GB2216608A - Fuel injection pumping apparatus - Google Patents
Fuel injection pumping apparatus Download PDFInfo
- Publication number
- GB2216608A GB2216608A GB8906030A GB8906030A GB2216608A GB 2216608 A GB2216608 A GB 2216608A GB 8906030 A GB8906030 A GB 8906030A GB 8906030 A GB8906030 A GB 8906030A GB 2216608 A GB2216608 A GB 2216608A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- throttle member
- fuel
- pressure pump
- pump
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
- F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
- F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
-
- 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
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/005—Arrangement of electrical wires and connections, e.g. wire harness, sockets, plugs; Arrangement of electronic control circuits in or on fuel injection apparatus
-
- 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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/20—Varying fuel delivery in quantity or timing
- F02M59/34—Varying fuel delivery in quantity or timing by throttling of passages to pumping elements or of overflow passages, e.g. throttling by means of a pressure-controlled sliding valve having liquid stop or abutment
-
- 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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/44—Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
Description
22 116608 - 1 FUEL INJECTION PUMPING APPARATUS' 2 - This invention relates
to a fuel injection pumping apparatus for supplying fuel to an internal combustion engine the apparatus comprising a body which houses a high pressure fuel pump, a low pressure fuel pump for supplying fuel to the high pressure pump. the pressure of fuel developed at the outlet of the low pressure pump varying in accordance with the speed of the associated engine. an angularly movable throttle member for controlling the supply of fuel from said outlet to the high pressure pump, and an electromagnetic actuator coupled to the throttle member and operable in resonse to a control signal from an electronic control system to adjust the angular setting of the throttle member.
When starting the associated engine an extra is amount of fuel is required and whilst the control system can be arranged to set the throttle member at the required position a difficulty can arise if the accumulator used for starting the engine is also used to provide power to the control system. When starting a cold engine the voltage applied to the control system, can fall below that required for correct functioning of the system.
The object of the present invention is to provide an apparatus of the aforesaid kind in a simple and convenient form.
According to the inventionj the throttle member is movable axially and is axially biased by a spring to an engine start position. the output pressure of the low pressure pump acting on the throttle member in opposition to the force exerted by the spring and when said pressure following starting of the associated engine, reaches a sufficiently high value the throttle member is moved axially to an engine run position, the - 2A - throttle member in said engine start position allowing a sufficient flow of fuel to the high pressure pump and the associated engine to allow starting of the engine, the flow of fuel to the engine being reduced as the throttle member is moved towards the engine run position.
In the accompanying drawings:- Figure 1 is a sectional side elevation of a part of a fuel pumping apparatus in accordance with the invention.
Figure 2 is a plan view of the part of the apparatus seen in Figure 1, and Figure 3 is a view similar to Figure 2 with part of a cover removed.
With reference to the drawings the apparatus includes a body 10 which houses a rotary distributor type fuel injection pumping apparatus. The apparatus is of a well known type and the control of the supply of fuel to the high pressure pump 11 is by means of an angularly adjustable throttle member 12. the fuel under is pressure being supplied by a low pressure pump 13. The throttle member is of cylindrical form and is located within a bore in the body 10. the inner end of the bore being connected to the outlet of the low pressure pump the outlet pressure of which is controlled by a valve in known manner,, so that it varies in accordance with the speed of the associated engine. The throttle member has an axial groove 14 formed in its peripheral surface and the groove receives fuel from the outlet of the low pressure pump. For registration with the groove a port 15 is formed in the body 10. the port being connected to- the inlet of the high pressure pump. The groove 14 is, as shown in Figure 1. inclined slightly to the axis of the throttle member. the axis being shown at 16 in Figure 1. Mounted on the throttle member is an arm 17 and adjacent the end of the arm is an upstanding pin 18.
1 i i 1 i i 1 t The arm 17 and the pin 18 lie on the exterior of the body 10 within a hollow generally rectangular housing 19 which is secured to the body. The housing serves to house an electromagnetic actuator 20, a transducer 21 and a damping device 22. Moreover. the upper wall of the housing accommodates an electrically insulating cable location block 23 by which connections are effected to an electronic control system 54.
