EP0365143A1 - Buse d'injection de combustible - Google Patents

Buse d'injection de combustible Download PDF

Info

Publication number
EP0365143A1
EP0365143A1 EP89309497A EP89309497A EP0365143A1 EP 0365143 A1 EP0365143 A1 EP 0365143A1 EP 89309497 A EP89309497 A EP 89309497A EP 89309497 A EP89309497 A EP 89309497A EP 0365143 A1 EP0365143 A1 EP 0365143A1
Authority
EP
European Patent Office
Prior art keywords
valve member
fuel
bore
sleeve means
sleeve
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Withdrawn
Application number
EP89309497A
Other languages
German (de)
English (en)
Inventor
Robert Henry Scott
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
Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of EP0365143A1 publication Critical patent/EP0365143A1/fr
Withdrawn legal-status Critical Current

Links

Images

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
    • 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

Definitions

  • the present invention relates to a fuel injection nozzle.
  • Fuel injection nozzles are used to supply fuel to an internal combustion engine. They are used in both diesel and petrol injection engines, although the preferred embodiment to be described is primarily intended for a diesel injection engine which operates at hig pressures.
  • the preferred fuel injection nozzle of the invention is of a so called "two-stage lift" type of injection nozzle, in which a valve member which closes fuel injection jets in the nozzle, is retractable against a spring force over a first range of movement by the effect of a lower fuel pressure range, and over a further, second range of movement by the effect of a discontinuously greater range of pressure.
  • a valve member which closes fuel injection jets in the nozzle is retractable against a spring force over a first range of movement by the effect of a lower fuel pressure range, and over a further, second range of movement by the effect of a discontinuously greater range of pressure.
  • the discontinuity between the two ranges of pressures be great, but in some applications it is desired that the discontinuity be small and there have been difficulties with providing fuel injection nozzles in which this discontinuity is present, but is small.
  • the present invention provides, according to one aspect, a fuel injection nozzle for supplying fuel to an internal combustion engine comprising
  • a body including a bore and a fuel inlet passage through which, in use, fuel under pressure is supplied to the bore, one end of said bore including an outlet and a valve means; a valve member moveably mounted in the bore, said valve member being arranged so that when it is in a first position it closes said valve means to close communication between said bore and said outlet, the valve member including a rearwardly facing shoulder means; a sleeve means surrounding the valve member behind the rearwardly facing shoulder means, said valve member being retractable from said first position to a second position in which its rearwardly facing shoulder means engages said sleeve means; a stop means, said valve member being further retractable from said second position to a third position in which it is stopped from further retraction by engagement of said stop means with a first part of said sleeve means and a second part of said sleeve means with said rearwardly facing shoulder means of said valve member; biasing means for urging the valve member in a forwards direction towards said first position, the arrangement being such
  • Said first part of said sleeve means is preferably a rear end surface of said sleeve means, said second part is preferably a front end surface of said sleeve means and the third part is preferably a rearwardly facing shoulder intermediate the opposite ends of the sleeve means.
  • the rearwardly facing shoulder of the sleeve means preferably extends into a chamber formed by the sleeve means, and the bore, the chamber being fluidly connected to said fluid inlet passage whereby the pressure of the fuel is applied to said chamber.
  • Means may be provided to restrain movement of the sleeve means whilst said valve member is between said first and second positions, so that the second force is not transmitted by the front end of the sleeve means to said rearwardly facing shoulder.
  • Said means to restrain the sleeve means may comprise a shoulder in the bore, which engages with the front end surface of the sleeve means.
  • the nozzle comprises a body 10 above which is mounted an adapter plate 11. Above the adapter plate 11 is a spring housing 12, parts 10,11,12 being mounted in a casing 13. The parts 10 to 13 are of high grade steel suitable to withstand high pressure. Body 10 and adapter plate 11 which are mounted face to face include a stepped axial bore 14.
  • the lower (front) end of the bore 14 is substantially closed, but includes fuel jets 17.
  • the bore 14 extends both into the body 10 and through the adapter plate 11.
  • the part of the bore 14 in the boly 10 comprises a front end 14A between an enlarged part of the bore 14 forming a gallery 18 and the fuel jet 17, and a second more rearward part 14B between the gallery 18 and a rear face 19 of the body 10.
  • the parts 14C,14D, 14E of the bore 14 in the adapter plate 11 are shown in the figure.
  • the diameter of the part 14C is greater than that of 14B.
  • the diameter of the part 14D is smaller than that of 14C.
  • the diameter of part 14E is considerably smaller than the diameter of the part 14D whereby a forward facing shoulder 33 is formed between the parts 14D and 14E.
  • An oblique bore 16 extends from the gallery 18 formed by an enlargement of the bore 14 to the rear face 19 of the body 10.
