Fuel injector

Information

  • Patent Grant
  • 6321999
  • Patent Number
    6,321,999
  • Date Filed
    Friday, May 14, 1999
    25 years ago
  • Date Issued
    Tuesday, November 27, 2001
    23 years ago
Abstract
A fuel injector comprises a valve needle spring biased towards a seating. The valve needle defines a thrust surface orientated such that the application of fuel under pressure thereto applies a force to the needle urging the needle away from the seating. A valve is provided to control the supply of fuel to the thrust surface.
Description




This invention relates to a fuel injector for use in supplying fuel under pressure to a combustion space of a compression ignition internal combustion engine. In particular the invention relates to a fuel injector of the type arranged to receive fuel from an associated fuel pump, for example a pump/injector or an arrangement in which a pump and injector are connected to one another by a high pressure pipe, the pump delivering fuel exclusively to the injector.




In a known pump/injector arrangement, the timing of fuel injection is controlled by controlling the fuel pressure within a control chamber which applies a force to a valve needle of the injector, urging the needle towards a seating. The fuel pressure within the control chamber is conveniently controlled by an electromagnetically actuator valve.




The use of such a control chamber in controlling the operation of the injector requires the provision of a number of additional bores or drillings, thus increasing the complexity of the injector.




According to the present invention there is provided a fuel injector comprising a valve needle spring biased into engagement with a seating to control fuel delivery, the valve needle including a thrust surface orientated such that the application of fuel under pressure thereto applies a force to the needle urging the needle away from the seating, and a valve controlling the application of fuel under pressure to the thrust surface.




The injector conveniently further comprises a fuel pump arranged to supply fuel to the thrust surface when the valve is open. Preferably, the injector further comprises a drain valve controlling communication between a pump chamber of the fuel pump and a fuel reservoir.




Such an injector is advantageous in that the provision of a control chamber is avoided thus the injector is of relatively simple construction.











The invention will further be described, by way of example, with reference to the accompanying drawings, in which like reference numerals are used to denote like parts, and in which:





FIG. 1

is a sectional view of part of an injector in accordance with an embodiment of the invention;





FIG. 2

is a sectional view illustrating a modification to the injector of

FIG. 1

; and





FIG. 3

is a diagrammatic view of part of the injector of FIG.


1


.











The injector illustrated in

FIG. 1

comprises a nozzle body


10


provided with a blind bore


12


within which a valve needle


14


is slidable. Adjacent the blind end of the bore


12


, a seating is formed with which an end part of the needle


14


is engageable to control the supply of fuel from the bore


12


to one or more outlet openings located downstream of the seating. The needle


14


is shaped to include a region which is of substantially the same diameter as the adjacent part of the bore


12


to form a substantially fluid-tight seal therewith and to guide the needle for sliding movement within the bore


12


. A lower part of the needle


14


is of reduced diameter and defines, with the bore


12


, a chamber


12




a


(see

FIG. 3

) from which fuel under pressure is able to flow past the seating, in use, to be injected into a combustion space of an associated engine. At the intersection of the upper, enlarged diameter portion of the needle


14


and the lower reduced diameter portion thereof, the valve needle


14


defines a thrust surface


14




a


which is exposed to the fuel pressure within the chamber


12




a.






The bore


12


is shaped to define an annular gallery


16


. The needle


14


is shaped to include flutes whereby fuel is able to flow from the annular gallery


16


to the chamber


12




a


. The annular gallery is supplied with fuel, in use, through an inlet passage


18


provided in the nozzle body


10


.




The upper surface of the nozzle body


10


abuts a first distance piece


20


which includes an axially extending through bore into which an upper end of the needle


14


extends, and a drilling


22


which communicates with the supply passage


18


of the nozzle body


10


. The first distance piece


20


abuts a spring housing


24


which includes a drilling


26


communicating with the drilling


22


. The spring housing


24


is further provided with a through bore including a region of relatively large diameter which defines a spring chamber


28


within which a helical compression spring


30


is located. The spring


30


engages a shim


32


located at the intersection of the spring chamber


28


with a reduced diameter portion of the through bore, the spring


30


further engaging a spring abutment member


34


which is carried by the upper end of the needle


14


. The spring


30


acts to bias the valve needle


14


into engagement with the seating. The spring chamber


28


communicates through a passage


36


with a low pressure drain reservoir.




