brief description of the drawings FIGURE 1 is a diagrammatic view of the fuel metering system of the present invention;
FIGURE 2 is a fragmentary sectional view showing the position of a fuel metering transducer relative to the engine cylinder;
FIGURE 3 is a fragmentary sectional view of the connection for adjustably positioning the fuel metering transducer within the engine manifold;
FIGURE 4 is an enlarged longitudinal sectional view of the fuel metering transducer of the present invention;
FIGURE 5 is a view of the transducer taken along line 55 of FIGURE 4;
FIGURE 6 is a view taken along line 66 of FIG- URE 4;
FIGURE 7 is a view taken along line 77 of FIGURE 4; and
FIGURE 8 is a plan view of a modified form of a valve element adapted to be employed in the fuel metering transducer of the present invention.
Description 07 the preferred embodiment Referring to the drawings and more particularly to FIGURE 1, the precision fuel metering system in which the fuel metering transducers of the present invention are adapted to be employed, comprises essentially, a fuel rail 1 for supplying fuel to a plurality of fuel metering transducers 2 adjustably mounted on the engine head by swivel joint connections 3, to be described more fully hereinafter. The fuel supplied to be transducer through the fuel rail is fed thereto at constant pressure by a fuel pump connected to one end of the fuel rail and an accumulator at the opposite end thereof, said accumulator being of the type disclosed in my copending application Ser. No. 645,701, filed June 13, 1967. An electronic modulator of the type described in my copending application Ser. No. 653,484, filed July 14, 1967, is electrically connected to the transducer 2 for actuating the same in response to various engine operational and environmental parameters fed to the modulator by a throttle valve assembly and trigger unit. For example, the engine manifold air temperature and vacuum, barometric pressure and throttle position would be sensed by the throttle valve assembly; and the trigger unit, actuated by the engine cam shaft, would sense the engine speed. When desirable, the trigger unit may be actuated by an electrical signal from the ignition system. The electronic modulator, in turn, feeds the transducers 2 with a square wave pulse, the duration or width of which is a direct function of the integrated valve of the various system sensors.
As will be seen in FIGURE 2, the engine upon which the fuel metering transducer 2 of the present invention is adapted to be mounted is a conventional internal combustion engine including an air intake manifold 4, cylinder 5 and piston 6. Fuel taken into the cylinder through intake port 7, controlled by valve 8, is ignited by spark plug 9.
Referring to FIGURES 4 to 7, the fuel metering transducer 2 of the persent invention comprises a housing connected to the end of a fuel line 11 which is maintained in communication with the fuel rail 1 (FIGURE 1). A solenoid is mounted within the housing and includes an inner pole piece member 12 and an outer pole piece member 13 surrounding and positioned concentrically with respect to the inner pole piece member. A plastic spool 14 having an electrical coil 15 wound thereon is secured to the inner pole piece member, one end of the coil interconnecting the pole piece members as at 16 and the opposite end of the coil being connected to a terminal 17 adhesively secured to the inner pole piece as at 18. A lead 19 is also connected to the terminal 17 and extends upwardly within the fuel line 11 and is connected to a terminal 20 (FIGURE 3) secured to the Wall of the fuel line, the terminal 20, in turn, being electrically connected to the electronic modulator (FIG- URE 1).
A nozzle 21 is rigidly secured within the lower end of housing 10 and sealed therein by an O-ring 22. A longitudinally extending, centrally disposed orifice 23 is formed in the nozzle and communicates with a recess 24 formed by an annular shoulder or land member 25 disposed on the upper surface of the nozzle and positioned concentrically with respect to the orifice. The annular shoulder 25 forms a seat for a flapper valve 26 which is biased to closed position on the seat by a coil spring 27 having one end engaging the upper surface of the flapper valve and the opposite end engaging a shoulder 28 formed on the opposite end portion of the housing. When the flapper valve is biased to closed position on seat 25, there is a clearance of .004" between the end of the outer pole piece member 13 and the upper surface of the flapper valve; thus, when the solenoid is actuated, the flapper valve, functioning as an armature, is drawn upwardly a distance of .004" against the end of the outer pole piece. While in this position, there is a .003" residual air gap between the end of the inner pole piece member 12 and the upper surface of the flapper valve whereby an adequate magnetic force may be generated in the solenoid. In order to provide a hydrostatic relief to thereby allow the flapper valve 26 to move freely between open and closed positions, apertures 13a and 26a are formed in the lower end portion of the outer pole piece member and in the flapper valve, respectively.
