GB2140081A - Fuel injection nozzle - Google Patents

Fuel injection nozzle Download PDF

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Publication number
GB2140081A
GB2140081A GB08410444A GB8410444A GB2140081A GB 2140081 A GB2140081 A GB 2140081A GB 08410444 A GB08410444 A GB 08410444A GB 8410444 A GB8410444 A GB 8410444A GB 2140081 A GB2140081 A GB 2140081A
Authority
GB
United Kingdom
Prior art keywords
valve member
fuel
bore
seating
passage
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.)
Granted
Application number
GB08410444A
Other versions
GB8410444D0 (en
GB2140081B (en
Inventor
David John Gaskell
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
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
Priority claimed from GB838313904A external-priority patent/GB8313904D0/en
Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB08410444A priority Critical patent/GB2140081B/en
Publication of GB8410444D0 publication Critical patent/GB8410444D0/en
Publication of GB2140081A publication Critical patent/GB2140081A/en
Application granted granted Critical
Publication of GB2140081B publication Critical patent/GB2140081B/en
Expired legal-status Critical Current

Links

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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/12Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship providing a continuous cyclic delivery with variable pressure
    • 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

Abstract

A fuel injection nozzle for supplying fuel to a compression ignition engine includes a valve member 17 movable against a spring 21 to allow fuel flow through an outlet 12 from a fuel inlet passage 15. The valve member is actuated by the pressure of fuel and the nozzle includes a passage 22 extending from said inlet passage 15 to a drain. The passage 22 includes a variable restrictor defined by a port 23 and the valve member 17, the degree of restriction to the flow of fuel through the passage 22 increasing as the valve member 17 moves against the action of the spring. <IMAGE>

Description

SPECIFICATION Fuel injection nozzles This invention relates to a fuel injection nozzle for supplying fuel to a compression ignition internal combustion engine and of the kind comprising a nozzle body, a bore defined in the body, an outlet at one end of the bore, a seating defined in the bore adjacent said outlet, a valve member slidable in said bore, said valve member being shaped for co-operation with said seating, resilient means biasing the valve member into contact with the seating, a fuel supply passage in the body, said passage communicating with said bore, and the valve member defining a surface against which in use, fuel under pressure in said passage can act to lift the valve member from the seating thereby to allow fuel flow from the supply passage through said outlet.
Such nozzles are well known in the art and in use the fuel supply passage is connected to the outlet of a fuel injection pump which delivers fuel at high pressure in timed relationship with the associated engine. For smooth running of a compression ignition engine it is desirable particularly when the total volume of fuel delivered to the engine is low as for example under light load conditions, that the injection period should be prolonged. In general, pumps of the kind utilised to supply fuel to a compression ignition engine are of the type in which the period of fuel delivery depends upon the amount of fuel to be delivered.Most of the pumps are cam actuated and while it is possible to so design a pumping flank of the cam lobe or lobes and to use different parts of the flank to obtain different rates of delivery, the pump and associated controls are not easy to design and put into practice.
The object of the present invention is to provide a fuel injection nozzle of the kind specified in a form in which the injection period of fuel to the associated engine can be prolonged.
According to the invention a fuel injection nozzle of the kind specified comprises a variable area restrictor in a flow passage extending from said supply passage to a drain, the degree of restriction offered by said restrictor being dependent upon the axial position of the valve member in the bore, the flow area of the restrictor decreasing as the valve member moves away from the seating.
An example of a fuel injection nozzle in accordance with the invention will now be described with reference to the accompanying diagrammatic drawing.
Referring to the drawing the nozzle comprises a stepped nozzle body 10 which in use, is secured to one end of a holder by means of a cap nut. The narrower end of the body extends into a combustion chamber of the associated engine.
Formed in the nozzle body is a bore 11 which at its end which opens onto the narrower end of the body, defines an outlet 1 2 of reduced diameter. The bore adjacent the aforesaid end also defines a seating 1 3 and intermediate the ends of the bore there is defined an enlargement 14 which is connected to a fuel supply passage 15. The passage 1 5 communicates with a further passage formed in the holder and in use, this passage is connected to the outlet of a fuel injection pump shown at 16. In practice there may be further passages 1 5 spaced about the axis of the nozzle to balance the flow of fuel into the enlargement 14.
Slidable within the bore 11 is a valve member 1 7 the valve member having an end shaped to co-operate with the seating 1 3. The valve member between the aforesaid end and the enlargement 14, is of reduced diameter to define an annular space between the bore and the valve member through which fuel can flow from the enlargement to the outlet 1 2.
The valve member because of the reduction in its diameter, defines an area which is exposed within the enlargement 14 against which fuel under pressure supplied through the passage 1 5 can act to lift the valve member away from the seating.
At its end adjacent the seating the valve member is provided with a shaped extension 1 8 which extends through the outlet 1 2 and which as the valve member moves away from the seating alters the effective area of the outlet.
At its opposite end the valve member is provided with a reduced portion 1 9 which mounts a spring abutment 20, this forming an abutment for one end of a coiled compression spring 21 which acts upon the valve member to bias the valve member into contact with the seating 13. The spring and the abutment are located within a chamber defined in the aforesaid hoider and the chamber is connected with a drain.
A flow path is defined between the passage 1 5 to the chamber and therefore the drain, by way of a short passage 22 extending from the passage 1 5 and opening into the bore 11 at a port 23. The remaining portion of the flow passage is defined by the aforesaid chamber.
The port 23 in conjunction with the valve member 17, constitutes a variable restrictor the flow area of which reduces as the valve member moves away from the seating. If the nozzle has more than one passage 1 5 additional passages 22 may be provided.
In operation, when fuel under pressure is supplied to the passage 1 5 by the pump 16 a flow of fuel will occur through the port 23.
However, the pressure in the enlargement 14 will increase to a value sufficient to lift the value member against the action of the spring 21. As the valve member lifts away from the seating 13, fuel will start to flow through the outlet 1 2 which forms in effect a variable restrictor. As the valve member lifts away from the seating there will be an increased area against which the fuel under pressure in the passage 1 5 can act. Moreover, the valve member continues to move away from the seating, the area of the outlet 1 2 will increase but at the same time the area of the port 23 will decrease and with continued movement of the valve member may decrease to zero.
The flow of fuel which occurs through the port 23 represents a loss in the volume of fuel delivered by the pump and therefore for a given volume of fuel required to flow through the outlet 1 2 an extra volume of fuel must be delivered by the pump. The period of fuel delivery will therefore be increased. Moreover, the rate of pressure rise in the enlargement 14 is more gradual than in a conventional nozzle and the initial rate of delivery of fuel through the outlet 1 2 will be reduced as compared with a nozzle in which the variable restrictor is absent. The extension of the injection period of fuel to the associated engine is more pronounced when the amount of fuel to be supplied to the engine is low as for example under light load running conditions.
At low lift as much as 50% of the fuel delivered by the pump can flow through the port 23.

Claims (3)

1. A fuel injection nozzle for supplying fuel to a compression ignition internal combustion engine and of the kind comprising a nozzle body, a bore defined in the body, an outlet at one end of the bore, a seating defined in the bore adjacent said outlet, a valve member slidable in said bore, said valve member being shaped for co-operation with said seating, resilient means biasing the valve member into contact with the seating, a fuel supply passage in the body, said passage communicating with said bore, and the valve member defining a surface against which in use, fuel under pressure in said passage can act to lift the valve member from the seating thereby to allow fuel flow from the supply passage through said outlet, characterised by a variable area restrictor in a flow passage extending from said supply passage to a drain, the degree of restriction offered by said restrictor being dependent upon the axial position of the valve member in the bore, the flow area of the restrictor decreasing as the valve member moves away from the seating.
2. A nozzle according to Claim 1 in which said flow passage includes a port opening into said bore, said port being progressively covered by said valve member as the valve member is lifted from its seating, the port and valve member constituting said variable area restrictor.
3. A fuel injection nozzle for supplying fuel to a compression ignition internal combustion engine comprising the combination and arrangement of parts substantially as hereinbefore described with reference to the accompanying drawing.
GB08410444A 1983-05-19 1984-04-24 Fuel injection nozzles Expired GB2140081B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08410444A GB2140081B (en) 1983-05-19 1984-04-24 Fuel injection nozzles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838313904A GB8313904D0 (en) 1983-05-19 1983-05-19 Fuel injection nozzles
GB08410444A GB2140081B (en) 1983-05-19 1984-04-24 Fuel injection nozzles

Publications (3)

Publication Number Publication Date
GB8410444D0 GB8410444D0 (en) 1984-05-31
GB2140081A true GB2140081A (en) 1984-11-21
GB2140081B GB2140081B (en) 1986-09-17

Family

ID=26286179

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08410444A Expired GB2140081B (en) 1983-05-19 1984-04-24 Fuel injection nozzles

Country Status (1)

Country Link
GB (1) GB2140081B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2562605A1 (en) * 1984-04-05 1985-10-11 Lucas Ind Plc FUEL INJECTION DEVICE FOR A COMPRESSION IGNITION ENGINE
GB2255373A (en) * 1991-04-26 1992-11-04 Kloeckner Humboldt Deutz Ag Diesel engine fuel injection system.
GB2299374A (en) * 1995-03-27 1996-10-02 Caterpillar Inc Valved injection nozzle
US5743237A (en) * 1997-01-28 1998-04-28 Caterpillar Inc. Hydraulically-actuated fuel injector with needle valve operated spill passage

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB407654A (en) * 1933-02-25 1934-03-22 Sulzer Ag Improvements in or relating to water-cooled fuel injection valves for internal combustion engines
GB1435702A (en) * 1972-06-12 1976-05-12 Nat Res Dev Injectors for the fuel injection systems of internal combustion engines
GB1560548A (en) * 1975-10-29 1980-02-06 Cummins Engine Co Inc Fuel injector for an internal combustion engine
GB2080414A (en) * 1980-07-18 1982-02-03 Lucas Industries Ltd I.C. engine fuel injection nozzle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB407654A (en) * 1933-02-25 1934-03-22 Sulzer Ag Improvements in or relating to water-cooled fuel injection valves for internal combustion engines
GB1435702A (en) * 1972-06-12 1976-05-12 Nat Res Dev Injectors for the fuel injection systems of internal combustion engines
GB1560548A (en) * 1975-10-29 1980-02-06 Cummins Engine Co Inc Fuel injector for an internal combustion engine
GB2080414A (en) * 1980-07-18 1982-02-03 Lucas Industries Ltd I.C. engine fuel injection nozzle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2562605A1 (en) * 1984-04-05 1985-10-11 Lucas Ind Plc FUEL INJECTION DEVICE FOR A COMPRESSION IGNITION ENGINE
GB2255373A (en) * 1991-04-26 1992-11-04 Kloeckner Humboldt Deutz Ag Diesel engine fuel injection system.
GB2299374A (en) * 1995-03-27 1996-10-02 Caterpillar Inc Valved injection nozzle
US5645224A (en) * 1995-03-27 1997-07-08 Caterpillar Inc. Modulating flow diverter for a fuel injector
GB2299374B (en) * 1995-03-27 1999-02-24 Caterpillar Inc Modulating flow diverter for a fuel injector
US5743237A (en) * 1997-01-28 1998-04-28 Caterpillar Inc. Hydraulically-actuated fuel injector with needle valve operated spill passage

Also Published As

Publication number Publication date
GB8410444D0 (en) 1984-05-31
GB2140081B (en) 1986-09-17

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Legal Events

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PCNP Patent ceased through non-payment of renewal fee