The actuator, damping device and the transducer are constructed as a unit which is secured on the housing and the unit comprises a support 24 which at one end is machined or formed to hollow cup shape form to receive the stator of the actuator and at its other end is formed or machined to cup shape form to receive the stator of the transducer. Intermediate its ends the support defines a bore 25 and opening into the bore are a pair of axially spaced drillings 25A. The support 24 is formed from non-magnetic material such as aluminium and the inner peripheral surface of the skirt at said one end of the support is screw threaded to receive the complementarily threaded end portion of a tubular yoke 26 formed from magnetic material. The yoke is spun about a magnetic core member 26A within which is defined a tapering bore. A further magnetic core member 27 is provided with a cylindrical bore and also with a peripheral flange and is held in position against a base wall defined by the support 24 by the yoke 26. Surrounding the core members and lying within the yoke 26 is an annular winding 28.
Moreover. supported in the bore in the the core member 27 is a bearing sleeve formed from non-magnetic material. The sleeve supports an armature 29 for axial movement. the armature having a tapered portion which can enter into the tapered bore in the core member 26A. The armature and core membersare designed as a proportional solenoid.
In the end of the armature opposite to the tapered portion thereof there is formed a threaded drilling in which is secured the threaded end of a stepped non-magnetic connecting rod 30 the other end portion of which is provided with a transverse slot. A pin 31 extends across the slot and through the forked end portion of a link 32 the opposite end portion of which is also forked. the forks being provided with apertures through which can extend the pin 18. The two pins are engaged by the ends of a wire spring 33 which acts to take up any backlash between the pins and the apertures in the forks of the links.
Located about the rod is a tubular soft iron core 34,, a flanged locating piece 35 and a spring abutment 36, the latter engaging the armature 29 and the core 34 engaging a step defined on the rod. The core 34, the piece 35 and the abutment 36 are held in end to end engagement when the rod is screwed into the drilling in the armature. A coiled compression spring 37 is positioned between the abutment 36 and the core member 27 and an apertured cup-shaped damper piston 38 is located between the spring abutment 36 and the flange of the locating piece 35.
The skirt of the damper piston 38 is a sliding fit within the wall of the bore 25 and the piston together with the wall of the bore and the drillings 25A form a damper with the damping fluid being fuel,, which is contained within the housing. The aperture in the base wall of the piston 38 is slightly larger than the locating piece so that the piston can move transversely relative to the locating piece to avoid any problems due to misalignment. The piston is located against 1 is axial movement relative to the spring abutment by means of a shim interposed between the piston 38 and the abutment 36 or by means of a light spring. However. if desired the base wall of the piston can be formed to the correct thickness.
The transducer 21 includes a stator 40 formed from magnetic material which is of hollow cylindrical form having an inwardly directed flange at one end. The stator 40 is positioned within the cup-shaped end of the support 24 and within the stator is a tubular former 42 at one end of which is a boss 43 the former and boss being formed from an electrically insulating and non-magnetic material. The stator 40 is retained on the tubular former by means of a spring fastener 41 with the flange of the stator being held against a flange of the former. As seen in Figure 3 the boss 43 is secured by means of screws 44A to a pair of ears 45 defined by the support 24. As shown a shim is provided between the ears and the boss for the purpose of adjustment of the position of the boss and the associated components,, relative to the support. A winding 44 is wound about the former. The boss 43 defines a bearing for the rod and interposed between the boss and a sleeve 45A which surrounds the rod, is a further coiled compression spring 46. The sleeve 45A bears against a step defined adjacent the end of the rod and helps acts to locate and retain the pin 31.
Although a single winding 40 is shown it is in fact composed of a number of series connected axially spaced coils which are located in slots defined by the former.
