Fuel injection valve

Information

  • Patent Grant
  • 6745993
  • Patent Number
    6,745,993
  • Date Filed
    Wednesday, July 24, 2002
    22 years ago
  • Date Issued
    Tuesday, June 8, 2004
    20 years ago
Abstract
A fuel injector, such as a fuel injector for fuel injection systems in internal combustion engines, includes a valve needle, the valve-closure member of which cooperates with a valve seat surface to form a sealing seat, and includes an armature engaging with the valve needle, the armature being arranged on the valve needle in an axially movable manner and being damped by a damping element including an elastomer. A ring space is formed between damping element and the valve needle, which is filled with fuel, the ring space being in contact with a throttle gap.
Description




FIELD OF THE INVENTION




The present invention is based on a fuel injector of the type set forth in the main claim.




BACKGROUND INFORMATION




A fuel injector is referred to in U.S. Pat. No. 4,766,405, having a valve-closure member, connected to a valve needle, which acts together with a valve seat surface formed on a valve seat element to form a sealing seat. A magnetic coil is provided for electromagnetically actuating the fuel injector, the magnetic coil acting together with an armature which is connected to the valve needle by force-locking. Around the armature and the valve needle an additional cylindrical mass is provided, which is connected to the armature via an elastomeric layer.




It is believed that a disadvantage with this fuel injector may include a costly construction method with an additional component. In addition, the large surface elastomer ring is unfavorable for the pattern of the magnetic field and may hinder the closing of the field lines, and thus the achievement of great attractive forces during the opening movement of the fuel injector.




A specific embodiment of a fuel injector is also referred to in the above document in which, for damping and debouncing, a further cylindrical mass is provided around the armature and the valve needle, which is hemmed in and held in its position by two elastomeric rings. When the valve needle strikes the valve seat, this second mass may move relatively to the armature and the valve needle and prevent bouncing of the valve needle.




It is believed that a disadvantage of this specific embodiment may include an additional cost and requirement for space. Also, the armature is not decoupled, whereby its impulse on the valve needle may increase the tendency to bouncing.




A fuel injector having a valve needle and an armature is referred to in U.S. Pat. No. 5,299,776, in which the armature is movably guided on the valve needle, and the movement of which in the lift direction of the valve needle is limited by a first stop and, opposite to the lift direction, by a second stop. The play in the movement of the armature in the axial direction, fixed by the two stops, leads within certain limits to a decoupling of the inert mass of the valve needle as well as the inert mass of the armature. Within certain limits, this counteracts the bouncing back of the valve needle from the valve seat surface when the fuel injector is closed. However, since the axial position of the armature with respect to the valve needle is totally undefined, due to the free movement of the armature, bounces may be avoided to only a limited extent. In particular, with regard to the method of construction of the fuel injector referred to in the above document, what is not avoided is that the armature strikes the stop facing the valve-closure member during a closing movement of the fuel injector and transfers its linear momentum to the valve needle. This impact-like transfer of linear momentum may cause additional bounces of the valve-closure member.




Furthermore, the armature guided on the valve needle may be fastened by an elastomeric ring in a position in which it is movably clamped. To do this, the armature may be held between two flanges welded to the valve needle, there being an elastomeric ring between the armature and the lower flange. With this arrangement, however, a borehole through the armature may be necessary for the supply of fuel to the sealing seat. The boring through the armature is made close to the valve needle, the opening of the boring facing the valve seat being partially covered by the elastomeric ring. Thereby a nonuniform compression of the elastomeric ring arises, and the bore edges finally lead to the destruction of the elastomeric ring by the pressure of the edges. Additionally, this may cause excitation of vibrations of the unsupported elastomeric ring, which may also contribute to the trouble. caused by the bore edges. This may occur, for example, at low temperatures, when the elastomer converts into a stiff condition.




SUMMARY OF THE INVENTION




By contrast, an exemplary fuel injector according to the present invention may have the advantage that the armature and the valve needle are damped by a fluid damper that is formed between the armature and the valve needle by the collaboration of an elastomeric ring and a fluid-filled chamber. This may stop armature bounces from the lower armature as well as effectively damp valve needle bounces from the sealing seat.




It is believed that the damping action of the damping space between valve needle and armature wall into which fuel is squeezed from the annular space during the closing movement is an advantage.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

illustrates a schematic section through a fuel injector having armature debouncing.





FIG. 2

is an enlarged sectional view of an exemplary fuel injector according to the present invention.





FIG. 3

is an enlarged sectional view of a second exemplary embodiment of the fuel injector according to the present invention.