  • the rear end of oblique bore 16 aligns with a bore 21 formed through the adapter plate 11 and the rear end of this bore 21 align with a bore 22 through the housing 12.
  • the bores 16,21,22 form a fuel inlet passage 23.
  • valve member 24 Slidably mounted within the bore 14 is a valve member 24.
  • a first part 24A of the valve member 24 of diameter D1 extends between the gallery 18 and the front end of the bore 14. This part 24A is narrower than the corresponding part 14A of the bore 14 so as to allow fuel to pass from the gallery 18 to around the front end 26 of the valve member 24.
  • the front end 26 of the valve member 24 cooperates with a valve seat 27 formed at the front end or the bore 14, to provide a valve 28. Axial movement of the valve member 24 controls the flow of fuel from tl e bore 14 to the jets 17.
  • a second part 24B of the valve member 24 has an outer diameter D2 larger than the first part 24A but the same as the diameter of the corresponding part 14B of the bore 14 (with a suitable working clearance).
  • the rear end of part 24B of the valve member 24 is defined by a rearward facing shoulder 29 and the bore 14 includes a rearward facing shoulder 31 (between bore parts 14B and 14C) disposed at a distance a rearwardly of the shoulder 29 when the valve member 24 is in a position closing the valve 28 (ie as in the Figure and defined as a "first position").
  • this rearwardly facing shoulder 31 comprises the rear end 19 of body 10 and is provided by the greater diameter of the bore part 14C in the adapter plate 11 than the bore part 14B in the body 10.
  • valve member 24 Rearward of the shoulder 29, the valve member 24 forms a third narrower cylindrical part 24C of diameter D3.
  • the rear end of the part 24C is terminated by a coaxial spigot 24E extends rearwardly into engagement with a spring seat 34 which is urged forwardly by a coil spring 36.
  • a sleeve 37 Between the shoulder 29 and the shoulder 33 there is mounted a sleeve 37, the sleeve 37 having an inner diameter that it is a sliding fit with the part 24C of the valve member 24 and a stepped outer diameter, with a rearwardly directed shoulder 38 between a forward greater diameter part 37C of diameter D4 and a rearward part 37D of diameter D5.
  • the sleeve 37 also has rear, 37A, and front, 37B, ends.
  • the rear end 37A of the sleeve 37 is spaced from the shoulder 33 by a distance b .
  • the parts 37C and 370 are sliding fits with close clearance with the respective bore parts 14C,14D.
  • a side bore 39 interconnects the fuel inlet passage 23 and an annular slot 41 formed between the shoulder 38 and adjacent part of the bore 14, the relevant parts of the bore 14 and sleeve 37 being relieved to provide the slot 41.
  • the complete assembly is mounted to an engine and fuel is supplied to the fuel inlet passage 23 and thence to the jets 17 where it is injected into the engine.
  • valve 28 is closed by the spring 36 (ie the valve member 24 is in the first position as shown the Figure).
  • Fuel under pressure is supplied to the fuel inlet passage 23, and the pressure passes down that passage through the adapter plate 11 to the gallery 18.
  • the pressure of the fuel within the gallery 18, causes a first, rearward force to tend to retract the valve member 24 against the bias of the coiled compression spring.
  • the fluid pressure of the fuel is applied to an effective cross sectional area of the valve member 24 comprising an annular area of outer diameter D2, and inner diameter approximating to the diameter of the valve seat 27.
  • the valve member 24 will retract thereby opening the valve 28. It will normally continue to retract because although substantially to all of the forward faces of the valve member 24, thereby effectively increasing the rearwardly applied first force.
  • the pressure of fuel is also applied through the side bore 39 to the annular slot 41 and this produces a force which urges the sleeve 37 forwards so that the front end 37B of sleeve 37 engages the rearwardly facing shoulder 31 of the bore 14.
  • valve member 24 will continue to retract.
  • valve member 24 When the fuel pressure rises to a point sufficient to move the valve member 24 rearwardly from the second position, the valve member 24 will move towards a third Position in which the rear surface 37A of the sleeve 37 engages with the shoulder 33 of the adapter plate 11. The sleeve 37 is then effectively trapped between the valve member 24 and the adapter plate 11 thereby preventing further rearward movement of the valve member 24.
  • the present arrangement of the invention has a number of advantages.
  • the value of the second force is proportional to the area of the annulus having an inner diameter D5 and an outer diameter D4 and this can readily be adjusted during manufacture so as to be quite small.
  • the surfaces which finally stop the valve member in its rearward movement and which are therefore subject to wear comprise the relatively large areas of the opposite ends of the sleeve 37 acting between the shoulder 33 and the shoulder 29 of the valve member 24. The relatively large size of the surfaces reduces the wear on them.
  • the invention is not restricted to the details of the foregoing example. For example, it might be applied to 'other types of' injection nozzle. Also the adapter plate 11 could be part of the body 12.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
EP89309497A 1988-10-19 1989-09-19 Buse d'injection de combustible Withdrawn EP0365143A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8824478 1988-10-19
GB888824478A GB8824478D0 (en) 1988-10-19 1988-10-19 Fuel injection nozzle

Publications (1)

Publication Number Publication Date
EP0365143A1 true EP0365143A1 (fr) 1990-04-25

Family

ID=10645444

Family Applications (1)

Application Number Title Priority Date Filing Date
EP89309497A Withdrawn EP0365143A1 (fr) 1988-10-19 1989-09-19 Buse d'injection de combustible

Country Status (3)

Country Link
EP (1) EP0365143A1 (fr)
JP (1) JPH02256874A (fr)
GB (1) GB8824478D0 (fr)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0240693A1 (fr) * 1986-04-04 1987-10-14 Robert Bosch Gmbh Injecteur de combustible pour moteurs à combustion interne

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0240693A1 (fr) * 1986-04-04 1987-10-14 Robert Bosch Gmbh Injecteur de combustible pour moteurs à combustion interne

Also Published As

Publication number Publication date
GB8824478D0 (en) 1988-11-23
JPH02256874A (ja) 1990-10-17

Similar Documents

Publication Publication Date Title
US6601566B2 (en) Fuel injector with directly controlled dual concentric check and engine using same
JP2601977B2 (ja) 電磁燃料噴射弁
US6446613B1 (en) Two-stage pressure limiting valve
US4628957A (en) Pressure valve for fuel injection pump
EP0675282B1 (fr) Circuits de carburant
GB2279706A (en) Fuel injection pumping system
US6427664B1 (en) Pressure booster for a fuel injection system for internal combustion engines
US8136741B2 (en) Fuel injection device for an internal combustion engine using direct fuel injection
US4601269A (en) Fuel injection nozzle
JPH02149766A (ja) 燃料噴射ノズル
US6820594B2 (en) Valve for controlling a communication in a high-pressure fluid system, in particular in a fuel injection system for an internal combustion engine
EP0365143A1 (fr) Buse d'injection de combustible
EP1245822A2 (fr) Injecteur de carburant avec un limiteur de débit dans la soupape de commande
US6953157B2 (en) Fuel injection device for an internal combustion engine
EP3085947B1 (fr) Soupape de carburant pour un moteur à combustion interne à auto-allumage à deux temps de grande dimension
US4830285A (en) Fuel injection nozzle
GB2273134A (en) Delivery valve for a fuel injection pump.
US3237568A (en) Fuel injection pump with pneumatic damper
GB2030219A (en) Fuel injection nozzles
EP0890733B1 (fr) Soupape d'amortissement
EP0805271B1 (fr) Système d'injection de combustible
JP2890782B2 (ja) 燃料噴射ポンプの逆止弁
EP0939219A2 (fr) Injecteur à combustible
WO1992019857A1 (fr) Injecteur de carburant
JPS6235050A (ja) ガスで駆動されるジ−ゼルエンジンのための燃料噴射弁

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19890929

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES FR GB IT

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN

18W Application withdrawn

Withdrawal date: 19901115

R18W Application withdrawn (corrected)

Effective date: 19901115