In the operation of the fuel metering transducer, fuel, being fed under constant pressure through fuel line 11, flows into the annular chamber defined by the outer peripheral wall of the outer pole piece member 13 and the inner peripheral wall of the housing 10. When a signal is received from the electronic modulator for actuating the solenoid, the flapper valve 26 is pulled upwardly from seat 25 thereby compressing spring 27 and allowing the fuel to flow into recess 24 and through orifice 23 into the engine cylinder. When the solenoid is de-energized, the spring 27 expands forcing the flapper valve downwardly onto the seat 25.
Since the fuel metering transducers are to be actuated once per engine cycle, the relatively small mass of the magnetically actuated flapper valve 26, moving through the fixed distance of .004" to open and close the orifice 23 of fixed area, readily adapts the flapper valve for operating speeds in the order of 1000 cycles per second, and since the fuel is being fed to the transducer at constant pressure, the quantity of {fuel admitted into the engine cylinder depends upon the length of time the flapper valve is held in open position.
While the flapper valve shown in FIGURES 4 and 6 consists of a disc having axially extending hydrostatic relief apertures formed in the body of the disc, another embodiment of the flapper valve is illustrated in FIG- URE 8 wherein the disc 29 is formed with a plurality of circumferentially spaced hydorstatic relief notches 29a formed in the periphery thereof.
While the admission of the proper quantity of fuel to the engine cylinder in response to the engine speed and the absolute weight of the air charge is an important feature of the present invention, another equally important feature of the invention is the location of the fuel metering transducer within the engine manifold to provide port injection of the fuel to thereby prevent deposition of the fuel on the walls of the manifold while at the same time allowing proper vaporization of the fuel. In order to properly position each fuel transducer within the manifold, the swivel joint connection 3, as illustrated in FIGURE 3, is provided, comprising a socket 30 mounted within the wall 4a of the engine air intake manifold; the socket being provided with a tapered bore 30a forming a divergent throat portion on one end thereof. The opposite end of the socket has a threaded portion 30b for receiving a socket nut 31. The socket nut is also provided with a tapered bore 31a, similar to bore 30a formed in the socket, but diverging in an opposite direction therefrom; the construction and arrangement of the divergent bores facilitating the later-a1 adjustment of the fuel line, to be described more fully hereinafter. Seat portions 30c and 3112 are formed on the socket and nut, respectively, for accommodating a spherical member 32 through which the fuel line 11 is slidably mounted.
When mounting the fuel metering transducers on an engine, a plurality of apertures are formed in the wall 4a of the manifold; and a fuel line 11, having a fuel metering transducer 2 secured to the end thereof, is inserted through each of the apertures, after which the socket 30 is slipped on the fuel line and swaged into the aperture. The spherical member 32 and socket nut 31 are similarly slipped on the fuel line and assume the position shown in FIGURE 3; however, before the nut 31 is tightened, the fuel metering transducer is properly positioned relative to its respective injection port by manually pushing the fuel line through the sphere 32 until the fuel metering transducer 2 touches the stem of valve 8. The fuel line and associated transducer is then backed off slightly from the valve stem and adjusted laterally as shown in dotted lines in FIGURE 3. When the proper position of the transducer has been obtained, the nut 31 is tightened to thereby bind the sphere 32 on the seats 30c and 31b. The spherical member 32 is formed from a suitable plastic, such as Teflon, which is characterized by its relatively low coeflicient of friction and sealant properties. Accordingly, by forming the spherical member 32 from Teflon, the lateral and longitudinal adjustment of the fuel line and associated fuel metering transducer is not only enhanced but also when the nut 31 is tightened, the Teflon sphere provides an excellent seal within the swivel joint connection.
The construction and arrangement of the fuel line 11, fuel metering transducer 2 and swivel joint connection 3 readily adapts the assembly for mounting on various types of conventional engines. While it has been found that the swivel joint connection, as described hereinabove, will generally accommodate adjustment of the fuel metering transducer, in some instances, it may be necessary to bend the end of the fuel line as shown in FIGURE 3.
From the above description, it will be appreciated by those skilled in the art that the precision fuel metering system of the present invention provides a system having good cold starting and warm-up characteristics, good part throttle economy and good wide open throttle power; and since very few moving parts are employed, the system is not likely to get out of order even after long and continued use.
I claim:
1. In a fuel metering system for an internal combus tion engine wherein an electronic modulator is employed for actuating a fuel metering transducer in response to various engine operational and environmental parameters, the improvement comprising, fuel metering transducer means adjustably positioned within the injection port of the engine cylinder, and swivel joint means mounted on the wall of the engine air manifold and connected to said fuel metering transducer means; said swivel joint means comprising, a socket mounted within the wall of the engine air intake manifold, a tapered bore formed in one end of said socket forming a divergent throat portion, a nut threadably mounted in the opposite end of said socket, a tapered bore formed in said nut forming a divergent throat portion extending in a direction opposite to the throat portion formed in the socket, seat portions formed on the interior wall of said socket and on the end portion of the nut extending within the socket, and a spherical member mounted between said seat portions, said fuel transducer means including a fuel line slidably mounted within said spherical member and extending through said divergent throat portions, whereby the position of the fuel metering transducer means may be adjusted relative to the injection port of the engine cylinder by manually sliding the fuel line through the spherical member and swivelling the fuel line and associated spherical member to a predetermined position, said transducer means being held at the predetermined position by tightening said nut to thereby bind the spherical members on said seat portions.
2. In a fuel metering system according to claim 1, wherein the fuel metering transducer means comprises, a housing, a fuel line connected to one end of said housing, solenoid means mounted within said housing, a nozzle rigidly connected to the opposite end of the housing and spaced from said solenoid means, said nozzle including a longitudinally extending orifice formed therein, an annular land disposed on the inlet end of the nozzle and positioned concentrically with respect to the orifice, a flapper valve positioned within said housing between the solenoid and said land, and a coil spring surrounding said solenoid means and extending between the end of the housing and the flapper valve for biasing the flapper valve against said land to close said nozzle orifice, said flapper valve being spaced from said solenoid means when biased to closed position, whereby when the solenoid is energized the flapper valve is drawn against said solenoid means to open said nozzle orifice.
3. In a fuel metering system according to claim 2, wherein the flapper valve comprises a disc having hydrostatic relief apertures formed therein whereby the flapper valve may move freely between open and closed positions.
4. In a fuel metering system according to claim 2, wherein the flapper valve comprises a disc having a plurality of circumferentially spaced hydrostatic relief notches formed in the periphery thereof, whereby the flapper valve may move freely between open and closed positions.
5. A fuel metering transducer comprising, a housing, a fuel line connected to one end of said housing, means operatively connected to the fuel line for supplying fuel at constant pressure to said housing, solenoid means having a core mounted within said housing, a nozzle rigidly connected to the opposite end of the housing and spaced from said solenoid means, said nozzle including a centrally disposed, longitudinally extending orifice formed therein, an annular land disposed on the inlet end of the nozzle and positioned concentrically with respect to the orifice, a flapper valve positioned within said housing between the solenoid and said land, and a coil spring surrounding said solenoid means and extending between the end of the housing and the flapper valve for biasing the flapper valve against said land to close said nozzle orifice, said flapper valve being spaced from the core of said solenoid means when open and when biased to closed position, whereby when the solenoid is energized the flapper valve is drawn a fixed distance against said solenoid means to open the nozzle orifice of fixed area, thereby allowing the fuel to flow through said nozzle orifice, the quantity of fuel discharged through the nozzle orifice depending upon the length of time the flapper valve is held in open position.
6. A fuel metering transducer according to claim 5, wherein the flapper valve comprises a disc having hydrostatic relief apertures formed therein whereby the flapper valve may move freely between open and closed positions.
7. A fuel metering transducer according to claim 5, wherein the flapper valve comprises a disc having a plurality of circumferentially spaced hydrostatic relief notches formed in the periphery thereof, whereby the flapper valve may move freely between open and closed positions.
8. A fuel metering transducer according to claim 5 wherein said flapper valve is spaced from the solenoid means a distance of the order of .004 when in closed position.
References Cited UNITED STATES PATENTS 1,025,884 5/1912 Schmitt 285- 2,706,976 4/1955 Gianini 123139.17 2,856,910 10/1958 Goodridge.
2,859,741 11/1958 Gl nn 123139.17 3,032,025 5/1962 Long.
FOREIGN PATENTS 858,966 1/1961 Great Britain.
LAURENCE M. GOODRIDGE, Primary Examiner.
US650563A 1967-06-13 1967-06-13 Precision fuel metering system Expired - Lifetime US3412718A (en)

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Application Number Priority Date Filing Date Title
US650563A US3412718A (en) 1967-06-13 1967-06-13 Precision fuel metering system
GB40984/68A GB1236062A (en) 1967-06-13 1968-08-27 Electronically controlled fuel injection system for internal combustion engines
DE19681776012 DE1776012B2 (en) 1967-06-13 1968-09-03
FR166361 1968-09-16

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Application Number Priority Date Filing Date Title
US650563A US3412718A (en) 1967-06-13 1967-06-13 Precision fuel metering system
GB40984/68A GB1236062A (en) 1967-06-13 1968-08-27 Electronically controlled fuel injection system for internal combustion engines
DE19681776012 DE1776012B2 (en) 1967-06-13 1968-09-03
FR166361A FR1593020A (en) 1967-06-13 1968-09-16

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Cited By (18)

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US3776209A (en) * 1973-04-05 1973-12-04 Bendix Corp Fuel injector manifold and mounting arrangement
US3941109A (en) * 1972-08-31 1976-03-02 Dr. -Ing. H.C.F. Porsche Aktiengesellschaft Arrangement for mounting a fuel injection nozzle
US4205637A (en) * 1976-12-13 1980-06-03 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic fuel injection system for an internal combustion engine having electromagnetic valves and a fuel damper upstream thereof
FR2452005A1 (en) * 1979-03-19 1980-10-17 Bendix Corp INJECTOR SUPPLY APPARATUS
EP0026060A1 (en) * 1979-09-20 1981-04-01 LUCAS INDUSTRIES public limited company Fuel injector
US4295452A (en) * 1978-07-01 1981-10-20 Robert Bosch Gmbh Fuel injection system
US4372272A (en) * 1981-07-31 1983-02-08 The Bendix Corporation Fuel delivery system with feed and drain line damping
US4440134A (en) * 1981-05-15 1984-04-03 Kabushiki Kaisha Komatsu Seisakusho Fuel injection system for internal combustion engines
US4570601A (en) * 1983-11-15 1986-02-18 Nippondenso Co., Ltd. Fuel delivery pipe
US4809665A (en) * 1986-12-22 1989-03-07 Webasto Ag Fahrzeugtechnik Fuel supply system for an auxiliary motor vehicle heating device
US4895124A (en) * 1987-12-02 1990-01-23 Proprietary Technology, Inc. Fuel and electrical distribution system for fuel injected engines
US4909221A (en) * 1987-11-19 1990-03-20 General Motors Corporation Internal combustion engine fuel injection system
US5360079A (en) * 1989-10-02 1994-11-01 Yamaha Hatsudoki Kabushiki Kaisha Fuel injected automotive engine
US5522369A (en) * 1995-06-26 1996-06-04 Ford Motor Company System and method for controlling delivery of gaseous fuel to an internal combustion engine
US6263863B1 (en) * 1998-07-01 2001-07-24 MAGNETI MARELLI S.p.A. Coupling system between engine head, injector and fuel manifold
EP1255038A2 (en) * 1997-06-25 2002-11-06 Robert Bosch Gmbh Fuel injection system
US20060027214A1 (en) * 2004-08-03 2006-02-09 Usui Kokusai Sangyo Kaisha, Ltd. Fuel delivery pipe
US20090196687A1 (en) * 2008-01-07 2009-08-06 Daniel Marc Coupling arrangement and connection assembly

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GB1567041A (en) * 1975-11-06 1980-05-08 Allied Chem Fuel injection system
DE2614703C3 (en) * 1976-04-06 1981-04-23 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart, De
DE3714693A1 (en) * 1987-05-02 1988-11-10 Bosch Gmbh Robert ELECTROMAGNETICALLY ACTUABLE VALVE
DE4003337C1 (en) * 1990-02-05 1991-05-23 Straetling, Geb. Toelle, Hedwig, 4630 Bochum, De Rotary piston IC engine - has injection nozzles pivoting in housing wall inlets and directed toward piston surface
DE10115325A1 (en) 2001-03-28 2002-10-17 Bosch Gmbh Robert Fuel injector, for an IC motor, has a clamp system to hold the injector housing at the base body, with a convex curvature in a ball segment shape at the clamping surface for an increased sealing action

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US2856910A (en) * 1956-04-23 1958-10-21 Acf Ind Inc Fuel injection system
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GB858966A (en) * 1957-05-10 1961-01-18 Bendix Corp Fuel injection nozzle for internal combustion engines
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US1025884A (en) * 1911-07-19 1912-05-07 John O Schmitt Combined stuffing-box and shaft-bearing.
US2706976A (en) * 1951-03-07 1955-04-26 Moto Guzzi Societa Per Azioni Carburator and carburation system for internal combustion engines
US2856910A (en) * 1956-04-23 1958-10-21 Acf Ind Inc Fuel injection system
US2859741A (en) * 1956-09-20 1958-11-11 Edward R Glenn Fuel injecting apparatus
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Cited By (23)

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Publication number Priority date Publication date Assignee Title
US3941109A (en) * 1972-08-31 1976-03-02 Dr. -Ing. H.C.F. Porsche Aktiengesellschaft Arrangement for mounting a fuel injection nozzle
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Also Published As

Publication number Publication date
DE1776012B2 (en) 1971-07-22
DE1776012A1 (en) 1970-10-01
FR1593020A (en) 1970-05-25

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