Fuel injection valve for a combustion engine

Information

  • Patent Grant
  • 6565017
  • Patent Number
    6,565,017
  • Date Filed
    Thursday, July 6, 2000
    24 years ago
  • Date Issued
    Tuesday, May 20, 2003
    21 years ago
Abstract
Located between the frustoconical needle tip and the cylindrical needle shank of a nozzle needle of a fuel injection valve is a frustoconical needle portion, into which is introduced a peripheral groove. Through this kind of arrangement damping is capable of being set, depending on the position of the groove, during the axial movement of the nozzle needle.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The invention relates to a fuel injection valve with a nozzle needle which is guided in a central guide bore of a nozzle body and has a peripheral sealing region having a sealing edge which, together with the valve seat of the nozzle body, forms a valve which is opened or closed, depending on the position of the nozzle needle, and controls the inflow of fuel to at least one injection hole in the nozzle tip of the nozzle body.




In injection systems, fuel is injected under high pressure into the combustion space of an internal combustion engine via a fuel injection valve.




2. Description of the Related Art




WO 96/19661 discloses a fuel injection valve having a nozzle body with a central guide bore, in which a nozzle needle is guided. The valve opens as a result of the axial movement of the nozzle needle, said valve being formed by the sealing edge of the nozzle needle and the conical valve seat at the nozzle tip of the nozzle body. The valve thus controls the flow of fuel to the injection holes which are introduced into the nozzle tip. A step in the form of a peripheral groove is introduced below the sealing edge of the nozzle needle, in order to prevent the change in the valve seat diameter which is caused by wear.




When the valve closes, the sealing edge of the nozzle needle strikes the conical valve seat sharply, thus giving rise to pronounced mechanical stress on the nozzle body which may lead to a curtailed service life of the latter.




SUMMARY OF THE INVENTION




The object of the invention is to reduce the mechanical stress on the nozzle body which occurs during the closing of the valve.




The object of the invention is achieved by means of the features of the independent patent claim.




Advantageous embodiments of the invention are specified in the dependent claims.




In the invention, the nozzle needle has, between its frustoconical nozzle needle tip and its cylindrical needle shank, a frustoconically designed body portion which, at its transition to the nozzle needle tip, has a sealing edge which, together with the conical valve seat of the nozzle tip of a nozzle body, forms a valve. The conical valve seat forms, with the frustoconical body portion of the nozzle needle, an angle the sides of which meet at the sealing edge and which forms a small angle in the region of a few degrees. During the closing of the valve, that is to say when the sealing edge strikes the conical valve seat, the fuel in the gap between the body portion of the nozzle needle and the conical valve seat is pressed out, with the result that the closing action is damped.




The peripheral gap between the valve seat and the body portion is partially enlarged by means of a recess in the nozzle needle or in the nozzle body, with the result that the effect of damping the closing action can be set. The recess is designed as a peripheral groove in the nozzle needle or in the nozzle body. The damping effect can be set, depending on the position of the recess, that is to say on the axial position of the recess and on the size of the recess.




In one embodiment, the peripheral groove is made directly at the sealing edge of the nozzle needle, with the result that, in addition to the damping effect, the valve seat diameter does not change, or changes only insignificantly, when the nozzle needle undergoes wear at the sealing edge.




In a further embodiment, a frustoconical body portion of the nozzle needle is arranged between the peripheral groove and the sealing edge, as a result of which the damping effect can be set, depending on the axial length of this body portion.




In a further embodiment, the peripheral groove has a first and a second groove portion which is arranged in the direction of the sealing edge or of the shank bore, the first groove portion being of cylindrical design. This makes it possible to manufacture the groove in a simple way within the respective body portion of the nozzle needle. Additionally, when the cylindrical second groove portion is arranged directly at the sealing edge, the effect of wear on the valve seat diameter is only slight.




Furthermore, the recess is introduced as a peripheral groove into the inner wall of the valve seat of the nozzle body.




In a further embodiment, a further peripheral groove is introduced into the frustoconical nozzle needle tip and serves for guiding the nozzle needle radially during the opening and closing of the valve.




The nozzle body is advantageously designed in the form of a seat hole nozzle, the injection holes of which are located in the region of the conical valve seat.