FIG. 4

is an enlarged sectional view of a third exemplary embodiment of the fuel injector according to the present invention.











DETAILED DESCRIPTION




Before exemplary embodiments of a fuel injector


1


according to the present invention are described more precisely with reference to

FIGS. 2 through 4

, to better understand the invention, a structurally similar fuel injector, apart from the measures according to the present invention, as it exists in the related art, shall be briefly explained with the aid of FIG.


1


.




Fuel injector


1


is designed in the form of an injector for fuel-injection systems of mixture-compressing internal combustion engines with externally supplied ignition. Fuel injector


1


may be suitable for directly injecting fuel into a combustion chamber (not illustrated) of an internal combustion engine.




Fuel injector


1


includes a nozzle body


2


, in which a valve needle


3


is positioned. Valve needle


3


is connected in operative connection to a valve-closure member


4


that cooperates with a valve-seat surface


6


, arranged on a valve-seat member


5


, to form a sealing seat. Fuel injector


1


in the embodiment shown in

FIG. 1

is an inwardly opening fuel injector


1


, having a spray-discharge opening


7


. Nozzle body


2


is sealed from external pole


9


of a magnetic coil


10


by a seal


8


. Magnetic coil


10


is encapsulated in a coil housing


11


and wound on a bobbin


12


which lies adjacent to an internal pole


13


of magnetic coil


10


. Internal pole


13


and external pole


9


are separated from each other by a constriction


26


and are connected to each other by a non-ferromagnetic connecting part


29


. Magnetic coil


10


is energized via an electric line


19


by an electric current, which may be supplied via a plug-in contact


17


. Plug-in contact


17


is enclosed in a plastic jacket


18


, which may be sprayed onto internal pole


13


.




Valve needle


3


is guided in a valve needle guide


14


, which is designed as a disk. A paired adjustment disk


15


adjusts the lift. An armature


20


is on the other side of adjustment disk


15


. It is connected by force-locking to valve needle


3


via a first flange


21


, and valve needle


3


is connected to first flange


21


by a welded seam


22


. Braced against valve needle


21


is a return spring


23


which, in the embodiment shown in

FIG. 1

, is prestressed by a sleeve


24


. Fuel channels


30




a


through


30




c


run through valve needle guide


14


, armature


20


and valve seat member


5


, which conduct the fuel, supplied via central fuel supply


16


and filtered by a filter element


25


, to spray-discharge opening


7


. Fuel injector


1


is sealed by a seal


28


from a fuel line (not shown).




On the spray-discharge side of armature


20


is positioned a ring-shaped damping element


32


, made of an elastomeric material. Damping element


32


rests on second flange


31


, which is connected by force-locking to valve needle


3


via a welded seam


33


.




During manufacturing of the component including armature


20


and valve needle


3


, first flange


21


is welded to valve needle


3


, armature


20


and damping element


32


are slipped on, and subsequently second flange


31


is pressed on damping element


32


under pressure and also welded to valve needle


3


. In this manner, armature


20


has only little, strongly damped play between first flange


21


and damping element


32


.




In the neutral position of fuel injector


1


, return spring


23


acts upon armature


20


counter to its lift direction so that valve-closure member


4


is retained in sealing contact against valve seat


6


. Upon excitation of magnetic coil


10


, a magnetic field is generated, which moves armature


20


in the lift direction, counter to the spring force of return spring


23


, the lift being predefined by a working gap


27


existing in the neutral position between internal pole


13


and armature


20


. Armature


20


also carries along in the lift direction flange


21


, which is welded to valve needle


3


. Valve-closure member


4


, being connected to valve needle


3


, lifts off from valve seat surface


6


, and fuel guided via fuel channels


30




a


through


30




c


is sprayed off through spray-discharge opening


7


.




When the coil current is switched off, after sufficient decay of the magnetic,field, armature


20


falls away from internal pole


13


due to the pressure of return spring


23


, whereupon flange


21


, being connected to valve needle


3


, moves in a direction counter to the lift, thereby causing valve needle


3


to move in the same direction in which valve-closing body


4


sets down upon valve seat surface


6


and fuel injector


1


is closed.




In this phase the bounces occur, which are caused by armature


20


falling off from internal pole


13


in the spray-discharge direction during the closing process of fuel injector


1


, and by valve needle


3


, or rather valve-closure body


4


setting down upon the sealing seat.




In an extracted sectional illustration,

FIG. 2

shows a section of fuel injector


1


corresponding to the section denoted by II in FIG,


1


. Corresponding components are designated by corresponding reference numerals.




