Common rail injector

Information

  • Patent Grant
  • 6726121
  • Patent Number
    6,726,121
  • Date Filed
    Monday, August 20, 2001
    23 years ago
  • Date Issued
    Tuesday, April 27, 2004
    20 years ago
Abstract
The invention relates to a common rail injector for injecting fuel in a common rail injection system of an internal combustion engine, which system has an injector housing (1) with a fuel inlet (24) that is in communication with a central high-pressure fuel reservoir outside the injector housing (1) and with a pressure chamber (27) inside the injector housing (1), from which fuel subjected to high pressure is injected as a function of the position of a control valve (18) that assures that a nozzle needle (8), which is movable back and forth and received in a longitudinal bore (6) of the injector axially counter to the prestressing force of a nozzle spring (21) that is received in a nozzle spring chamber (20), lifts from a seat when the pressure in the pressure chamber (27) is greater than the pressure in a control chamber (30) that communicates with the fuel inlet (24) via an inlet throttle (19).To achieve markedly higher nozzle needle speeds, the control chamber (15) is formed by a cylindrical chamber, in which a control peg (12), embodied on the end of the nozzle needle (8) remote from the combustion chamber, is displaceable causing a sealing effect, and that the nozzle spring chamber (20) is disposed outside the control chamber (15), in the region of the end of the nozzle needle (8) remote from the combustion chamber.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The invention relates to a common rail injector for injecting fuel in a common rail injection system of an internal combustion engine, which system has an injector housing with a fuel inlet that is in communication with a central high-pressure fuel reservoir outside the injector housing and with a pressure chamber inside the injector housing, from which fuel subjected to high pressure is injected as a function of the position of a control valve that assures that a nozzle needle, which is movable back and forth and received in a longitudinal bore of the injector axially counter to the prestressing force of a nozzle spring that is received in a nozzle spring chamber, lifts from a seat when the pressure in the pressure chamber is greater than the pressure in a control chamber that communicates with the fuel inlet via an inlet throttle.




2. Description of the Prior Art




In common rail injection systems, a high-pressure pump pumps the fuel into the central high-pressure fuel reservoir, which is called a common rail. From the high-pressure fuel reservoir, high-pressure lines lead to the individual injectors, which are assigned to the engine cylinders. The injectors are triggered individually by the engine electronics. The rail pressure prevails in the pressure chamber and at the control valve. When the control valve opens, the nozzle needle lifts from its seat counter to the prestressing force of the nozzle spring, and fuel subjected to high pressure is injected into the combustion chamber.




In conventional injectors of the kind known for instance from German Patent Disclosures DE 197 24 637 A1, relatively long nozzle needles are used. In operation, because of the high pressures and the rapid load changes, very strong forces act on the nozzle needle. These forces cause the nozzle needle to be stretched and compressed in the longitudinal direction. This in turn means that the nozzle needle stroke varies as a function of the forces acting on the nozzle needle.




SUMMARY OF THE INVENTION




It is the object of the invention to furnish a common rail injector that while using conventional injection nozzles makes markedly higher nozzle needle speeds possible. Furthermore, the injector of the invention should be simple in construction and should be able to be produced economically.




In a common rail injector for injecting fuel in a common rail injection system of an internal combustion engine, which system has an injector housing with a fuel inlet that is in communication with a central high-pressure fuel reservoir outside the injector housing and with a pressure chamber inside the injector housing, from which fuel subjected to high pressure is injected as a function of the position of a control valve that assures that a nozzle needle movable back and forth and received in a longitudinal bore of the injector axially counter to the prestressing force of a nozzle spring that is received in a nozzle spring chamber, lifts from a seat when the pressure in the pressure chamber is greater than the pressure in a control chamber that communicates with the fuel inlet via an inlet throttle, this object is attained in that the control chamber is formed by a cylindrical chamber, in which a control peg, embodied on the end of the nozzle needle remote from the combustion chamber, is displaceable causing a sealing effect, and that the nozzle spring chamber is disposed outside the control chamber, in the region of the end of the nozzle needle remote from the combustion chamber. It is also conceivable to accommodate the nozzle spring in the control chamber. Then, however, the installation space of the nozzle spring can unfavorable impact the function of the injector. To achieve acceptable closing speeds, a high spring rigidity is necessary, which in turn requires a large installation space. This increases the control chamber volume, and the performance of the injector becomes worse. This impairs in particular the definition of the instant of injection and the length of injection. Furthermore, the requisite control quantity is increased, so that the overall efficiency drops and there is a risk of excessive fuel heating. The invention offers the advantage that the control chamber and the nozzle spring chamber can be combined on the end remote from the combustion chamber of the nozzle needle, without the volume of the control chamber depending on the structural space of the nozzle spring. It is therefore possible to build in a nozzle spring with high spring rigidity, which assures good closure of the nozzle needle. As a result, the injection time and the instant of injection can be defined exactly. With the injector of the invention, nozzle needle speeds that are greater than 1 m/s can be attained during opening and closing. Because of the control peg that is displaceable in the control chamber, the nozzle needle diameter can be selected arbitrarily. By separating the functional measure, or length, which for instance can amount to 3 mm, and the production measure, or length, which can for instance amount to 4 mm, production costs are reduced.