Other features which are considered as characteristic for the invention are set forth in the appended claims.




Although the invention is illustrated and described herein as embodied in a fuel injection valve for an internal combustion engine, it is nevertheless not intended to be limited to the details shown, since various modifications and structural changes may be made therein without departing from the spirit of the invention and within the scope and range of equivalents of the claims.




The construction and method of operation of the invention, however, together with additional objects and advantages thereof will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings.











BRIEF DESCRIPTION OF THE DRAWING





FIG. 1

shows a longitudinal section through the nozzle body of a fuel injection valve with a nozzle needle,





FIG. 2

shows a further exemplary embodiment of the nozzle body and of the nozzle needle,





FIG. 3

shows a longitudinal section through part of the nozzle body of a fuel injection valve with a nozzle needle,





FIG. 4

shows a further exemplary embodiment of the nozzle body and of the nozzle needle,





FIG. 5

shows a further exemplary embodiment of the nozzle body and of the nozzle needle.











DESCRIPTION OF THE PREFERRED EMBODIMENT





FIG. 1

shows, as prior art, a longitudinal section through a fuel injection valve with an essentially rotationally symmetric nozzle body


5


, in the central guide bore


54


of which is guided axially a rotationally symmetric nozzle needle


1


. Starting from the orifice of the guide bore


54


in the end face


58


of the nozzle body


5


, the guide bore


54


merges into a radially widening pressure chamber


51


which thereupon narrows again, a shank bore


57


and a conically tapering valve seat


55


with a valve seat angle a


3


which terminates in a pocket


56


. An inflow duct


59


is arranged laterally in relation to the guide bore


54


and opens laterally into the pressure chamber


51


. At least one injection hole


9


is introduced into the tip of the nozzle body in the region of the valve seat


55


.




The nozzle needle


1


is subdivided axially into various cylindrical or frustoconical body portions, the diameters of which decrease from the rear side


11


of the nozzle needle


1


in the direction of the flattened needle tip


45


. The nozzle needle


1


is subdivided, from its rear side


11


in the direction of its nozzle needle tip, into




a cylindrical guide shank


12


which is guided in the guide bore


54


and has approximately the diameter of the guide bore


54


,




a frustoconical thrust shoulder


13


level with the pressure chamber


51


,




a cylindrical needle shank


15


level with the shank bore


57


of the nozzle body


5


, in another embodiment the needle shank


15


being capable of having a noncylindrical cross section, at least in part of its length, for example being in the shape of a uniform polygon,




a frustoconical needle portion


20


,


25


with a first frustoconical angle a


1


, and




a frustoconical needle tip


45


having a flattened tip, with a second frustoconical angle a


2


, which is larger than the first frustoconical angle a


1


.




The transition between the needle portion


20


,


25


and the needle tip


45


forms a peripheral edge


27


, referred to below as a sealing edge


27


, which, together with the conical valve seat


55


, forms a valve


27


,


55


which, depending on the axial position of the nozzle needle


1


in the nozzle body


5


, controls the flow of fuel to the injection holes


9


which are arranged below the sealing edge


27


in the direction of the needle tip


45


.




The fuel injection valve functions as follows:




The nozzle needle


1


is subjected on its rear side


11


to a force which is aimed in the direction of the needle tip


45


. The force may be transmitted to the rear side


11


of the nozzle needle


1


directly by an actuator, for example a piezoelectric or electromagnetic actuator, or indirectly via a hydraulic servovalve. Fuel flows via the inflow duct


59


, the pressure chamber


51


and the shank bore


57


and, depending on the valve position of the valve


27


,


55


, is injected through the injection holes


9


into the combustion chamber of an internal combustion engine. The flow of fuel to the injection holes


9


is controlled, depending on the axial position of the nozzle needle


1


. The movement of the nozzle needle


1


and therefore its position depend essentially on the fuel pressure in the pressure chamber


51


and on the force acting on the rear side


11


of the nozzle needle


1


.