As compared to fuel injector


1


according to the related art, described in

FIG. 1

, the present first exemplary embodiment of a fuel injector


1


according to the present invention, as shown in

FIG. 2

, has an inner circular ring projection


34


on spray-discharge side


42


of armature


20


, and a funnel-shaped recess


35


. Fuel channel


30




a


opens out on funnel-shaped recess


35


. Circular ring-shaped projection


34


, which is penetrated by valve needle


3


in a central recess


38


of armature


20


, is supported on damping element


32


, and thus on second flange


31


, which is integrally connected to valve needle


3


via welding seam


33


. Second flange


31


has a ring-shaped depression


36


in which damping element


32


is arranged, and which is covered, as if by a lid, by circular ring-shaped projection


34


. In this context, circular ring-shaped projection


34


lies on damping element


32


. Ring-shaped depression


36


has an inner edge


43


facing valve needle


3


, and a radially outer edge


44


, which is axially higher than inner edge


43


. Thus, circular ring-shaped projection


34


closes off ring-shaped depression


36


toward the outside, while in the neutral position of fuel injector


1


an axial gap remains between edge


43


and projection


34


. In ring-shaped depression


36


an annular space


37


is formed, which is radially limited by valve needle


3


and damping element


32


. Annular space


37


is filled with fuel that flows into annular space


37


via central recess


38


of armature


20


, which acts as a throttle.




During closing of fuel injector


1


, as soon as valve-closure member sets down upon valve seat surface


6


, armature


20


, which is positioned movably on valve needle


3


, swings through. Usually, this swinging through leads to a renewed motion of armature


20


in the lift direction, which may bring on a brief, undesired further opening procedure of fuel injector


1


, since thereby, valve needle


3


is also moved once more in the lift direction. This is prevented in two ways by the fuel contained in ring space


37


, as well as by damping element


32


.




The fuel in ring space


37


is compressed by the at first countercurrent motions of armature


20


and valve needle


3


. Armature


20


may swing through only to the point at which gap


45


, between edge


43


and projection


34


of armature


20


, is closed. Due to the closed form of ring space


37


, the fuel may leave ring space


37


only through throttle gap


39


, acting like a throttle between an inner wall


40


of armature


20


and valve needle


3


. Thus, the motion of armature


20


and the swing-back motion of valve needle


3


are damped. Furthermore, the swing-back motion of armature


20


may be effectively damped by damping element


32


, which is positioned in ring-shaped depression


36


, since damping element


32


converts a major portion of the energy of motion of armature


20


into energy of deformation of damping element


32


, and because an underpressure is created in ring space


37


during the swing-back motion.




In the same view as in

FIG. 2

,

FIG. 3

shows a second exemplary embodiment of fuel injector


1


according to the present invention.




In this exemplary embodiment, second flange


31


is furnished with a deeper ring-shaped depression


36


than in the previous exemplary embodiment shown in FIG.


2


. Outer edge


44


of second flange


31


is raised, while inner edge


43


is omitted. A lower end


46


of projection


34


of armature


20


is formed so that damping element


32


is arranged radially between thin end


46


of projection


34


and edge


44


of second flange


31


, an axial gap


45


being formed between lower end


46


of projection


34


and the second flange. At equal outer diameter of second flange


31


to that of the exemplary embodiment shown in

FIG. 2

, the effective damping volume, which is arranged below damping element


32


, is thereby increased.




In the case of the second exemplary embodiment of fuel injector


1


according to the present invention, it may not be important to have accurately fitting and exact manufacturing or assembly of the individual components. This may make manufacturing and assembly of the component parts more cost-effective.




In the mode of operation, the second exemplary embodiment of fuel injector


1


according to the present invention is similar to the first exemplary embodiment shown in FIG.


2


. When the fuel injector


1


is closed, armature


20


swings through, whereby damping element


32


as well as the fuel in ring space


37


are compressed by projection


34


of armature


20


. Armature


20


may only swing through until lower end


46


of projection


34


strikes second flange


31


. Damping element


32


absorbs the greatest part of the energy of motion of armature


20


, while the fuel displaced from ring space


37


flows out via throttle gap


39


between valve needle


3


and inner wall


40


of armature


20


, whereby the swinging through of valve needle


3


is braked and valve-closing member


4


is prevented from once again briefly lifting off from valve seat surface


6


.




A third exemplary embodiment of fuel injector


1


according to the present invention is shown in FIG.