As described the core 34 is subjected to the clamping force which is developed when the rod 30 is screwed into the armature 29. This can upset the magnetic properties of the core and as an alternative the rod can be surrounded by a stainless steel sleeve which is located between the step and the locating piece 35 and is subjected to the clamping force. The core surrounds the sleeve and is fractionally shorter than the sleeve. It can be secured in position for example by a suitable adhesive. Alternatively a further step can be defined as the rod which is engaged by the locating piece.
The unit formed by the support 24 and the components associated therewith is clamped relative to the upper wall of the housing 19 using a split clamp 47 which locates about the yoke 26. The clamp is secured to the housing by screws 47A and a clamping screw 47B can be slackened to permit axial adjustment of the support 24 within the housing,, the adjustment being facilitated by the provision of a slot 48 which is accessible through an access hole in the housing and which is closed by a plug 49or by a connector body. The support 24 defines a tongue 50 which locates in a slot in a part of the clamp to prevent angular movement of the support during the adjustment process.
When the winding 28 is de-energised the parts assume the position shown in the drawings with the flange of the locating piece 35 in engagement with the end of the tubular former 42. The axial adjustment of the support 24 will determine the setting of the throttle member 12 and once this has been set,, the clamp can be tightened. It is convenient to set the support 24 by first passing a current through the winding 28 thereby moving the armature until a predetermined transducer output is obtained. the support is then adjusted until the output of the pumping apparatus is within prescribed limits. Fine adjustment is achieved by using an adjustable stop 51 Y, which can be used to determine the axial setting of the throttle member when the pump is running and fuel under pressure is applied to the lower end of the throttle member.
In operation, the control system. 54 supplies electric current to the winding 28 of the actuator. The armature and therefore the throttle member will assume a position dependent upon the magnitude of the current. A signal indicative of the actual position of the rod and therefore the throttle member is obtained from the winding 44. Damping of the movement of the armature and the throttle member is provided by the damper and this limits the degree of overshoot or undershoot when the current flow in the winding 28 is varied.
The spring 33 serves to eliminate any backlash between the pins 18 and 31 and the apertures in which they are located and as will be seen from Figure 3, it is conveniently locat6d within the slotted end portions of the link 32. The spring 33 acts on the centre lines of the rod 30 and the arm 17 thereby to minimise the risk of causing jamming of the connection between the rod and the arm.
Two springs are provided to bias the rod and therefore the throttle member to the minimum fuel position and this provides a safety feature in the event that one of the springs breaks or weakens. it will be noted that the transducer is located intermediate the actuator and the throttle member so that assuming no breakage of the connection between the transducer and the throttle membert the transducer will always provide a signal indicative of the position of the throttle member. In the event therefore that the rod 30 becomes unscrewed from the armature 29, the transducer will still continue to give a signal indicative of the actual position of the throttle member. If for example, the rod 30 breaks adjacent the forked end thereof,, the spring 46 will move the throttle member to the minimum or zero fuel position. The transducer will however continue to provide a signal indicating a higher fuelling position, which is a safe condition.
If the control system is provided with stored information regarding the expected -position of the throttle for a given current flow in the winding 28 then if there is an appreciable difference in the actual position of the throttle for a given current, such as would be the case if one or both springs weaken or break or the rod unscrews. the control system can cause engine shut down or at least reduce the current flowing in the winding.
For engine starting purposes the control system can be arranged to set the throttle member at the desired position. However,, in cold conditions the voltage of the battery which powers the system can fall to a value which is less than that required for operation of the normal processor of the control system. It is therefore preferable to provide a separate start up control section which sets the throttle member and which receives signals from a speed sensor. If the engine speed exceeds a predetermined value before the battery voltage has risen to a value to allow operation of the processor,. the throttle member will be closed and an ONIOFF valve operated to prevent further flow of fuel to the engine.
