[go: up one dir, main page]

US3175771A - Fuel injectors for internal combustion engines - Google Patents

Fuel injectors for internal combustion engines Download PDF

Info

Publication number
US3175771A
US3175771A US231726A US23172662A US3175771A US 3175771 A US3175771 A US 3175771A US 231726 A US231726 A US 231726A US 23172662 A US23172662 A US 23172662A US 3175771 A US3175771 A US 3175771A
Authority
US
United States
Prior art keywords
fuel
valve
injector
needle
internal combustion
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
US231726A
Inventor
Breting Olivier
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
Application granted granted Critical
Publication of US3175771A publication Critical patent/US3175771A/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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/20Closing valves mechanically, e.g. arrangements of springs or weights or permanent magnets; Damping of valve lift
    • 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
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/06Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series the valves being furnished at seated ends with pintle or plug shaped extensions
    • 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
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • 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
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for

Definitions

  • This invention relates to a closed, automatic fuel injector wherein the valve member opens in the direction opposite to the fuel output, thus acting as a simple needlevalve device.
  • the fuel injector according to the present invention is of the valve needle type wherein the valve face, by coacting with the registering valve seat formed on the nozzle, will on the one hand atomize the fuel when the needle valve is lifted and on the other hand provide the necessary fluid-tightness when the needle valve is seated.
  • This spring meets two requirements: on one hand its thrust is applied directly on the needle-valve in order to reduce the weight of moving parts during the needle valve movements, and on the other hand its stiffness is such that the increase in the needle valve surface areas subjected to the injection pressure during the valve lift produces additional efiorts incrementing the spring deflection by a height equal to the optimum lift of said needle valve.
  • This lift is of the order of 0.004" for a 60-degree needle valve.
  • the spring action which as already stated is coincident with the needle valve action and exerted in the direction of the valve axis, eliminates any side thrust in the needle valve movements and therefore conventional sources of wear and tear which are a frequent cause of valve jamming.
  • FIGURE 1 illustrates by way of example a typical embodiment of a fuel injector according to this invention
  • FIGURE 2 illustrates a second embodiment thereof.
  • This device comprises a needle valve 1 similar to those of conventional needle-valve fuel injectors.
  • the injection nozzle 2 may be consistent with standard requirements concerning the manufacture of these parts.
  • the needle-valve face is such that its end portion 3, on the downstream side of the needle valve, acts jointly as an atomizing nozzle when the fuel under pressure accumulating in chamber 5 has exerted an upward pressure on the thrust cone 6 suflicient to lift the valve.
  • the nozzle is formed downstream of the outer-most meridian 3 of this face with an outfiaring surface 4, according to a known arrangement now in general use in the manufacture of injection equipment.
  • the angle of this outflaring surface 4 is greater than that of the injection jet in order to avoid any interference with this jet; however, an angle inferior to degrees is preferred.
  • a cavity may be substituted for this outflaring or tapered surface, and in this case the cavity may have an optimum contour as determined by systematic tests. In fact, it is stated in certain conventional works dealing with fuel injection that under strictly determined conditions this cavity may play a substantial part in the atomization and improve the quality thereof.
  • the needle valve portion projecting from the atomizing nozzle constitutes a useless cone which may be very sensitive to the high temperatures attained in the combustion chamber. Therefore, this end portion may be truncated to increase the heat resistance.
  • the light, strong spring exerting a constant force on the needle valve stem consists of a plurality of stacked dished washers, according to the rules well known in the technical field.
  • the upper portion 8 of this washer stacking is prestressed by an adjustable stop member 9 solid with the fixed part on which the injector is mounted, generally the so-called injector carrier (not shown).
  • the pressure wave from the fuel pump (not shown) or another source reaches the chamber 5 through a passageway 10.
  • the pressure in chamber 5 has risen to a value such that the action exerted on the thrust cone 6 exceeds the force of spring 7, the needle valve is lifted.
  • the wet surface area increases very rapidly, thus reducing the time period during which the atomization is rather poor, a fact well known to those conversant with the art, since the optimum requirements for a goodquality atomization are not met.
  • the optimum valve lift corresponding to the tapered atomizing nozzle, is very low, of the order of 0.004". A valve lift of this value is thus rapidly attained and permits at the same time a direct atomization.
  • the tapered nozzle of this injector is improved by a slight centrifugal action.
  • the latter may be created by inclining conduit 10 with respect to the vertical axis of the injector and also with respect to a plane through said vertical axis and the point of intersection of said conduit 'with the chamber of said injector.
  • This embodiment is shown at FIGURE 2, wherein the inclined or oblique conduit is referenced as 10', and the end 3 of the needle valve is truncated.
  • the needle valve may be provided with various perforations 11 and/ or circular grooves 12 to constitute a kind of labyrinth and reduce injector leakages.
  • Any other suitable spring means capable of applying a centered and relatively strong force with a moderate deflection may be substituted for the dished washers illustrated.
  • An automatic fuel injector for thermal motors of the close type comprising, a single axial needle valve having a conical tapered end portion and a thrust cone portion 3 and being adapted to open in a direction opposite the flow of fuel, a nozzle having a central channel which houses said needle, said nozzle having at its lower part a fuelreceiving chamber into which there opens an oblique conduit communicating with the injector members for placing the fuel under pressure, said conduit being oblique with respect to the vertical axis of said injector and also with respect to a plane through said vertical axis and the point of intersection of said conduit with the chamber of said injector, and said nozzle having a seat below said chamber which cooperates with the conical end of said needle, as
  • said needle being supported by a stack of washer springs acting directly at the top and the said fuel-feed conduit opening into the said chamber obliquely at the periphery of the latter so as to impart a centrifugalmovement to the liquid projected out of the chamber, and said thrust cone portion being in the form of a conical tapered surface which defines a shoulder on which the accumulated fuel in said chamber exerts a pressure, thereby lifting said valve.