The upper surface of the spring housing


24


engages a control valve housing


38


including a through bore


40


within which a control valve member


42


is slidable. The through bore


40


defines a seating with which an enlarged diameter portion of the valve member


42


is engageable to control the flow of fuel along a drilling


44


which extends from the upper surface of the control valve housing


38


to a portion of the lower surface of the valve housing


38


which communicates with the drilling


26


. The upper part of the control valve member


42


is of diameter substantially equal to that of the adjacent part of the bore


40


to form a substantially fluid-tight seal therewith. The lower part of the control valve member


42


also forms a good seal with the bore


40


, but as it is difficult to manufacture bores including regions of different diameter, the regions being concentric with one another, a small amount of leakage is likely between the lower part of the valve member


42


and the adjacent part of the bore


40


. Fuel escaping between the valve member


42


and the lower part of the bore


40


flows to the spring chamber


28


through the upper, small diameter part of the through bore of the spring housing


24


. In order to minimise the quantity of fuel flowing in this manner, when the control valve member


42


occupies a position in which the enlarged part thereof is spaced from its seating, the lower end of the control valve member


42


is arranged to engage, and form a substantially fluid-tight seal with the upper surface of the spring housing


24


.




The upper end of the control valve member


42


carries an armature


46


, the armature


46


being secured to the control valve member


42


by means of an internally screw-threaded member


48


. The armature


46


is moveable under the influence of a magnetic field generated, in use, by a first winding


50


of an actuator


52


located within an actuator housing


54


which abuts the upper surface of the control valve housing


38


. The actuator housing


54


includes a drilling


56


which communicates with the upper part of the drilling


44


.




The upper surface of the actuator housing


54


abuts a drain valve housing


58


which includes a through bore


60


within which a drain valve member


62


is slidable. The drain valve member


62


includes a region of enlarged diameter which is engageable with a seating to control the flow of fuel between a passage


64


which communicates with the drain reservoir and a passage


66


which communicates with a recess


68


formed in the upper surface of the drain valve housing


58


.




The recess


68


further communicates with a drilling


70


formed in a pump housing


72


which abuts the upper surface of the drain valve housing


58


. The pump housing


72


includes a plunger bore


74


within which a plunger


76


is reciprocable under the influence of a conventional cam and tappet arrangement (not shown).




The lower end of the drain valve member


62


carries an armature


78


, the armature


78


being secured to the drain valve member


62


by means of an internally screw-threaded member


80


. The armature


78


is moveable under the influence of a magnetic field generated, in use, by a second winding


82


forming part of the actuator


52


. The drain valve member


62


further carries a shim


84


, a spring


86


being located between the shim


84


and the member


48


. The spring


86


acts to bias the drain valve member


82


away from its seating and to bias the control valve member


42


away from its seating.




The various housings forming part of the injector are secured to the pump housing


72


by means of a cap nut


88


which engages a shoulder defined by the nozzle body


10


, the cap nut


88


being in screw-threaded engagement with external screw-thread formations formed on the pump housing


72


. The cap nut


88


and various housing parts of the injector together define a chamber with which the passage


36


and the passage


64


communicate, the chamber communicating with the low pressure reservoir through passages


90


formed in the cap nut


88


.




In use, with the plunger


76


occupying its innermost position and with the first and second windings


50


,


82


of the actuator


52


de-energized, the drain valve member


62


and control valve member


42


both occupy positions in which they are spaced from their respective seatings. Retraction of the plunger


76


under the action of a return spring (not shown) draws fuel from the low pressure fuel reservoir past the drain valve member


62


to charge the plunger bore


74


with fuel under relatively low pressure. Fuel continues to flow into the injector until the plunger


76


occupies its outermost position. Once the plunger


76


occupies its outermost position, subsequent inward movement of the plunger


76


displaces fuel back past the drain valve member


62


to the low pressure fuel reservoir.




When it is determined that pressurization of fuel should commence, the first and second windings


50


,


82


of the actuator


52


are energized resulting in movement of the control valve member


42


into engagement with its seating, and movement of the drain valve member


62


into engagement with its seating. As a result of the engagement of the drain valve member


62


with its seating, continued inward movement of the plunger


76


no longer displaces fuel to the lower pressure fuel reservoir, and instead the fuel present in the plunger bore


74


and in the passages in communication therewith is pressurised.




When the control valve is closed, the valve member


42


thereof is substantially pressure balanced so the increase in fuel pressure does not result in movement of the control valve member


42


or in commencement of injection.




When it is determined that injection should commence, the first winding


50


of the actuator


52


is de-energized thus permitting movement of the control valve member


42


away from the seating under the action of the spring


86


. The dimensions of the control valve member


42


are such that once movement of the valve member


42


away from its seating has commenced, the control valve member is no longer pressure balanced, and the fuel pressure acting upon the control valve member


42


applies a force assisting the spring


86


in moving the control valve member


42


in a downward direction. The movement of the control valve member


42


permits fuel under pressure to be supplied to the bore


12


of the nozzle body


10


, thus increasing the fuel pressure acting upon the thrust surfaces of the needle, and a point will be reached beyond which the fuel pressure acting upon the needle


14


is sufficient to cause movement of the needle


14


away from its seating against the action of the spring


30


. Once such movement has occurred, injection takes place.




During injection, a small amount of leakage of fuel between the control valve member


42


and bore


40


may occur, but this flow of fuel is limited by the seating of the lower end of the valve member


42


against the upper surface of the spring housing


24


.




In order to terminate injection, the second winding


82


of the actuator


52


is de-energized, and the drain valve member


62


moves under the influence of the spring


86


to lift the drain valve member


62


away from its seating, thus re-establishing communication between the plunger bore


74


and the low pressure drain reservoir. The fuel pressure within the plunger bore


74


and passages in communication therewith rapidly reduces, thus the fuel pressure acting upon the thrust surfaces


14




a


of the needle


14


rapidly falls, and the valve needle


14


moves under the action of the spring


30


into engagement with its seating, thus terminating the flow of fuel to the outlet apertures of the nozzle body


10


. After termination of injection, continued inward movement of the plunger


76


continues to displace fuel to the low pressure fuel reservoir until the plunger


76


reaches its innermost position. Once this position has been reached, the plunger


76


commences outward movement as described hereinbefore.




It will be appreciated that the use of the control valve and drain valve to control commencement of pressurization, commencement of injection and termination of injection permits accurate control of the injector. It will further be appreciated that as the provision of a control chamber is avoided, the injector is of relatively simple construction.





FIG. 2

illustrates a modification to the arrangement of FIG.


1


. In the modification of

FIG. 2

, the drain valve member


62


includes an enlarged diameter end region


62




a


which is engageable with a seating defined by the bore


60


to control fuel flow between the passage


66


and a chamber


60




a


defined by part of the bore


60


. The chamber


60




a


communicates through a passage


64




a


with a low pressure fuel reservoir. As the chamber


60




a


is at low pressure, the provision of additional passages in the drain valve housing to avoid the formation of a hydraulic lock preventing movement of the valve member


62


can be avoided.




Operation of the modification illustrated in

FIG. 2

is as described with reference to FIG.


1


.




Although the description hereinbefore is of a pump injector, it will be appreciated that the invention is also applicable to an arrangement in which the pump is located in a position remote from the injector, and is connected thereto by means of a high pressure pipe, the fuel pump supplying fuel exclusively to the injector.




In the description hereinbefore, the first winding


50


is energized at the same time as energization of the second winding


82


. It will be appreciated, however that the first winding


50


may be energized to close the control valve


42


at a stage in the operating cycle of the injector earlier than that described hereinbefore. For example, the control valve member


42


may be moved into engagement with its seating whilst the plunger


76


is being withdrawn from the plunger bore


74


, rather than awaiting commencement of pressurization.



Claims
  • 1. A fuel injector comprising a valve needle spring biased into engagement with a seating to control fuel delivery, the valve needle including a thrust surface orientated such that the application of fuel under pressure thereto applies a force to the needle urging the needle away from the seating, and a valve, comprising a valve member, for controlling the supply of fuel under pressure to the thrust surface, the valve member including an enlarged diameter region which is engageable with a further seating to control fuel flow along a first passage, wherein the enlarged diameter region includes an end face adapted for engagement with a surface to close a second passage when the enlarged diameter region of the valve member is spaced from its seating.
  • 2. A fuel injector as claimed in claim 1, wherein the valve is electromagnetically controlled.
  • 3. A fuel injector as claimed in claim 1, further comprising a fuel pump arranged to supply fuel under pressure to the thrust surface when the valve is open.
  • 4. A fuel injector as claimed in claim 3, further comprising a drain valve controlling communication between a pump chamber of the pump and a fuel reservoir.
  • 5. The fuel injector as claimed in claim 1, wherein the valve is housed within a valve housing having an upper surface and a lower surface, the first passage extending from the upper surface of the valve housing to the lower surface of the valve housing to permit fuel to be supplied to the thrust surface of the valve needle when the valve member is moved away from the further seating.
  • 6. The fuel injector as claimed in claim 3, wherein the valve member is movable within a bore, the second passage being defined between the valve member and the bore.
  • 7. The fuel injector as claimed in claim 6, wherein the end of the valve needle is adapted for engagement with a surface of a further housing defining a chamber for housing a compression spring which serves to urge the valve needle into engagement with the seating.
Priority Claims (1)
Number Date Country Kind
9812889 Jun 1998 GB
US Referenced Citations (7)
Number Name Date Kind
5282574 Koch Feb 1994
5463996 Maley et al. Nov 1995
5538187 Mueller et al. Jul 1996
5628293 Gibson et al. May 1997
5673669 Maley et al. Oct 1997
5697342 Anderson et al. Dec 1997
6067955 Boecking May 2000
Foreign Referenced Citations (1)
Number Date Country
19512270 Sep 1996 DE