Alternatively as shown in Figure 40 a 'mechanical' approach is possible and in this case the throttle member 12 is movable axially downwardly by a light spring 52 to an engine start position. The underside of the throttle member is exposed to the output pressure of the pump 13 and a drilling or groove 53 is provided on the throttle member which at rest communicates with the port 15 to allow fuel flow to the high pressure pump in sufficient quantity to allow starting of the engine. Once the engine starts the output pressure of the pump 13 acting on the underside of the valve member will urge the throttle member upwardly until a spring abutment engages a stop 55. to reduce the fuel supply to the engine and the throttle member will act as an hydraulic governor to control the is engine speed to a value below its normal idling speed. once the engine has started the control of the angular setting of the throttle member 12 is taken over by the control system. When the spring abutment is in contact with the stop 55 the throttle member is said to be in the engine run position. AS with the electronic starting control an engine shut off valve is incorporated into the design of the apparatus and in this case it forms the sole means of stopping the associated engine so that its operation is checked each time the engine is stopped.
It can be arranged that the groove or drilling 53 in the throttle member does not register with the port 15 until the throttle member 12 has been moved angularly by a small amount.
Claims (3)
1. A fuel injection pumping apparatus for supplying fuel to an internal combustion engine, comprising a body which houses a high pressure fuel pump, a low pressure fuel pump for supplying fuel to the high pressure pump, the pressure of fuel developed at the outlet of the low pressure pump varying in accordance with the speed of the associated engine, an angularly movable throttle member for controlling the supply of fuel from the low pressure pump to the high pressure pump, an electromagnetic actuator coupled to the throttle member and operable in response to a control signal from an electronic control system to adjust the angular setting of the throttle member during normal running of the engine, a spring biasing the throttle member axially to an engine start position, the output pressure of the low pressure pump acting on said throttle member in opposition to the force exerted by the spring and when said pressure following starting of the associated engine, reaches a sufficiently high value the throttle member is moved axially to an engine run position, the throttle member in said engine start position allowing a sufficient flow of fuel to the high pressure pump and the associated engine to allow starting of the engine, the flow of fuel to the engine being reduced as the throttle member is moved towards the engine run position.
2. An apparatus according to Claim 1 including a stop to determine the extent of movement of the throttle member against the action of the spring.
3. A fuel injection pumping apparatus for supplying fuel to an internal combustion engine comprising the J Q! i - 12 combination and arrangement of parts substantially as hereinbefore described with reference to the accompanying drawings.
Published 1989 atThe Patent Office, State House, 66171 High Holborn, londonWCIR4TP. Further copies maybe obtained from The Patent Oface. Sales Branch, St Mary Cray, Orpington, Kent BR5 3RD. Printed by Multiplex techniques ltd, St Mary Cray, Kent, Con. 1187
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB888807137A GB8807137D0 (en) | 1988-03-25 | 1988-03-25 | Fuel injection pumping apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8906030D0 GB8906030D0 (en) | 1989-04-26 |
GB2216608A true GB2216608A (en) | 1989-10-11 |
Family
ID=10634105