A particular type of embodiment of the invention is characterized in that the fuel inlet discharges into the nozzle spring chamber, and that at least one flat face is embodied on the nozzle needle between the nozzle spring chamber and the pressure chamber. As a result of the flat face, a flow connection is created between the nozzle spring chamber and the pressure chamber, through which the fuel to be injected reaches the pressure chamber from the fuel inlet. The bore to the pressure chamber which is present in conventional injectors can be omitted.




A particular type of embodiment of the invention is characterized in that the control chamber is embodied in a valve piece, which has a central outlet bore with an outflow throttle and a valve seat. Through the central outlet bore, a communication between the control chamber and a relief chamber is created. The valve seat cooperates with a control valve member of a 2/2-way valve, which controls the course of injection of the injector of the invention.




Further particular types of embodiment of the invention are characterized in that the inlet throttle is integrated with either the valve piece or the nozzle needle. The inlet throttle can take the form of a bore or a groove. For production and/or cost reasons, one or the other type of embodiment will be preferable.




A particular type of embodiment of the invention is characterized in that the nozzle needle is guided by the control peg. Because of the functional principle according to the invention, no internal leakage at the guide occurs in the unactuated state. This means lower specific consumption values.




A particular type of embodiment of the invention is characterized in that the nozzle needle is guided on its end toward the combustion chamber. The additional guidance of the nozzle needle increases the operating reliability and the service life of the injector.




A particular type of embodiment of the invention is characterized in that a step which forms a stop for a spring plate is embodied on the nozzle needle. The spring plate forms an abutment for the nozzle spring and at the same time forms the stroke stop for the nozzle needle. By the choice of a suitable thickness of the spring plate, both the prestressing force of the nozzle spring and the nozzle needle stroke can be adjusted.











BRIEF DESCRIPTION OF THE DRAWINGS




Further advantages, characteristics and details of the invention will become apparent from the ensuing description, in which various exemplary embodiments of the invention are described in detail in conjunction with the drawing, in which:





FIG. 1

is a fragmentary sectional view of a first exemplary embodiment of an injector of the invention with an inlet throttle in the valve piece;





FIG. 2

is a view similar to FIG.


1


and showing a second exemplary embodiment of an injector of the invention with an inlet throttle in the nozzle needle;





FIG. 3

illustrates a third exemplary embodiment of an injector of the invention with a throttle groove in the nozzle needle; and





FIG. 4

illustrates a fourth exemplary embodiment of an injector of the invention with a throttle groove and separate needle guidance.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




The first exemplary embodiment of the injector of the invention, shown in longitudinal section in

FIG. 1

, has an injector housing identified overall by reference numeral


1


. The injector housing


1


includes a nozzle body


2


, which protrudes with its lower, free end into the combustion chamber of the internal combustion engine to be supplied. With its upper end face, remote from the combustion chamber, the nozzle body


2


is axially braced by a lock nut


5


against a valve body


3


and an injector body


4


. A circumferential rib


26


extending all the way around on the inside is embodied on the retaining body


4


. A valve piece


3


is braced with a collar on the circumferential rib


26


.




An axial longitudinal bore


6


is recessed out of the nozzle body


2


. A nozzle needle


8


is received axially displaceably in the longitudinal bore


6


. A sealing face is embodied on the tip


9


of the nozzle needle


8


, and this face cooperates with a sealing seat that is embodied on the nozzle body


2


. When the tip


9


of the nozzle needle


8


is located with its sealing face in contact with the sealing seat, an injection port


10


in the nozzle body


2


is closed. When the nozzle needle tip


9


lifts from its seat, fuel subjected to high pressure is injected through the injection port


10


into the combustion chamber of the engine.




Beginning at the tip


9


, the nozzle needle


8


has three regions of different diameters d


1


, d


2


and d


3


. The diameter d


2


is the largest, and the diameters d


1


and d


3


, in the present exemplary embodiment, are of equal size but can also be different. The end remote from the combustion chamber of the nozzle needle


8


having the diameter d


3


forms a control peg


12


, which is guided axially displaceably in a central bore


14


in the valve piece


3


.




The central bore


14


and the end face, remote from the combustion chamber, of the control peg


12


of the nozzle needle


8


define a control chamber


15


. The control chamber


15


can be made to communicate via a fuel outlet


16


with a relief chamber (not shown). An outflow throttle


17


is provided in the fuel outlet


16


. With the aid of a control valve member


18


, the fuel outlet


16


can be opened and closed.




Through an inlet throttle


19


, fuel can reach the control chamber


15


. The inlet throttle


19


connects the control chamber


15


to a nozzle spring chamber


20


. The nozzle spring chamber


20


communicates with a fuel inlet


24


, through which fuel subjected to high pressure from the rail (not shown) reaches the nozzle spring chamber


20


. A nozzle spring


21


is disposed in the nozzle spring chamber


20


. The nozzle spring


21


is braced by one end on the circumferential rib


26


of the retaining body


4


. By its other end, the nozzle spring


21


is braced on a spring plate


22


. The prestressing force of the nozzle spring


21


is transmitted to the nozzle needle


8


by the spring plate


22


. For that end, a step


23


is formed on the nozzle needle


8


between the control peg


12


having the diameter d


3


and the portion of the nozzle needle


8


having the diameter d


2


.




In the portion of the nozzle needle


8


having the diameter d


2


, a flat face


25


is formed. The flat face


25


creates a communication between the nozzle spring chamber


20


and a pressure chamber


27


, which forms a fuel reservoir. When the fuel outlet


16


is closed by the control valve member


18


, rail pressure prevails in the control chamber


15


and the pressure chamber


27


. The prestressing force of the nozzle spring


21


then assures that the tip


9


of the nozzle needle


8


will remain in contact with its associated seat on the nozzle body


2


. In this position of the nozzle needle


8


, no injection takes place.




When the control valve member


18


opens the fuel outlet


16


, the pressure in the control chamber


15


drops. In the pressure chamber


27


, rail pressure still prevails as before. As a result, the nozzle needle


8


with its tip


9


lifts from the associated seat, and fuel is injected into the combustion chamber of the engine. When the control valve member


18


closes the fuel outlet


16


again, the pressure in the control chamber


15


rises, which causes the nozzle needle


8


to close.




The valve piece


3


and the control valve member


18


form a servo valve. The servo valve can be embodied as a singly or doubly switching valve. As valve positioners, magnets or piezoelectric elements can be used. In the exemplary embodiment shown in

FIG. 1

, the inlet throttle


19


is located in the valve piece


3


. For production and cost reasons, the inlet throttle can also be embodied in some other component, such as the nozzle needle


8


. What is important is that the nozzle spring


21


be located outside the control chamber


15


. The prestressing and the stroke can be adjusted by the thickness of the spring plate


22


. Instead of one flat face


25


, a plurality of flat faces can also be provided on the nozzle needle


8


. The flow cross section resulting from the flat faces agrees with the inlet bore of a conventional nozzle.




If no injection is taking place, the nozzle needle


8


is pressed into the seat by the rail pressure. The total of the control chamber closing force and the nozzle spring closing force predominates over the seat force at the needle seat. The injection is initiated by the pressure relief of the control chamber


15


. The nozzle needle


8


lifts from its seat and in the final stroke, with the spring plate


22


, it strikes the valve piece


3


. The opening and closing speed are determined, given a fixed outlet/inlet ratio, by the cross section of the control peg


12


, whose positively displaced volume acts like an additional source (in the opening process) or sink (in the closing process). In order not to shift the balance of forces between the needle seat and the control peg unilaterally, in conventional common rail systems with a thrust rod, one must reduce the needle diameter from 4 mm to approximately 3 to 3.5 mm. The production and cost aspects are problematic here. The advantage of the invention is that the hydraulically effective diameter is independent of the geometrically predetermined needle diameter. As soon as the control valve member


18


closes again, the pressure in the control chamber


15


rises, and the nozzle needle


8


returns to its seat.




The exemplary embodiment shown in

FIG. 2

is largely equivalent to the first exemplary embodiment of the invention shown in FIG.


1


. For the sake of simplicity, the same reference numerals are used to designate identical parts. In addition, to avoid repetition, reference is made to the above description of the first exemplary embodiment. Below, only the distinctions between the two exemplary embodiments will be addressed. The procedure will be analogous for the extensive description of the exemplary embodiments shown in

FIGS. 3-4

.




In the second exemplary embodiment shown in

FIG. 2

, the inlet throttle is disposed not in the valve piece


3


but in the nozzle needle


8


. Fuel subjected to high pressure reaches the control chamber


15


, via a radial bore


31


and an axial bore


30


with an inlet throttle


29


.




In the third exemplary embodiment shown in

FIG. 3

, the inlet throttle takes the form of an axial groove


35


, which is made on the control peg


12


. Through the axial groove


35


, fuel at high pressure from the region of the flat face


25


on the nozzle needle


8


reaches the control chamber


15


.




In the exemplary embodiment shown in

FIG. 4

, unlike the third exemplary embodiment above, an additional guide


38


is formed on the end toward the combustion chamber of the nozzle needle


8


. A plurality of flat faces


39


assure a flow connection from the pressure chamber


27


to the nozzle needle tip


9


.




The foregoing relates to preferred exemplary embodiments of the invention, it being understood that other variants and embodiments thereof are possible within the spirit and scope of the invention, the latter being defined by the appended claims.



Claims
  • 1. In a common rail injector for injecting fuel in a common rail injection system of an internal combustion engine, which system has an injector housing (1) with a fuel inlet (24) that is in communication with a central high-pressure fuel reservoir outside the injector housing (1) and with a pressure chamber (27) inside the injector housing (1), from which fuel subjected to high pressure is injected as a function of the position of a control valve (18) that assures that a nozzle needle (8), which is movable back and forth and received in a longitudinal bore (6) of the injector axially counter to the prestressing force of a nozzle spring (21) that is received in a nozzle spring chamber (20), lifts from a seat when the pressure in the pressure chamber (27) is greater than the pressure in a control chamber (15) that communicates with the fuel inlet (24) via an inlet throttle (19), the improvement wherein the control chamber (15) is formed by a cylindrical chamber, into which a control peg (12), embodied on the end of the nozzle needle (8) remote from the combustion chamber, is displaceable causing a sealing effect, and that the nozzle spring chamber (20) is disposed outside the control chamber (15), in the region of the end of the nozzle needle (8) remote from the combustion chamber, wherein the fuel inlet (24) discharges into the nozzle spring chamber (20), and that at least one flat face (25) is embodied on the nozzle needle (8) between the nozzle spring chamber (20) and the pressure chamber (27).
  • 2. The common rail injector of claim 1, wherein the control chamber (15) is embodied in a valve piece (3), which has a central outlet bore (16) with an outflow throttle (17) and a valve seat.
  • 3. The common rail injector of claim 2, wherein the inlet throttle is provided in a bore (19) in the valve piece (3), which bore connects the control chamber (15) with the nozzle spring chamber (20).
  • 4. The common rail injector of claim 2, wherein the inlet throttle (30, 31; 35) is integrated with the nozzle needle (8).
  • 5. The common rail injector of claim 4, wherein the inlet throttle (29) is disposed in a central bore (30) in the nozzle needle (8), which bore communicates with the nozzle spring chamber (20) via a radial bore (31).
  • 6. The common rail injector of claim 4, wherein the inlet throttle is formed by a groove (35), which extends in the longitudinal direction of the nozzle needle (8) and is provided on the control peg (12).
  • 7. The common rail injector of claim 2, wherein the nozzle needle (8) is guided by the control peg (12).
  • 8. The common rail injector of claim 2, wherein the nozzle needle (8) is guided on its end (38) toward the combustion chamber.
  • 9. The common rail injector of claim 2, wherein a step (23) which forms a stop for a spring plate (22) is embodied on the nozzle needle (8).
  • 10. The common rail injector of claim 1, wherein the nozzle needle (8) is guided by the control peg (12).
  • 11. The common rail injector of claim 1, wherein the nozzle needle (8) is guided on its end (38) toward the combustion chamber.
  • 12. The common rail injector of claim 1, herein a step (23) which forms a stop for a spring plate (22) is embodied on the nozzle needle (8).
  • 13. The common rail injector of claim 1, wherein the inlet throttle is disposed in a central bore (30) in the nozzle needle (8), which bore communicates with the nozzle spring chamber (20) via a radial bore (31).
  • 14. The common rail injector of claim 1, wherein the inlet throttle is formed by a groove (35), which extends in the longitudinal direction of the nozzle needle (8) and is provided on the control peg (12).
Priority Claims (1)
Number Date Country Kind
199 36 667 Aug 1999 DE
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a 35 USC 371 application of PCT/DE 00/02530 filed on Aug. 1, 2000.

PCT Information
Filing Document Filing Date Country Kind
PCT/DE00/02530 WO 00
Publishing Document Publishing Date Country Kind
WO01/11219 2/15/2001 WO A
US Referenced Citations (4)
Number Name Date Kind
5183019 Suhara Feb 1993 A
5711277 Fuseya Jan 1998 A
5820033 Cooke Oct 1998 A
6168087 Cooke Jan 2001 B1
Foreign Referenced Citations (4)
Number Date Country
44 46 269 Jun 1996 DE
0 331 198 Sep 1989 EP
0 334 364 Sep 1989 EP
0789142 Mar 1997 EP