4


. The exemplary embodiment of

FIG. 3

differs little in its construction from the two previous exemplary embodiments of

FIGS. 2 and 3

. Instead of circular ring-shaped projection


34


of armature


20


, a cap-shaped cover shell


41


, on which projection


34


of armature


20


is supported, forms the ring-shaped depression


36


. In the third exemplary embodiment shown in

FIG. 4

, ring-shaped depression


36


opens in the downstream direction of the fuel flow. Second flange


31


is flat and closes ring-shaped depression


36


like a lid in the downstream direction. Cover shell


41


may be easy to manufacture as a separate part, independently of armature


20


.




Damping element


32


is positioned in ring-shaped depression


36


of cover shell


41


, and ring space


37


is in contact with throttle gap


39


, as in the preceding exemplary embodiments shown in

FIGS. 2 and 3

, between inner wall


40


of armature


20


and valve needle


3


. The component parts of the third exemplary embodiment of

FIG. 4

may be easy to manufacture, and armature


20


may be configured so that fuel channel


30




a


, inserted into armature


20


, may be processed more easily and deburred at its downstream end.




At the closing of fuel injector


1


, armature


20


swings through again in the spray-discharge direction, whereby cap-shaped cover shell


41


is pushed over second flange


31


, since the outer diameter of flange


31


is equivalent to the inner diameter of the mantle region of cover shell


41


(e.g., is minimally smaller). In the exemplary embodiment shown in

FIG. 4

, advantageously gap


45


may not have to be limited by a special geometrical arrangement like the exemplary embodiments described above, but may be equal to the height of ring space


37


. Damping element


32


, lying between cover shell


41


and second flange


31


, as well as the fuel present in ring space


37


are compressed by the movement, and in this context, damping element,


32


absorbs the energy of motion of armature


20


, while the fuel from ring space


37


is displaced into throttle gap


39


between valve needle


3


and inner wall


40


of armature


20


. The swinging through of valve needle


3


is damped by the viscosity of the fuel and/or the throttle effect of throttle gap


39


.




The present invention is not limited to the exemplary embodiments shown, and is also suitable, for example, for flat armatures or for any design of fuel injector.



Claims
  • 1. A fuel injector, comprising:a valve needle including a valve-closure member, the valve-closure member cooperating with a valve seat surface to form a sealing seat; a damping element made of an elastomer; a flange including a ring-shaped depression on which the damping element is arranged, the ring-shaped depression forming a ring space between the damping element and the valve needle, the ring-space being in contact with a throttle gap at the valve needle; and an armature engaging with the valve needle, the armature being arranged on the valve needle in an axially movable manner and damped by the damping element, and the damping element being arranged between the flange and the armature; wherein the ring-space is configured to receive fuel.
  • 2. The fuel injector according to claim 1, wherein the throttle gap is formed between the valve needle and an inner wall of the armature.
  • 3. The fuel injector according to claim 1, wherein the armature includes a fuel channel penetrating the armature and a funnel-shaped recess on a discharge side of the armature, and wherein the fuel channel discharges into the funnel-shaped recess.
  • 4. The fuel injector according to claim 1, wherein an inner edge of the flange facing the valve needle is lower than an outer edge of the flange.
  • 5. The fuel injector according to claim 4, wherein a gap is formed between the inner edge of the flange and a projection of the armature.
  • 6. The fuel injector according to claim 5, wherein the gap formed between the inner edge and the projection of the armature is in contact with the throttle gap.
  • 7. The fuel injector according to claim 1, wherein a circular ring-shaped projection of the armature covers the ring-shaped depression.
  • 8. The fuel injector according to claim 7, wherein the circular ring-shaped projection of the armature is arranged in the ring-shaped depression and lies against the damping element.
  • 9. The fuel injector according to claim 8, wherein the circular ring-shaped projection includes a lower end, a diameter of the lower end being smaller than a diameter of the flange.
  • 10. The fuel injector according to claim 9, wherein the damping element is radially clamped between the lower end of the circular ring-shaped projection and the flange.
  • 11. The fuel injector according to claim 8, wherein the circular ring-shaped projection is supported on a cup-shaped cover shell, penetrated by the valve needle.
  • 12. The fuel injector according to claim 11, wherein the flange is disk-shaped and flat and has an outer diameter equivalent to an inner diameter of the cover shell.
  • 13. The fuel injector according to claim 12, wherein the damping element is arranged between the cover shell and the flange.
Priority Claims (1)
Number Date Country Kind
100 43 085 Sep 2000 DE
PCT Information
Filing Document Filing Date Country Kind
PCT/DE01/03266 WO 00
Publishing Document Publishing Date Country Kind
WO02/18776 3/7/2002 WO A
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Number Date Country
198 16 315 Oct 1999 DE
198 55 547 Jun 2000 DE