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB888807137A Pending GB8807137D0 (en) | 1988-03-25 | 1988-03-25 | Fuel injection pumping apparatus |
GB8906030A Withdrawn GB2216608A (en) | 1988-03-25 | 1989-03-16 | Fuel injection pumping apparatus |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB888807137A Pending GB8807137D0 (en) | 1988-03-25 | 1988-03-25 | Fuel injection pumping apparatus |
Country Status (5)
Country | Link |
---|---|
US (3) | US4873959A (en) |
EP (3) | EP0334557A1 (en) |
JP (4) | JPH01249927A (en) |
ES (1) | ES2013866A6 (en) |
GB (2) | GB8807137D0 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0624727A1 (en) * | 1993-05-14 | 1994-11-17 | Deere & Company | Fuel injection pump |
Families Citing this family (22)
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GB8726520D0 (en) * | 1987-11-12 | 1987-12-16 | Bramford Excavators Ltd J C | Engine to provide power to apparatus |
DE3937922A1 (en) * | 1989-11-15 | 1991-05-16 | Bosch Gmbh Robert | FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES |
US5067460A (en) * | 1990-06-22 | 1991-11-26 | Massachusetts Institute Of Technology | Variable air/fuel ratio engine control system with closed-loop control around maximum efficiency and combination of Otto-diesel throttling |
US5315977A (en) * | 1991-04-22 | 1994-05-31 | Dwayne Fosseen | Fuel limiting method and apparatus for an internal combustion vehicle |
DE4130125C2 (en) * | 1991-09-11 | 1996-04-04 | Licentia Gmbh | Mechanical manual adjustment device for the control stroke of an actuator |
RU2085757C1 (en) * | 1991-10-11 | 1997-07-27 | Катерпиллар Инк. | Valve and actuator unit for hydraulically operated nozzle with electronic control |
US5551406A (en) * | 1995-05-19 | 1996-09-03 | Siemens Electric Limited | Canister purge system having improved purge valve |
DE69606994T2 (en) * | 1995-05-19 | 2001-03-15 | Siemens Canada Ltd | TANK BLEEDING VALVE WITH IMPROVED BLEEDING VALVE |
US5954487A (en) * | 1995-06-23 | 1999-09-21 | Diesel Technology Company | Fuel pump control valve assembly |
US6247456B1 (en) | 1996-11-07 | 2001-06-19 | Siemens Canada Ltd | Canister purge system having improved purge valve control |
JP3558486B2 (en) * | 1997-05-15 | 2004-08-25 | 日産ディーゼル工業株式会社 | Fuel injection control system for diesel engine |
US6102364A (en) * | 1997-07-30 | 2000-08-15 | Siemens Canada Limited | Control accuracy of a pulse-operated electromechanical device |
GB2332476B (en) * | 1997-12-19 | 2002-01-16 | Caterpillar Inc | Fuel injector with solenoid and terminal assemblies |
US6158419A (en) * | 1999-03-10 | 2000-12-12 | Diesel Technology Company | Control valve assembly for pumps and injectors |
US6089470A (en) * | 1999-03-10 | 2000-07-18 | Diesel Technology Company | Control valve assembly for pumps and injectors |
US6450778B1 (en) | 2000-12-07 | 2002-09-17 | Diesel Technology Company | Pump system with high pressure restriction |
US6955336B2 (en) * | 2001-02-06 | 2005-10-18 | Delphi Technologies, Inc. | Sleeveless solenoid for a linear actuator |
US6845314B2 (en) * | 2002-12-12 | 2005-01-18 | Mirenco, Inc. | Method and apparatus for remote communication of vehicle combustion performance parameters |
US20070032808A1 (en) * | 2005-08-03 | 2007-02-08 | Azam Anwar | System and method for addressing total occlusion in a vascular environment |
CN104455655B (en) * | 2014-11-25 | 2017-01-04 | 北京亚新科天纬油泵油嘴股份有限公司 | A kind of proportional solenoid spool and apply the proportional solenoid of this spool |
EP3409878B1 (en) | 2017-06-02 | 2021-08-18 | Sandvik Intellectual Property AB | Down the hole drilling machine and method for drilling rock |
CN115027864A (en) | 2018-06-12 | 2022-09-09 | 自动存储科技股份有限公司 | Automated storage system and method for transporting storage containers in a storage system |