During the closing operation of the valve


27


,


55


, that is to say during the movement of the nozzle needle


1


axially in the direction of the tip of the nozzle body


5


, the sealing edge


27


butts onto the conical valve seat


55


, with the result that the valve seat


55


undergoes wear (seat wear). The seat wear depends on the intensity with which the sealing edge


27


strikes the valve seat


55


and on the shaping of the sealing region


28


which is formed by the sealing edge


27


, the portion of the nozzle tip


45


near the sealing edge


27


and the valve seat


55


. When the nozzle needle


1


strikes the valve seat


55


, the nozzle body


5


is deformed elastically, so as to give rise to the dynamic sealing region


28


which serves for distributing the dynamic force arising during impact to the valve seat


55


uniformly over a large area, thus resulting in a lower load per unit area in the material.




The angle difference a (see

FIG. 2

) between the valve seat angle a


3


and the second frustoconical angle a


2


is small, and it is at most a few degrees and preferably in the range between 0.15 and 5°. Due to the small angle difference a, shortly before the sealing edge


27


strikes the valve seat


55


the fuel is pressed out of the needle portion


20


,


25


and the valve seat


55


, thus leading to a damping of the closing movement, with the result that the force with which the sealing edge


27


strikes the valve seat


55


and therefore the wear are reduced.





FIGS. 2

to


5


illustrate various exemplary embodiments of that part of the fuel injection valve from

FIG. 1

which extends from the shank bore


57


to the tip of the nozzle body


5


, together with different embodiments of the nozzle needle


1


and of the nozzle body


5


. Functionally identical body portions have been given the same reference symbols.




In contrast to

FIG. 1

, in

FIG. 2

a peripheral groove


33


is introduced into the needle portion


20


,


25


which is thereby subdivided into a first and a second needle portion


20


,


25


in the direction of the sealing edge


27


or of the needle shank


15


. The damping, referred to in

FIG. 1

, of the closing movement is capable of being set by means of the groove


33


and of thereby being adapted to customer-specific requirements.




The damping depends on:




the angle difference a,




the axial position of the groove


33


in the needle portion


20


,


25


,




the volume which the fuel occupies in the groove


33


,




the maximum clearance between the wall of the groove


33


and the surface of the valve seat


55


, and




the shape of the groove.




During the closing movement, due to the small angle difference a, shortly before the sealing edge


27


strikes the valve seat


55


the fuel is pressed out of the damping gap between the needle portion


20


,


25


and the valve seat


55


, while, in addition, due to the formation of the groove


33


, pressure waves and resonances occur in the damping gap, which, depending on




the angle difference a,




the closing speed of the nozzle needle


1


,




the fuel pressure,




the axial position of the groove


33


in the needle portion


20


,


25


,




the volume which the fuel occupies in the groove


33


,




the maximum clearance between the wall of the groove


33


and the surface of the valve seat


55


, and




the shape of the groove


33


, advantageously lead to a superproportional intensification or attenuation of the damping of the closing movement.




In contrast to

FIG. 2

, in

FIG. 3

the peripheral groove


33


is introduced into the needle portion


20


directly at the sealing edge


27


, as a result of which, when wear occurs, the valve seat diameter changes only slightly, or does not change at all, depending on the shape of the groove


33


.




In a further exemplary embodiment, the groove


33


is introduced into the needle portion


25


directly at the transition to the needle shank


15


, as a result of which the effective axial length of the needle portion


25


and therefore of the damping gap is shortened and damping can thus be set in a defined manner.




Furthermore, introducing a groove


33


into the needle portion


20


,


25


of the nozzle needle


1


in the way described in the previous figures brings about a radial stabilization of the nozzle needle


1


, since the fuel is distributed quickly and uniformly in the groove


33


and generates a radial stabilizing force on the nozzle needle


1


.




The groove


33


described in the previous figures is preferably subdivided into a first, frustoconical groove portion


35


and a second, cylindrical groove portion


40


which are arranged respectively in the direction of the needle shank


15


and of the needle tip


45


. When the groove


33


is arranged with its second, cylindrical groove portion


40


directly below the sealing edge


27


(see FIG.


3


), a valve seat diameter independent of wear is advantageously obtained.




In contrast to

FIG. 2

, in

FIG. 4

a further peripheral groove


43


is introduced into the frustoconical needle tip


30


,


45


and subdivides the needle tip into a first and a second body portion


30


,


45


.




The axes


90


of the injection holes


9


open into the further groove


43


when the valve


27


,


55


is closed and preferably also when the valve


27


,


55


is fully open with a maximum deflection of the nozzle needle


1


.




Preferably, the edge


91


, located in the direction of the nozzle tip


45


, of that orifice of the injection hole


9


which is located on the inside of the nozzle body


5


is arranged level with the second groove portion


40


when the nozzle needle


1


is in its closing position, preferably also when the nozzle needle


1


has maximum deflection.




During the opening of the nozzle needle


1


, pressure compensation takes place at the further groove


43


of the nozzle needle


1


, and, due to the fuel pressure and the flow of fuel toward the nozzle needle


1


, a force directed radially to the longitudinal axis


10


of the latter is exerted, which counteracts a radial deviation of the nozzle needle


1


, with the result that the nozzle needle


1


is radially stabilized and centered in the middle.




The introduction of two peripheral grooves


33


,


43


into the nozzle needle


1


results in mutually intensifying combination effects with regard to the radial stabilization of the nozzle needle


1


during the opening and closing of the latter.




In contrast to

FIG. 1

, in

FIG. 5

a peripheral wall groove


34


is introduced level with the needle portion


20


,


25


and has the same functionality as the groove


33


described in the previous figures. Depending on the manufacturing methods used, the manufacturing costs can thereby be reduced.




The maximum clearance, preferred in the exemplary embodiments described in the previous figures, between the wall of the groove


33


and the inner wall of the nozzle body


5


or between the wall of the wall groove


34


and the needle portion


20


,


25


is in the range of 0.01 to 0.1 mm.



Claims
  • 1. A fuel injection valve, comprising:a seat hole nozzle formed with a central guide bore, a conical valve seat, and a fuel injection hole formed in said conical valve seat; a nozzle needle having a needle shank guided in said central guide bore of said seat hole nozzle, and a frustoconical needle portion having a peripheral sealing region with a sealing edge defining, together with said valve seat of said seat hole nozzle, a valve to be opened or closed in dependence on a position of said nozzle needle, for controlling a flow of fuel to said fuel injection hole; and said nozzle needle and an inner wall of said seat hole nozzle forming a gap therebetween, and one of said seat hole nozzle and said nozzle needle having a recess formed therein in the region of said frustoconical needle portion within said conical valve seat axially between said sealing edge and said needle shank for enlarging said gap.
  • 2. The fuel injection valve according to claim 1, wherein said recess is a circumferential groove formed in said nozzle needle.
  • 3. The fuel injection valve according to claim 2, wherein said circumferential groove is directly adjacent said sealing edge.
  • 4. The fuel injection valve according to claim 2, wherein said frustoconical needle portion has a frustoconical first needle portion between said circumferential groove and said sealing edge.
  • 5. The fuel injection valve according to claim 4, wherein said frustoconical needle portion has a frustoconical second needle portion between said circumferential groove and said needle shank.
  • 6. The fuel injection valve according to claim 2, wherein said frustoconical needle portion is formed between said circumferential groove and said needle shank.
  • 7. The fuel injection valve according to claim 2, wherein said circumferential groove has a substantially cylindrical first groove portion in a vicinity of said sealing edge and a second groove portion remotely of said sealing edge.
  • 8. The fuel injection valve according to claim 1, wherein said recess is a circumferential groove formed in said inner wall of said seat hole nozzle.
  • 9. The fuel injection valve according to claim 1, wherein said nozzle needle is formed with a peripheral guide groove between said needle tip and said sealing edge.
Priority Claims (1)
Number Date Country Kind
199 31 891 Jul 1999 DE
US Referenced Citations (8)
Number Name Date Kind
1952816 Mock Mar 1934 A
4153205 Parrish, Jr. May 1979 A
4470548 Ushimura Sep 1984 A
4974565 Hashimoto et al. Dec 1990 A
5163621 Kato et al. Nov 1992 A
5580000 Kiuchi et al. Dec 1996 A
5890660 Stevens Apr 1999 A
6047905 Honda et al. Apr 2000 A
Non-Patent Literature Citations (1)
Entry
Published International Application No. 96/19661, dated Jun. 27, 1996.