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

0. BRETING March 30, 1965 FUEL INJECTORS FOR INTERNAL COMBUSTION ENGINES Filed Oct. 19, 1962 2 Sheets-Sheet 1 2 Sheets-Sheet 2 ,lillll I'll-ll INVENTOR ORNEYS O. BRETING March 30, 1965 FUEL INJECTORS FOR INTERNAL COMBUSTION ENGINES Filed 00L 19, 1962 nited States Patent 3,175,771 Patented Mar. 30, 1965 fiice 3,175,771 FUEL INJECTORS FGR INTERNAL COMBUSTION ENGINES Olivier Brting, 5 Ave. Valiond, Sainte-Foy-les-Lyon, France Filed Oct. 19, 1962, Ser. No. 231,726 Claims priority, application France, Nov. 4, 1961, 42,961, Patent 1,312,045 1 Claim. (Cl. 239-533) It is known that there is a constant search for improving the grade of fuel atomization of a fuel injector of thermal engines, notably diesel engines. In fact, in compression-ignition engines the ignition time period to which the quantity of fuel burned according to the detonating process is subordinated depends very closely on the fuel injection atomization fineness. As this quantity of detonating fuel involves simultaneously the characteristic and unpleasant noise of diesel engines together with a strong reduction in the engine efiiciency, it appears that the quality of the initial portion of the combustion is of particular importance.
Now it was amply proved that this atomization quality could not be attained with conventional injection methods and means. In fact, in most instances the first drops of injected fuel must clear many constricted or throttled passages successively so that their potential pressure is reduced and the final atomization occurring under a relatively low pressure is particularly poor.
This invention relates to a closed, automatic fuel injector wherein the valve member opens in the direction opposite to the fuel output, thus acting as a simple needlevalve device.
Tests have been made with a view to achieve in a needle valve injector the atomization and the necessary fluidtightness by means of the same co-operating surfaces of the needle-valve and injection nozzle. This mounting requiring a moderate valve lift for maximum efiiciency led to particularly strict requirements regarding the valve spring; on the other hand, the composite mounting of the device made it particularly costly and impaired therefore its marketability.
The fuel injector according to the present invention is of the valve needle type wherein the valve face, by coacting with the registering valve seat formed on the nozzle, will on the one hand atomize the fuel when the needle valve is lifted and on the other hand provide the necessary fluid-tightness when the needle valve is seated.
This last principle is already known per se and is set forth in detail in various works dealing with fuel injection. However, what characterizes the fuel injector according to this invention is on one hand the fact that the injector nozzle consists of a single member and on the other hand that the needle valve is seated under the influence of a lightweight yet powerful spring of which the action is coincident with the needle-valve action.
This spring meets two requirements: on one hand its thrust is applied directly on the needle-valve in order to reduce the weight of moving parts during the needle valve movements, and on the other hand its stiffness is such that the increase in the needle valve surface areas subjected to the injection pressure during the valve lift produces additional efiorts incrementing the spring deflection by a height equal to the optimum lift of said needle valve. This lift is of the order of 0.004" for a 60-degree needle valve.
It may be noted that the spring action, which as already stated is coincident with the needle valve action and exerted in the direction of the valve axis, eliminates any side thrust in the needle valve movements and therefore conventional sources of wear and tear which are a frequent cause of valve jamming.
Reference will now be made to the accompanying drawings of which FIGURE 1 illustrates by way of example a typical embodiment of a fuel injector according to this invention, and FIGURE 2 illustrates a second embodiment thereof.
This device comprises a needle valve 1 similar to those of conventional needle-valve fuel injectors. The injection nozzle 2 may be consistent with standard requirements concerning the manufacture of these parts.
One specific feature of the fuel injector according to this invention is that the needle-valve face is such that its end portion 3, on the downstream side of the needle valve, acts jointly as an atomizing nozzle when the fuel under pressure accumulating in chamber 5 has exerted an upward pressure on the thrust cone 6 suflicient to lift the valve.
In order to warrant a sufiicient strength to the nozzle at the level of this valve face, the nozzle is formed downstream of the outer-most meridian 3 of this face with an outfiaring surface 4, according to a known arrangement now in general use in the manufacture of injection equipment. The angle of this outflaring surface 4 is greater than that of the injection jet in order to avoid any interference with this jet; however, an angle inferior to degrees is preferred.
If desired, a cavity may be substituted for this outflaring or tapered surface, and in this case the cavity may have an optimum contour as determined by systematic tests. In fact, it is stated in certain conventional works dealing with fuel injection that under strictly determined conditions this cavity may play a substantial part in the atomization and improve the quality thereof.
The needle valve portion projecting from the atomizing nozzle constitutes a useless cone which may be very sensitive to the high temperatures attained in the combustion chamber. Therefore, this end portion may be truncated to increase the heat resistance.
According to a preferred embodiment of the injection device constituting the subject-matter of this invention,
,the light, strong spring exerting a constant force on the needle valve stem consists of a plurality of stacked dished washers, according to the rules well known in the technical field.
The upper portion 8 of this washer stacking is prestressed by an adjustable stop member 9 solid with the fixed part on which the injector is mounted, generally the so-called injector carrier (not shown).
The use of dished washers reduces to a minimum the weight of the movable component elements of the injector, thus improving the operation of the device of this invention, which takes place as follows:
The pressure wave from the fuel pump (not shown) or another source reaches the chamber 5 through a passageway 10. When the pressure in chamber 5 has risen to a value such that the action exerted on the thrust cone 6 exceeds the force of spring 7, the needle valve is lifted. At this time the wet surface area increases very rapidly, thus reducing the time period during which the atomization is rather poor, a fact well known to those conversant with the art, since the optimum requirements for a goodquality atomization are not met. Moreover, it is known that the optimum valve lift, corresponding to the tapered atomizing nozzle, is very low, of the order of 0.004". A valve lift of this value is thus rapidly attained and permits at the same time a direct atomization. Under these conditions it will be seen that as the pressure reaching the inject-or is absorbed completely for fuel atomizing purposes only the injector according to this invention will effect quickly a high-grade atomization, under optimum and high pressure conditions. This is the scope contemplated, which permits of reducing consider-ably the ignition time period constituting a very important element in the operation of diesel or compression-ignition engines. Actually, the noiselessness and economy of operation of diesel engines are to a large extent subordinate to this re- =duction in ignition time.
Conventionally, the tapered nozzle of this injector is improved by a slight centrifugal action. The latter may be created by inclining conduit 10 with respect to the vertical axis of the injector and also with respect to a plane through said vertical axis and the point of intersection of said conduit 'with the chamber of said injector. This embodiment is shown at FIGURE 2, wherein the inclined or oblique conduit is referenced as 10', and the end 3 of the needle valve is truncated.
On the other hand, in order to reduce the weight of the movable component elements of the injector the needle valve may be provided with various perforations 11 and/ or circular grooves 12 to constitute a kind of labyrinth and reduce injector leakages.
Any other suitable spring means capable of applying a centered and relatively strong force with a moderate deflection may be substituted for the dished washers illustrated.
Of course, the principles of this injection device are also applicable to different types of injectors, such as long injectors, non-conventional injectors, etc. without departing from the spirit and scope of the invention. Besides, many modifications may be brought to the specific form of embodiment illustrated, described-and suggested herein without departing from the basic principles of the invention as set forth in the appended claim.
I claim:
An automatic fuel injector for thermal motors of the close type comprising, a single axial needle valve having a conical tapered end portion and a thrust cone portion 3 and being adapted to open in a direction opposite the flow of fuel, a nozzle having a central channel which houses said needle, said nozzle having at its lower part a fuelreceiving chamber into which there opens an oblique conduit communicating with the injector members for placing the fuel under pressure, said conduit being oblique with respect to the vertical axis of said injector and also with respect to a plane through said vertical axis and the point of intersection of said conduit with the chamber of said injector, and said nozzle having a seat below said chamber which cooperates with the conical end of said needle, as
well as a frusto-conical shaped extension of the opening of said seat with an angle greater than that of the jet of fuel, said needle being supported by a stack of washer springs acting directly at the top and the said fuel-feed conduit opening into the said chamber obliquely at the periphery of the latter so as to impart a centrifugalmovement to the liquid projected out of the chamber, and said thrust cone portion being in the form of a conical tapered surface which defines a shoulder on which the accumulated fuel in said chamber exerts a pressure, thereby lifting said valve.
References Cited by the Examiner UNITED STATES PATENTS 1,157,305 10/15 Frost. 2,192,803 3/40 Purdy et al 239453 2,263,197 11/41 Tabb et a1. 239-453 2,382,151 8/45 Harper.
FOREIGN PATENTS 97,829 9/24 Austria. 91,209 4/97 Germany. 474,978 4/29 Germany.
20,758 9/11 Great Britain.
EVERETT W. KIRBY, Primary Examiner.
US231726A 1961-11-04 1962-10-19 Fuel injectors for internal combustion engines Expired - Lifetime US3175771A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR42002A FR1312045A (en) 1961-11-04 1961-11-04 Improvement in fuel injectors for heat engines

Publications (1)

Publication Number Publication Date
US3175771A true US3175771A (en) 1965-03-30

Family

ID=9694298

Family Applications (1)

Application Number Title Priority Date Filing Date
US231726A Expired - Lifetime US3175771A (en) 1961-11-04 1962-10-19 Fuel injectors for internal combustion engines

Country Status (5)

Country Link
US (1) US3175771A (en)
DE (1) DE1426141A1 (en)
FR (1) FR1312045A (en)
GB (1) GB1015429A (en)
LU (1) LU42528A1 (en)

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3465969A (en) * 1966-01-07 1969-09-09 Cav Ltd Liquid fuel injection nozzles
US3684176A (en) * 1970-07-27 1972-08-15 Rain Jet Corp Pulsation impact spray nozzle
US4248296A (en) * 1979-08-07 1981-02-03 Resources Conservation Company Fluid distributor for condenser tubes
US4763841A (en) * 1986-04-29 1988-08-16 Daimler-Benz Aktiengesellschaft Injection nozzle for injecting fuel into the combustion chamber of an air-compressing fuel-injection engine
US5421521A (en) * 1993-12-23 1995-06-06 Caterpillar Inc. Fuel injection nozzle having a force-balanced check
US5449119A (en) * 1994-05-25 1995-09-12 Caterpillar Inc. Magnetically adjustable valve adapted for a fuel injector
US5479901A (en) * 1994-06-27 1996-01-02 Caterpillar Inc. Electro-hydraulic spool control valve assembly adapted for a fuel injector
US5488340A (en) * 1994-05-20 1996-01-30 Caterpillar Inc. Hard magnetic valve actuator adapted for a fuel injector
US5494220A (en) * 1994-08-08 1996-02-27 Caterpillar Inc. Fuel injector assembly with pressure-equalized valve seat
US5520338A (en) * 1994-09-21 1996-05-28 Caterpillar Inc. Fuel injector needle check valve biasing spring
US5597118A (en) * 1995-05-26 1997-01-28 Caterpillar Inc. Direct-operated spool valve for a fuel injector
US5605289A (en) * 1994-12-02 1997-02-25 Caterpillar Inc. Fuel injector with spring-biased control valve
US5628293A (en) * 1994-05-13 1997-05-13 Caterpillar Inc. Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
US5673669A (en) * 1994-07-29 1997-10-07 Caterpillar Inc. Hydraulically-actuated fluid injector having pre-injection pressurizable fluid storage chamber and direct-operated check
US5685490A (en) * 1995-07-27 1997-11-11 Caterpillar Inc. Fuel injector with pressure bleed-off stop
US5687693A (en) * 1994-07-29 1997-11-18 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5697342A (en) * 1994-07-29 1997-12-16 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5720318A (en) * 1995-05-26 1998-02-24 Caterpillar Inc. Solenoid actuated miniservo spool valve
US5826562A (en) * 1994-07-29 1998-10-27 Caterpillar Inc. Piston and barrell assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US6082332A (en) * 1994-07-29 2000-07-04 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US6085991A (en) * 1998-05-14 2000-07-11 Sturman; Oded E. Intensified fuel injector having a lateral drain passage
US6148778A (en) * 1995-05-17 2000-11-21 Sturman Industries, Inc. Air-fuel module adapted for an internal combustion engine
US6161770A (en) * 1994-06-06 2000-12-19 Sturman; Oded E. Hydraulically driven springless fuel injector
US6257499B1 (en) 1994-06-06 2001-07-10 Oded E. Sturman High speed fuel injector
US6425375B1 (en) 1998-12-11 2002-07-30 Caterpillar Inc. Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US6575137B2 (en) 1994-07-29 2003-06-10 Caterpillar Inc Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US20150114353A1 (en) * 2012-06-05 2015-04-30 Caterpillar Motoren Gmbh & Co. Kg Injection nozzle
US20150211460A1 (en) * 2014-01-30 2015-07-30 Denso Corporation Fuel injection nozzle
CN108348931A (en) * 2015-04-30 2018-07-31 叶青有限公司 Spray nozzle device

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1181954B (en) * 1984-03-28 1987-09-30 Daimler Benz Ag INJECTOR NOZZLE FOR INTERNAL COMBUSTION ENGINES WITH AIR COMPRESSION INFECTION
DE3426950A1 (en) * 1984-07-21 1986-01-30 Daimler-Benz Ag, 7000 Stuttgart THROTTLE PIN NOZZLE FOR FUEL INJECTION IN AN AIR-COMPRESSING INTERNAL COMBUSTION ENGINE, IN PARTICULAR CHAMBER ENGINE
DE3502642A1 (en) * 1985-01-26 1986-07-31 Daimler-Benz Ag, 7000 Stuttgart FUEL INJECTION VALVE FOR AN AIR-COMPRESSING INJECTION COMBUSTION ENGINE
IT1183889B (en) * 1985-06-11 1987-10-22 Weber Spa VALVE FOR THE DOSING OF THE FUEL FOR A SUPPLY DEVICE OF AN INTERNAL COMBUSTION ENGINE
EP2003331A1 (en) * 2007-06-12 2008-12-17 Siemens Aktiengesellschaft Valve assembly for an injection valve and injection valve
ES2340962T3 (en) * 2007-11-28 2010-06-11 MAGNETI MARELLI S.p.A. FUEL INJECTOR WITH MECHANICAL SHOCK ABSORBER.

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE91209C (en) *
GB191120758A (en) * 1911-09-20 1912-09-29 Kenneth Crossley Improvement in Oil Sprayers for Internal Combustion Engines.
US1157305A (en) * 1912-10-11 1915-10-19 Gen Electric Pulverizer for oil-engines.
AT97829B (en) * 1923-09-15 1924-09-10 Georg Roediger Valve, in particular for fuel injection in internal combustion engines.
DE474978C (en) * 1922-05-10 1929-04-18 Acro Akt Ges Liquid-controlled injection valve
US2192803A (en) * 1937-07-21 1940-03-05 Eisemann Magneto Corp Fuel injection nozzle for internal combustion engines
US2263197A (en) * 1939-03-08 1941-11-18 Eisemann Magneto Corp Fuel injection nozzle
US2382151A (en) * 1940-12-11 1945-08-14 Jr William Harper Fuel injector

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE91209C (en) *
GB191120758A (en) * 1911-09-20 1912-09-29 Kenneth Crossley Improvement in Oil Sprayers for Internal Combustion Engines.
US1157305A (en) * 1912-10-11 1915-10-19 Gen Electric Pulverizer for oil-engines.
DE474978C (en) * 1922-05-10 1929-04-18 Acro Akt Ges Liquid-controlled injection valve
AT97829B (en) * 1923-09-15 1924-09-10 Georg Roediger Valve, in particular for fuel injection in internal combustion engines.
US2192803A (en) * 1937-07-21 1940-03-05 Eisemann Magneto Corp Fuel injection nozzle for internal combustion engines
US2263197A (en) * 1939-03-08 1941-11-18 Eisemann Magneto Corp Fuel injection nozzle
US2382151A (en) * 1940-12-11 1945-08-14 Jr William Harper Fuel injector