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FR822343A (en) * | 1936-05-30 | 1937-12-28 | Bosch Robert | Injection pump for internal combustion engines with varying speed between extended limits vehicle engines |
US2571571A (en) * | 1947-10-18 | 1951-10-16 | Nat Supply Co | Acceleration element for fuel controlling means for internal-combustion engines |
GB969825A (en) * | 1962-10-13 | 1964-09-16 | Georg Weisheit | Improvements in or relating to electro-magnetically-operated fluid flow control valves |
DE2138994C3 (en) * | 1971-08-04 | 1980-01-24 | Robert Bosch Gmbh, 7000 Stuttgart | Fuel distributor injection pump for internal combustion engines with electrical control of the delivery rate |
GB2061377B (en) * | 1979-09-18 | 1983-07-20 | Lucas Industries Ltd | I c engine fuel injection pumping systems |
GB2097484B (en) * | 1981-04-10 | 1984-04-26 | Lucas Industries Ltd | Fuel pumping apparatus |
US4351283A (en) * | 1981-05-01 | 1982-09-28 | General Motors Corporation | Diesel fuel injection pump secondary fuel metering control system |
US4446836A (en) * | 1981-10-23 | 1984-05-08 | Lucas Industries Public Limited Company | Fuel injection pumping apparatus |
DE3142715A1 (en) * | 1981-10-28 | 1983-05-05 | Robert Bosch Gmbh, 7000 Stuttgart | Adjustable radial piston pump |
JPS58160520A (en) * | 1981-12-31 | 1983-09-24 | オ−ビタル・エンジン・カンパニイ・プロプライエタリ・リミテツド | Fuel injector for internal combustion engine |
JPS58133081A (en) * | 1982-02-02 | 1983-08-08 | Canon Inc | Picture recorder |
DE3243348A1 (en) * | 1982-11-24 | 1984-05-24 | Robert Bosch Gmbh, 7000 Stuttgart | FUEL INJECTION PUMP |
ES8506138A1 (en) * | 1983-07-25 | 1985-07-01 | Stanadyne Inc | Electronic fuel control system for a fuel injection pump. |
GB8417862D0 (en) * | 1984-07-13 | 1984-08-15 | Lucas Ind Plc | Fuel pumping apparatus |
US4708111A (en) * | 1984-09-19 | 1987-11-24 | Nippondenso Co., Ltd. | Electronically controlled fuel injection based on minimum time control for diesel engines |
KR900009522Y1 (en) * | 1985-09-12 | 1990-10-13 | 지이제루 기기 가부시기가이샤 | Device for limiting rapid accelaration for internal combustion engine |
US4793311A (en) * | 1986-02-03 | 1988-12-27 | Stanadyne, Inc. | Fuel injection pump with multi-state load/speed control system |
JP2503410B2 (en) * | 1986-02-19 | 1996-06-05 | 日本電装株式会社 | Internal combustion engine speed control device |
-
1988
- 1988-03-25 GB GB888807137A patent/GB8807137D0/en active Pending
- 1988-07-18 JP JP63177282A patent/JPH01249927A/en active Pending
- 1988-07-18 JP JP63177283A patent/JPH01249928A/en active Pending
- 1988-07-18 JP JP63177281A patent/JPH01249930A/en active Pending
- 1988-07-18 JP JP63177280A patent/JPH01249929A/en active Pending
-
1989
- 1989-03-16 GB GB8906030A patent/GB2216608A/en not_active Withdrawn
- 1989-03-17 EP EP89302663A patent/EP0334557A1/en not_active Ceased
- 1989-03-17 EP EP89302664A patent/EP0334558A1/en not_active Withdrawn
- 1989-03-17 EP EP89302665A patent/EP0334559A1/en not_active Withdrawn
- 1989-03-20 US US07/325,540 patent/US4873959A/en not_active Expired - Fee Related
- 1989-03-20 US US07/326,155 patent/US4877005A/en not_active Expired - Fee Related
- 1989-03-20 US US07/326,154 patent/US4917065A/en not_active Expired - Fee Related
- 1989-03-22 ES ES8901053A patent/ES2013866A6/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0624727A1 (en) * | 1993-05-14 | 1994-11-17 | Deere & Company | Fuel injection pump |
Also Published As
Publication number | Publication date |
---|---|
EP0334559A1 (en) | 1989-09-27 |
GB8906030D0 (en) | 1989-04-26 |
JPH01249929A (en) | 1989-10-05 |
EP0334557A1 (en) | 1989-09-27 |
ES2013866A6 (en) | 1990-06-01 |
JPH01249928A (en) | 1989-10-05 |
JPH01249930A (en) | 1989-10-05 |
EP0334558A1 (en) | 1989-09-27 |
JPH01249927A (en) | 1989-10-05 |
US4917065A (en) | 1990-04-17 |
GB8807137D0 (en) | 1988-04-27 |
US4873959A (en) | 1989-10-17 |
US4877005A (en) | 1989-10-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |