USRE34999E - Hole type fuel injector and injection method - Google Patents
Hole type fuel injector and injection method Download PDFInfo
- Publication number
- USRE34999E USRE34999E US08/071,526 US7152693A USRE34999E US RE34999 E USRE34999 E US RE34999E US 7152693 A US7152693 A US 7152693A US RE34999 E USRE34999 E US RE34999E
- Authority
- US
- United States
- Prior art keywords
- valve
- metering
- fuel
- needle valve
- valve seat
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/10—Other injectors with elongated valve bodies, i.e. of needle-valve type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M45/00—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
- F02M45/02—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
- F02M45/04—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
- F02M45/08—Injectors peculiar thereto
- F02M45/083—Having two or more closing springs acting on injection-valve
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M45/00—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
- F02M45/12—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship providing a continuous cyclic delivery with variable pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
Definitions
- the present invention relates generally to fuel injectors for diesel engine fuel injection systems and relates more particularly to a new and improved hole type fuel injector and injection method.
- a principal object of the present invention is to provide in a hole type fuel injector, a new and improved fuel injection nozzle assembly and method providing multi-stage fuel injection or rate shaping.
- Another object of the present invention is to provide in a hole type fuel injector, a new and improved fuel injection nozzle assembly and method providing pre-injection.
- a further object of the present invention is to provide in a hole type fuel injector, a new and improved fuel injection nozzle assembly and method providing fuel metering during all initial stage of valve operation.
- a further object of the present invention is to provide in a hole type fuel injector, a new and improved fuel injection nozzle assembly and method which assists in maintaining fuel pressure at the valve seat until valve closure to reduce or eliminate secondary injections, end of injection fuel dribble and cavitation erosion of the valve seat and adjacent area.
- a further object of the present invention is to provide in a hole type fuel injector, a new and improved nozzle assembly which fulfills one or more of the foregoing objects of the present invention and which has an economical design that can be manufactured at relatively low cost.
- FIG. 1 is a longitudinal sectional view, partly broken away and partly in section, of a hole type fuel injector incorporating an embodiment of the present invention
- FIG. 2 is an enlarged longitudinal sectional view, partly broken away and partly in section, of a nozzle body and needle valve of the fuel injector;
- FIG. 3 is an enlarged longitudinal sectional view, partly broken away and partly in section, showing the relationship of inner and outer metering rings and metering edges of the nozzle body and needle valve when the valve is closed;
- FIG. 4 is a graph showing the relationship of needle valve lift and time during an exemplary injection cycle of the fuel injector.
- FIGS. 1-3 show a hole type fuel injector 10 comprising an elongated, one piece, nozzle body 12 with an elongated valve bore 14 and an elongated nozzle needle valve 16 axially reciprocable within the valve bore 14.
- Tile nozzle body 12 has a lower end tip 20 coaxial with and enclosing the lower end of the valve bore 14.
- the nozzle body 12 has an internal, upwardly facing, coaxial conical surface 18 providing an annular valve seat 19 immediately above the nozzle lip 20.
- the needle valve 16 has a lower conical end with approximately line contact engagement with the valve seat 19 when the valve is closed.
- One or more small diameter spray holes 22 are provided below the valve seat 19 in the end tip 20.
- one or more spray holes 22 may be provided in the cortical surface 18 below the valve seat 19.
- the spray holes 22 provide for spraying small droplets of fuel for combustion. The number, diameter and exact location of the spray holes 22 are selected for each application.
- the nozzle body 12 has upper and lower, coaxial valve guides 26, 28 which cooperate with upper and lower, coaxial guides 30, 32 of the needle valve 16 to guide the reciprocal movement of the needle valve 16.
- the upper valve guide 26 is located just below the top of the nozzle body 12 and the lower valve guide 28 is spaced below the upper valve guide 26 and above the valve seat 19.
- An upper annular fuel chamber 34 surrounding the needle valve 16 is provided between the upper and lower valve guides 26, 28.
- a lower annular fuel chamber 36 surrounding the needle valve 16 is provided between the lower valve guide 28 and valve seat 19.
- a coil compression spring 38 mounted above the needle valve 16 urges the needle valve 16 downwardly to its closed position.
- a single spring 38 is shown.
- An additional second stage spring (not shown) may be used if desired to enhance, extend or modify the characteristics of the two stage valve operation hereinafter described.
- a shim 39 is employed to precisely set the pre-load of the spring 38 and thereby precisely establish the valve opening pressure (i.e., 1he pressure at which the needle valve 16 begins to lift off the valve seat 19).
- An adaptor plate 40 mounted on the nozzle body 12 serves as a stop engageable by the upper guide 30 of the needle valve 16 to limit valve lift.
- the needle valve 16 has a predetermined maximum lift which is preferably within the usual range of maximum lift of 0.008 to 0.016 inch of hole type nozzles.
- the diameter of the upper guide 30 of the needle valve 16 is larger than the diameter of the annular valve seat 19 to provide a differential area for hydraulically lifting the needle valve 16 from the valve seat 19 for fuel injection.
- the needle valve 16 is periodically actuated by high pressure pulses of fuel supplied via one or more internal fuel passages 42 in the nozzle body 12 to the upper annular chamber 34.
- the high pressure pulses typically have a maximum pressure within a range of 4,000 to 17,000 psi. That maximum pressure and the valve opening pressure (which is typically within the range of 2,800 to 5,000 psi) are functions of the spring characteristics and pre-load setting of the closure spring 38 and the shape of the high pressure pulse.
- each high pressure pulse acts on the described differential area to open the needle valve 16 against the bias of the closure spring 38 and to supply fuel for fuel injection through the spray holes 22.
- the lower guide 32 of the needle valve 16 cooperates with the lower valve guide 28 to restrict or throttle fuel flow between the upper and lower fuel chambers 34, 36 during part of the reciprocable movement of the needle valve 16. Regulation is provided during an initial upward increment of travel and a corresponding last downward increment of travel of the needle valve 16. That increment is preferably within the range of approximately 0.004 to 0.008 inch or approximately one-half the maximum lift of the needle valve 16.
- the lower guide 32 of the needle valve 16 has upper and lower spaced sections 80, 82 with outer cylindrical surfaces.
- the lower section 52 is shown having three equiangularly spaced, axially extending flats 54 providing axial passages for unrestricted fuel flow.
- a conical surface 56 in combination with the flats 54, provides a peripheral annulus between the spaced sections 50, 52 for connecting the upper ends of the three axial passages.
- the lower part of the upper section 50 forms an inner metering ring 60 that is received within an outer metering ring 62 of the lower fixed guide 28 when the needle valve 16 is seated.
- the inner metering ring 60 has an external cylindrical metering surface with a lower circular metering edge 64.
- the outer metering ring 62 has an internal cylindrical metering surface with an upper circular metering edge 66.
- Each metering edge 64, 66 is a sharp edge formed in the shown embodiment by the respective cylindrical metering surface and an adjacent perpendicular shoulder.
- a clearance passage 68 having a radial clearance b is provided between the two opposing cylindrical metering surfaces.
- the diametrical clearance between the two metering surfaces in the shown embodiment is preferably within the range of 0.0003 to 0.0006 inch.
- the lower section 52 is provided to maintain the concentricity of the inner and outer metering rings 62, 64.
- the lower guide section 52 and intermediate conical surface 56 and flats 54 may be excluded and the axial length of the lower valve guide 28 may be reduced accordingly.
- the inner and outer metering rings 60, 62 cooperate to regulate flow between the upper and lower chambers 34, 36 during part of the upward and downward movement of the needle valve 16.
- Flow metering or throttling occurs during an initial increment of valve lift and a corresponding last increment of needle valve 16 closure.
- the annular metering rings 60, 62 cooperate to regulate flow during the initial upward and last downward increments of movement of the needle valve 16 of 0.006 inch.
- Both metering edges 64, 66 are preferably coaxial, circular edges as shown.
- one or both of the metering rings 60, 62 may have a different shape to provide a more gradual transition between regulated and non-regulated conditions as the needle valve 16 reciprocates.
- the pressure in the lower chamber 36 Prior to valve opening, the pressure in the lower chamber 36 is essentially the same as that in the upper chamber 34. That is so, even during a rapid increase in pressure at the beginning of a high pressure pulse, because, with the needle valve 16 closed, only extremely little flow through the clearance passage 68 is required to equalize the pressure between the upper and lower chambers 34, 36.
- the lower chamber pressure will be less than the upper chamber pressure due to the fuel throttling or metering provide by the clearance passage 68. Accordingly, the net hydraulic opening bias on the needle valve 16 will be less than before the needle valve 16 opened and less than it would have been if there were no restriction. Consequently, an upper chamber pressure higher than otherwise is required to open the needle valve 1 further. Further valve opening is therefore slowed or delayed for a short but meaningful period during which the rate of fuel injection is metered or throttled by the clearance passage 68.
- valve operation and fuel injection occur in two stages: a first stage of partial valve opening during which there is a regulated or reduced rate of fuel injection and a second stage of unthrotlled fuel injection.
- the first stage may be viewed as having two phases.
- a first initial opening phase as the upper chamber pressure rises above the valve opening pressure, the valve may modulate or dither briefly between open and closed positions.
- Valve modulation continues during a succeeding second phase when the upper chamber pressure is sufficiently high to keep the valve from closing.
- Second phase valve modulation continues until the total valve opening force produced by the different fuel pressures in the upper and lower chambers 34, 36 is sufficient to propel the valve upward to its fully open position.
- a representative fuel injection cycle is illustrated in FIG. 4.
- the diameter of the lower guide 32 is selected to provide the the desired valve modulation. If the lower guide 32 diameter is less than or equal to the diameter of the valve seat 19, there will be no first stage valve modulation and the needle valve 16 will be propelled to its fully open position in a single step. At the other extreme, if the lower guide 32 diameter is equal to or greater than the diameter of the upper guide 30, the needle valve 16 will dither or fluctuate between open and closed positions and never fully open. Although each of those modes of operation may be desirable certain applications, in general the diameter of the lower guide 32 should lie in a central range between the diameter of the valve seat 19 and upper guide 30.
- the two stage valve operation is affected by the pressure/time curve or shape of the high pressure fuel pulse.
- the pulse shape varies with engine speed. At higher engine speeds, the pressure of the high pressure pulse increases more rapidly, thereby giving less time for effective two stage operation to occur. As a result, first stage operation typically is more pronounced at lower RPM.
- Certain nozzle dimensions or parameters are established for each application to provide the desired two stage and two phase operation.
- nozzle parameters and their preferred nominal dimensional range are as follows:
- the axial position of the metering rings 60, 62 relative to the valve seat 19 can affect the two stage operation. In general, it is believed that the metering rings 60, 62 should be located closer to the valve seat 19 than to the upper guides 26, 30 to reduce the volume of the lower fuel chamber 36 and to increase the responsiveness of needle valve 16.
- first stage fuel regulation can be made relatively insensitive to valve lift by reducing the reliance on fuel metering between the needle valve 16 and valve seat 19. More effective and consistent rate shaping is thereby achieved.
- first stage valve operation can be extended to higher speeds or otherwise enhanced or modified by adding a second stage closure spring (not shown).
- the first stage spring provides a first stage valve opening limit of for example 0.004 inch (for use in combination with a metering ring width a of 0.006 inch) and the second stage spring provides an additional second stage valve opening limit of for example 0.008 inch (giving a total valve lift of 0.012 inch).
- the needle valve 16 would be temporarily held at the first stage limit position of 0.004 inch lift.
- the needle valve 16 would be held at the second stage limit position of 0.012 inch lift.
- the rate of fuel injection is not affected by the metering rings 60, 62. Also, the transition between the first and second stages, during which the cooperating metering rings 60, 62 have varying transitional affect, is extremely quick. In the first stage, valve behavior and thus the rate of fuel injection are determined primarily by the rate of fuel flow between the metering rings 60, 62. In the second stage, the needle valve 16 is quickly propelled to and held at its fully open position. The width, diameter and configuration of the metering rings are predetermined for each nozzle application to shape this two stage valve operation as desired.
- the metering rings 60, 62 also affect fuel flow during valve closure.
- the inner metering ring 60 serves as a pump to pressurize fuel in the lower chamber 36 and to restrict fuel flow between the upper and lower chambers 34, 36.
- the parameters and other factors discussed above will also impact that pumping action. Because of that pumping action, the fuel pressure at the spray holes 22 and valve seat 19 will be maintained at a higher pressure than otherwise until the needle valve 16 is completely closed. The higher pressure will help eliminate or reduce fuel dribble from the spray holes 22 and will help eliminate or reduce cavitation within the lower fuel chamber 36 by helping to both collapse and prevent vapor cavities which typically form at or near the valve seat 19 during valve closure.
- the clearance passageway 68 will help dampen any pressure wave in the tapper chamber 34 (caused by reflection of the injection pulse and following each injection event) from reaching the lower fuel chamber 36 to eliminate undesirable "secondary" fuel injection and further minimize cavitation within the lower fuel chamber 36.
- the injector 10 shown in the drawings is designed to be employed in fuel systems utilizing a remote high pressure pump connected to supply the high pressure fuel pulses to the fuel injector 10 via a high pressure fuel line.
- the present invention is also readily adaptable to other types of fuel injectors, for example unit injectors employing a high pressure pump as part of the fuel injector assembly. Also, as will be apparent to persons skilled in the art, other modifications, adaptations and variations of the foregoing specific disclosure can be made without departing from the teachings of the present invention.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
______________________________________ Parameter Nominal Dimensional Range ______________________________________ Diameter ofupper valve guide 26 0.150 to 0.180 inch Diameter oflower valve guide 28 0.120 to 0.160inch Diametrical clearance 68 0.0003 to 0.0006 inch Diameter ofvalve seat 19 0.079 to 0.104 inch Metering ring width a 0.004 to 0.006 inch Maximum valve lift 0.008 to 0.012 inch ______________________________________
Claims (21)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/071,526 USRE34999E (en) | 1990-03-28 | 1993-06-02 | Hole type fuel injector and injection method |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/500,714 US5020500A (en) | 1990-03-28 | 1990-03-28 | Hole type fuel injector and injection method |
| US08/071,526 USRE34999E (en) | 1990-03-28 | 1993-06-02 | Hole type fuel injector and injection method |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US07/500,714 Reissue US5020500A (en) | 1990-03-28 | 1990-03-28 | Hole type fuel injector and injection method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USRE34999E true USRE34999E (en) | 1995-07-25 |
Family
ID=23990610
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US07/500,714 Ceased US5020500A (en) | 1990-03-28 | 1990-03-28 | Hole type fuel injector and injection method |
| US08/071,526 Expired - Lifetime USRE34999E (en) | 1990-03-28 | 1993-06-02 | Hole type fuel injector and injection method |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US07/500,714 Ceased US5020500A (en) | 1990-03-28 | 1990-03-28 | Hole type fuel injector and injection method |
Country Status (1)
| Country | Link |
|---|---|
| US (2) | US5020500A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0892171A3 (en) * | 1997-06-11 | 2000-06-07 | Stanadyne Automotive Corp. | Servo controlled common rail injector |
| US6116209A (en) | 1998-05-27 | 2000-09-12 | Diesel Technology Company | Method of utilization of valve bounce in a solenoid valve controlled fuel injection system |
| US7249722B2 (en) | 2004-03-30 | 2007-07-31 | Stanadyne Corporation | Fuel injector with hydraulic flow control |
| US20090032622A1 (en) * | 2007-07-31 | 2009-02-05 | Dennis Henderson Gibson | Fuel injector nozzle with flow restricting device |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6161773A (en) * | 1994-05-31 | 2000-12-19 | Caterpillar Inc. | Fuel injector nozzle with guide to check clearance passage providing injection rate shaping |
| US5505384A (en) * | 1994-06-28 | 1996-04-09 | Caterpillar Inc. | Rate shaping control valve for fuel injection nozzle |
| JPH08144896A (en) * | 1994-11-25 | 1996-06-04 | Zexel Corp | Variable nozzle hole type fuel injection nozzle |
| US5647536A (en) * | 1995-01-23 | 1997-07-15 | Cummins Engine Company, Inc. | Injection rate shaping nozzle assembly for a fuel injector |
| US5619969A (en) * | 1995-06-12 | 1997-04-15 | Cummins Engine Company, Inc. | Fuel injection rate shaping control system |
| US5947389A (en) * | 1996-06-06 | 1999-09-07 | Zexel Corporation | Variable nozzle hole type fuel injection nozzle |
| GB9623469D0 (en) * | 1996-11-12 | 1997-01-08 | Lucas Ind Plc | Injector |
| US5765755A (en) * | 1997-01-23 | 1998-06-16 | Cummins Engine Company, Inc. | Injection rate shaping nozzle assembly for a fuel injector |
| US5743237A (en) * | 1997-01-28 | 1998-04-28 | Caterpillar Inc. | Hydraulically-actuated fuel injector with needle valve operated spill passage |
| DE19818200A1 (en) * | 1998-04-23 | 1999-10-28 | Bosch Gmbh Robert | Fuel injection valve for internal combustion engine |
| DE19844638A1 (en) * | 1998-09-29 | 2000-03-30 | Siemens Ag | Fuel injection valve for an internal combustion engine |
| DE19901057A1 (en) * | 1999-01-14 | 2000-07-27 | Bosch Gmbh Robert | Fuel injection valve for internal combustion engines |
| US6173913B1 (en) * | 1999-08-25 | 2001-01-16 | Caterpillar Inc. | Ceramic check for a fuel injector |
| DE10101562A1 (en) * | 2001-01-15 | 2002-07-25 | Bosch Gmbh Robert | Fuel injector |
| US7334741B2 (en) | 2005-01-28 | 2008-02-26 | Cummins Inc. | Fuel injector with injection rate control |
| WO2006091429A1 (en) * | 2005-02-22 | 2006-08-31 | Siemens Vdo Automotive Corporation | Common rail injector with active needle closing device |
| GB0801997D0 (en) * | 2007-05-01 | 2008-03-12 | Delphi Tech Inc | Fuel injector |
| US8591747B2 (en) * | 2008-05-27 | 2013-11-26 | Dober Chemical Corp. | Devices and methods for controlled release of additive compositions |
| US7942349B1 (en) * | 2009-03-24 | 2011-05-17 | Meyer Andrew E | Fuel injector |
| DE102009055135A1 (en) * | 2009-12-22 | 2011-06-30 | Robert Bosch GmbH, 70469 | Leak-free fuel injector |
| CN102213166B (en) * | 2010-04-08 | 2013-01-30 | 北京亚新科天纬油泵油嘴股份有限公司 | High-pressure common-rail electronic control oil injector |
| US9822748B2 (en) | 2014-05-31 | 2017-11-21 | Cummins Inc. | Restrictive flow passage in common rail injectors |
| CN104061101A (en) * | 2014-07-14 | 2014-09-24 | 北京亚新科天纬油泵油嘴股份有限公司 | Fuel feed system oil sprayer and oil spray nozzle thereof |
| US20250369410A1 (en) * | 2024-06-04 | 2025-12-04 | Caterpillar Inc. | Fuel injector and nozzle assembly configured for limiting cavitation damage |
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| US3032279A (en) * | 1960-11-21 | 1962-05-01 | Eddington Metal Specialty Comp | Nozzle construction |
| US3368761A (en) * | 1965-10-15 | 1968-02-13 | Mack Trucks | Variable flow rate fuel injection nozzle |
| US3838821A (en) * | 1972-07-20 | 1974-10-01 | Cav Ltd | Fuel injection nozzle units |
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| US4470548A (en) * | 1981-11-09 | 1984-09-11 | Nissan Motor Company, Limited | Fuel injection nozzle for an internal combustion engine |
| US4506833A (en) * | 1981-11-09 | 1985-03-26 | Nissan Motor Company, Limited | Fuel injection nozzle for an internal combustion engine |
| US4524914A (en) * | 1983-01-27 | 1985-06-25 | Diesel Kiki Co., Ltd. | Throttling pintle-type fuel injection nozzle having an improved initial injection characteristic |
| US4540126A (en) * | 1982-04-08 | 1985-09-10 | Nissan Motor Co., Ltd. | Fuel injection nozzle |
| US4627571A (en) * | 1984-03-15 | 1986-12-09 | Nippondenso Co., Ltd. | Fuel injection nozzle |
| US4629127A (en) * | 1983-09-05 | 1986-12-16 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Intermittent swirl type injection valve |
| US4684067A (en) * | 1986-03-21 | 1987-08-04 | General Motors Corporation | Two-stage, hydraulic-assisted fuel injection nozzle |
| US4693420A (en) * | 1986-08-25 | 1987-09-15 | General Motors Corporation | Air-assist fuel injection nozzle |
| US4715541A (en) * | 1985-02-26 | 1987-12-29 | Steyr-Daimler-Puch Ag | Fuel injection nozzle for combustion engines |
| US4811715A (en) * | 1987-11-02 | 1989-03-14 | Stanadyne, Inc. | Electronic unit injector |
| US4957085A (en) * | 1989-02-16 | 1990-09-18 | Anatoly Sverdlin | Fuel injection system for internal combustion engines |
-
1990
- 1990-03-28 US US07/500,714 patent/US5020500A/en not_active Ceased
-
1993
- 1993-06-02 US US08/071,526 patent/USRE34999E/en not_active Expired - Lifetime
Patent Citations (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1944371A (en) * | 1930-06-25 | 1934-01-23 | Ritz Frederick | Injector |
| US2627254A (en) * | 1947-06-12 | 1953-02-03 | Texas Co | Fuel injection nozzle |
| US2588485A (en) * | 1949-03-07 | 1952-03-11 | Lucas Ltd Joseph | Liquid fuel burner nozzle |
| US3032279A (en) * | 1960-11-21 | 1962-05-01 | Eddington Metal Specialty Comp | Nozzle construction |
| US3368761A (en) * | 1965-10-15 | 1968-02-13 | Mack Trucks | Variable flow rate fuel injection nozzle |
| US3838821A (en) * | 1972-07-20 | 1974-10-01 | Cav Ltd | Fuel injection nozzle units |
| US4036192A (en) * | 1974-02-08 | 1977-07-19 | Diesel Kiki Co. | Engine fuel injection system |
| US4284049A (en) * | 1978-03-22 | 1981-08-18 | Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | Fuel injector valve needle lift control arrangement |
| DE3113755A1 (en) * | 1981-04-04 | 1982-12-16 | Daimler-Benz Ag, 7000 Stuttgart | Fuel injection nozzle for internal combustion engine |
| US4394972A (en) * | 1981-04-14 | 1983-07-26 | Lucas Industries Plc | Fuel injection nozzles |
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| US4629127A (en) * | 1983-09-05 | 1986-12-16 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Intermittent swirl type injection valve |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0892171A3 (en) * | 1997-06-11 | 2000-06-07 | Stanadyne Automotive Corp. | Servo controlled common rail injector |
| US6116209A (en) | 1998-05-27 | 2000-09-12 | Diesel Technology Company | Method of utilization of valve bounce in a solenoid valve controlled fuel injection system |
| US7249722B2 (en) | 2004-03-30 | 2007-07-31 | Stanadyne Corporation | Fuel injector with hydraulic flow control |
| US20090032622A1 (en) * | 2007-07-31 | 2009-02-05 | Dennis Henderson Gibson | Fuel injector nozzle with flow restricting device |
| US7690588B2 (en) | 2007-07-31 | 2010-04-06 | Caterpillar Inc. | Fuel injector nozzle with flow restricting device |
Also Published As
| Publication number | Publication date |
|---|---|
| US5020500A (en) | 1991-06-04 |
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