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3465969A (en) * 1966-01-07 1969-09-09 Cav Ltd Liquid fuel injection nozzles
US3684176A (en) * 1970-07-27 1972-08-15 Rain Jet Corp Pulsation impact spray nozzle
US4248296A (en) * 1979-08-07 1981-02-03 Resources Conservation Company Fluid distributor for condenser tubes
US4763841A (en) * 1986-04-29 1988-08-16 Daimler-Benz Aktiengesellschaft Injection nozzle for injecting fuel into the combustion chamber of an air-compressing fuel-injection engine
US5421521A (en) * 1993-12-23 1995-06-06 Caterpillar Inc. Fuel injection nozzle having a force-balanced check
US5628293A (en) * 1994-05-13 1997-05-13 Caterpillar Inc. Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
US5752308A (en) * 1994-05-20 1998-05-19 Caterpillar Inc. Method of forming a hard magnetic valve actuator
US5488340A (en) * 1994-05-20 1996-01-30 Caterpillar Inc. Hard magnetic valve actuator adapted for a fuel injector
US5449119A (en) * 1994-05-25 1995-09-12 Caterpillar Inc. Magnetically adjustable valve adapted for a fuel injector
US6257499B1 (en) 1994-06-06 2001-07-10 Oded E. Sturman High speed fuel injector
US6161770A (en) * 1994-06-06 2000-12-19 Sturman; Oded E. Hydraulically driven springless fuel injector
US5479901A (en) * 1994-06-27 1996-01-02 Caterpillar Inc. Electro-hydraulic spool control valve assembly adapted for a fuel injector
US5826562A (en) * 1994-07-29 1998-10-27 Caterpillar Inc. Piston and barrell assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US6575137B2 (en) 1994-07-29 2003-06-10 Caterpillar Inc Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US5673669A (en) * 1994-07-29 1997-10-07 Caterpillar Inc. Hydraulically-actuated fluid injector having pre-injection pressurizable fluid storage chamber and direct-operated check
US6082332A (en) * 1994-07-29 2000-07-04 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5687693A (en) * 1994-07-29 1997-11-18 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5697342A (en) * 1994-07-29 1997-12-16 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US6065450A (en) * 1994-07-29 2000-05-23 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5738075A (en) * 1994-07-29 1998-04-14 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5494220A (en) * 1994-08-08 1996-02-27 Caterpillar Inc. Fuel injector assembly with pressure-equalized valve seat
US5520338A (en) * 1994-09-21 1996-05-28 Caterpillar Inc. Fuel injector needle check valve biasing spring
US5605289A (en) * 1994-12-02 1997-02-25 Caterpillar Inc. Fuel injector with spring-biased control valve
US6173685B1 (en) 1995-05-17 2001-01-16 Oded E. Sturman Air-fuel module adapted for an internal combustion engine
US6148778A (en) * 1995-05-17 2000-11-21 Sturman Industries, Inc. Air-fuel module adapted for an internal combustion engine
US5597118A (en) * 1995-05-26 1997-01-28 Caterpillar Inc. Direct-operated spool valve for a fuel injector
US5720318A (en) * 1995-05-26 1998-02-24 Caterpillar Inc. Solenoid actuated miniservo spool valve
US5685490A (en) * 1995-07-27 1997-11-11 Caterpillar Inc. Fuel injector with pressure bleed-off stop
US6085991A (en) * 1998-05-14 2000-07-11 Sturman; Oded E. Intensified fuel injector having a lateral drain passage
US6425375B1 (en) 1998-12-11 2002-07-30 Caterpillar Inc. Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US20150114353A1 (en) * 2012-06-05 2015-04-30 Caterpillar Motoren Gmbh & Co. Kg Injection nozzle
US20150211460A1 (en) * 2014-01-30 2015-07-30 Denso Corporation Fuel injection nozzle
US9562503B2 (en) * 2014-01-30 2017-02-07 Denso Corporation Fuel injection nozzle
CN108348931A (en) * 2015-04-30 2018-07-31 叶青有限公司 Spray nozzle device
US20180236466A1 (en) * 2015-04-30 2018-08-23 Leafgreen Limited Spray nozzle arrangements

Also Published As

Publication number Publication date
GB1015429A (en) 1965-12-31
FR1312045A (en) 1962-12-14
LU42528A1 (en) 1962-12-15
DE1426141A1 (en) 1969-02-27

Similar Documents

Publication Publication Date Title
US3175771A (en) Fuel injectors for internal combustion engines
US4202500A (en) Multi-hole injection nozzle
US3035780A (en) Fuel injection nozzles for internal combustion engines
US1952816A (en) Fuel injector
US4528951A (en) Fuel injection valve for internal combustion engines
US3559892A (en) Fuel injection nozzle with auxiliary spray orifice
US5044561A (en) Injection valve for fuel injection systems
US3469793A (en) Fuel injection system
US4650121A (en) Injection nozzle for an air-compression fuel-injection internal combustion engine
US2627254A (en) Fuel injection nozzle
US4275845A (en) Fuel injector for internal combustion engines
US4394970A (en) Fuel injection nozzle for combustion engines
GB2319062A (en) Fuel-injection valve for internal combustion engines
US4413780A (en) Fuel injection nozzles
US4205790A (en) Fuel injector
EP0030258B1 (en) Fuel-injection nozzle for internal-combustion engines
US4208014A (en) Fuel injector for internal combustion engines
US6439483B2 (en) Variable orifice electronically controlled common rail injector (VOECRRI)
US1607805A (en) op milwaukee
KR960703196A (en) Fuel injection nozzel for internal combustion engine
US2708601A (en) Fuel-injecting apparatus for an internal combustion engine
GB2057057A (en) Fuel injector for diesel engine
US4162043A (en) Fuel injection nozzle
JPH05256228A (en) Fuel injection nozzle for internal combustion engine
JPS6245079Y2 (en)