EP1131552B1 - Fuel injection valve for internal combustion engines - Google Patents

Fuel injection valve for internal combustion engines Download PDF

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Publication number
EP1131552B1
EP1131552B1 EP99947182A EP99947182A EP1131552B1 EP 1131552 B1 EP1131552 B1 EP 1131552B1 EP 99947182 A EP99947182 A EP 99947182A EP 99947182 A EP99947182 A EP 99947182A EP 1131552 B1 EP1131552 B1 EP 1131552B1
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EP
European Patent Office
Prior art keywords
control
injection valve
bore
fuel
piston
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Expired - Lifetime
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EP99947182A
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German (de)
French (fr)
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EP1131552A1 (en
Inventor
Marco A. Ganser
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Ganser Hydromag AG
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Ganser Hydromag AG
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure

Definitions

  • the invention relates to a fuel injection valve for intermittent fuel injection in the combustion chamber of an internal combustion engine according to the preamble of claim 1.
  • This Injection valve can for example in so-called common rail injection systems Diesel engines are used.
  • Fuel injection valves of this type are known, for example, from the patents EP 0 262 539, DE 196 50 865, EP 0 603 616 or US 5 685 483 are known.
  • the opening and closing movement of the injection valve member is controlled by Control of the control room pressure in a control room above a control piston, with the the injection valve member is operatively connected. At the end of its opening movement, the injection valve member stopped by a mechanical stop.
  • the injection valve member is multi-part and long.
  • the length of the injector member is depending on the application of the injection system for a certain engine type depending on the engine design.
  • the stop is in a distance from the top of the injector member. This causes a swing the free, upper end of the injection valve member after stopping its opening movement. This vibration causes undesired, imprecise closing movements of the injection valve member at the end of the injection process.
  • the present invention aims at both avoiding swinging and detaching of the injection valve member in a precisely controllable manner, with which the injection processes can be realized with great reproducibility and accuracy.
  • a fuel injection valve 1 via a high-pressure fuel connection 10 with a high-pressure delivery device for the fuel and via electrical connections 12 connected to an electronic control.
  • the high pressure conveyor and the electronic Controls are not shown in the drawing.
  • the housing of the fuel injector 1 is designated 14. At the bottom is that Housing 14 screwed with a retaining part 16 designed as a union nut.
  • the cap nut 16 presses a middle part 18 against a sealing surface 20 in a sealed manner is located between the housing 14 and the middle part 18.
  • the union nut 16 a nozzle body 22 on a sealing surface 24 between the middle part 18 and the nozzle body 22 pressed tightly.
  • the nozzle tip 26 protrudes from the union nut 16.
  • the nozzle tip 26 has a nozzle needle seat 28 and a plurality of injection openings 30 Mistake.
  • the nozzle body 22 there is an axially adjustable nozzle needle forming an injection valve member 32 closely guided in a needle guide bore 34.
  • the injection ports 30 of the Nozzle tip 26 can be closed by a lower end 36 of the nozzle needle 32.
  • the nozzle needle 32 On the face side, the nozzle needle 32 is in the middle part 18 in a piston guide bore 40 closely sliding, axially adjustable control piston 38 operatively connected.
  • the movement of the Control piston 38 and thus also the nozzle needle 32 is by means of a solenoid valve 6 cooperating control device 8, which is further below with reference to FIG. 2nd are described in more detail.
  • the fuel is fed through the high-pressure delivery device via the high-pressure fuel connection 10 into a fuel supply bore 42 and from there into a downward bore 44 of the housing 14 promoted.
  • the bore 44 opens into a made in the middle part 18 Bore 46.
  • the bore 46 opens at the lower end into a nozzle body bore 48.
  • In the middle part 18 connects a further, short bore 50 to the control device 8 with the bore 46.
  • the nozzle body bore 48 opens into an annular space 52 in the nozzle body 22. From the annular space 52, the fuel reaches the nozzle needle seat 28 via passages (not shown) or to the injection openings 30.
  • a retaining screw 54 is screwed, which with the extended portion 56, which extends into a receiving bore 58, the solenoid valve 6 holds in the housing 14.
  • the solenoid valve 6 is guided radially in the receiving bore 58.
  • the magnetic valve 6 has a magnetic body 60 in which a pole disk 62 is permanently installed.
  • the coil 64 which is the electrical Connections 12 is connected to the electronic control, not shown.
  • a magnetic valve spring 66 and a spring tensioning element 68 are located in the magnetic body 60 Choice of the length of the spring tensioning element 68 is an optimal bias of the solenoid valve spring 66 set.
  • the magnet armature 70 is firmly connected to the control valve stem 72, so that these two elements form a control valve 74.
  • a control body 78 is inserted in a bore 76 of the housing 14 and on the lower one Supported area 80 of the federal government 82.
  • the control body 78 is preferably provided with a press or a narrow sliding seat in the bore 76, so that no significant Leakage can take place.
  • other fuel-tight connections could also be used, for example can be realized using suitable sealing rings.
  • the control piston 38 which is guided in the piston guide bore 40 in the middle part 18 so as to slide closely has a groove 84 and a transverse bore 86 connected to the groove 84.
  • the groove is 84 with the short bore 50, the transverse bore 86 with an axially made in the control piston 38
  • a needle spring 90 a spring tensioning element
  • the spring tensioning element 92 serves to set a specific one Force of the needle spring 90.
  • the needle spring 90 holds the nozzle needle in a known manner 32 in contact with the nozzle needle seat 28 when there is no injection and when there is no pressure Injection system.
  • the fuel pressure it pushes the upper end 96 of the control sleeve 94 continuously on the control body 78.
  • the control sleeve 94 has a longitudinal bore 98 opening into the bore 88.
  • a first one Control bore 100 connects the longitudinal bore 98 to the control chamber 102.
  • the control chamber 102 is connected to the second control bore 106.
  • the control bore 106 By means of a Flat seat 108 between the control body 78 and control valve 74, the control bore 106 at de-energized solenoid valve 6 closed by the control valve 74 against the high system pressure held.
  • the one emerging from the second control bore 106 when the control valve 74 is raised Fuel is, together with the leak fuel, which from the two guide holes 34 and 40 enters the annular space 110, by means of the bore 112 (FIG. 1) to known ones Returned way at low pressure of the high pressure conveyor.
  • the longitudinal axis 114 is the receiving bore 58 of the solenoid valve 6 with respect to the longitudinal axis common to the control piston 38 and the nozzle needle 32 116 disaxed. This is only in the dimensions of the housing 14 and shown Solenoid valve 6 required to have enough wall thickness for the high pressure bore 44 available to deliver. With larger dimensions of the housing 14, or smaller dimensions of the solenoid valve 6, the two longitudinal axes 114 and 116 can also match.
  • the connection 104 in the control body 78 is omitted in this case.
  • Control piston 38 has an annular web 124 which is not interrupted on the circumference. 3a, 3b and 3c, the two annular leak gaps 126 (between the control sleeve 94 and control piston 38) and 128 (between control piston 38 and middle part 18) for clarification the operation of the fuel injector 1 shown exaggerated.
  • the mode of operation of the fuel injection valve 1 is now based on FIGS. 1, 2, 3a, 3b and 3c as follows: when the solenoid valve 6 is energized with a current pulse, the control valve shaft moves 72 after a short time away from the flat seat 108 and gives the second control bore 106 free. The fuel control pressure in the connection 104, in the control chamber 102 and in the relief chamber 122 drops. On the one hand, this enables injection by lifting the control piston 38 and the nozzle needle 32 start away from the nozzle needle seat 28. The control piston moves 38 relative to the middle part 18 and the stationary control sleeve 94 upwards.
  • the fuel flow through the leakage gaps 128 and 126 is quantitative is smaller than that through the first control bore 100. This is achieved by realizing a tight sliding fit (with, for example, 1 to 3 micrometers of play) between the parts.
  • the height of the web 124 can only amount to a few hundredths of a millimeter (for example 2 to 10 hundredths). That was realized causes very small volume of the relief space 122, despite the small inflow amount through the leakage gap 124, an instantaneous increase in the pressure in the relief space 122nd
  • Fig. 4 shows a partial longitudinal section of a second embodiment of a fuel injector 2.
  • the elements not shown can be the same as those of the fuel injector 1 according to Fig. 1. Same elements as in Figs. 1 to 3c or those which are the exact perform the same function have been given the same numbers in FIG. 4.
  • the control valve stem 72 is located in the fuel injector 2 (and therefore not shown solenoid valve 6) on the same longitudinal axis 116 as the control piston 130 and the Nozzle needle 32.
  • the control body 132 is in the middle part 18 in an analogous manner to the Fuel injector 1 installed.
  • the control sleeve 94 of the fuel injector 1 is omitted in the fuel injector 2.
  • a short bore 142 connects the groove 84 with the first Control bore 100.
  • the control bore 100 opens into a made in the control piston 130 Longitudinal bore 136, which together with the bore 134 in the control body 132 and the Disk space 138 forms the control space 140.
  • the needle spring 144 is in the lower tapered portion 146 of spool 130 in a region with low fuel pressure level. Two elements 148a and 148b position and tension the needle spring 144.
  • the tapered one Section 146 presses on the end face of the nozzle needle 32.
  • this area of the fuel injection valve 2 becomes simplified. Attaching the needle spring 144 outside the high pressure spool area enables a freer design of the volume of the control room 140 and the radial dimensioning of the web 124. On the other hand, a longer version of the middle part 18 are accepted. How the fuel injector works 2 is analogous to that of the fuel injection valve 1.
  • the middle part 18 in the a lower thread on which the union nut 16 is screwed With another The middle part 18 is screwed onto the housing 14. The middle part 18 points in this top a waistband. This embodiment is cheap if a long one Fuel injector must be used.
  • Fig. 5 shows a partial longitudinal section of a third embodiment of a fuel injector 3. Again, the elements not shown are the same as those of the fuel injector 1 according to Fig. 1. The same elements as in the preceding figures or those which perform exactly the same function, were also in Fig. 5 with the same digits as in the preceding Figures.
  • the control valve stem 72 is located on the longitudinal axis 116.
  • a disk-shaped one Intermediate plate 150 is located between the lower end of the housing 14 and the nozzle body 22.
  • the intermediate plate 150 and the nozzle body 22 held together by the union nut 16 in a sealed manner by means of the two sealing surfaces 20 and 24.
  • the fuel supply bore 44 opens into a bore 152 in the intermediate plate 150.
  • the first control bore 100 in a on the longitudinal axis 116 in the intermediate plate 150 Bore 158. Bore 158 is with the second control bore 106 and with an in Control piston 160 connected bore 162 connected.
  • a pressed-in can be used instead of the intermediate plate 150 Part, similar to the control body 78 of FIG. 2 or the control body 132 of FIG. 4, be used.
  • control piston 160 is now one piece with the nozzle needle 32.
  • a needle spring 164 is located together with the spring tensioning element 166, in the bore 162.
  • the spring tensioning element 166 has a nose 167, which as Filler piece is used. Without the nose 167, the total volume of the control room consists of the fuel volume in the bores 158 and 162 depending on the dimensioning of these Elements unfavorably large. With the nose 167 it can be reduced. That being said the function of these elements the same as before.
  • the relief chamber 122 is in turn between that at the upper end of the control piston 160 existing web 124 and the needle guide bore 34.
  • the leak fuel now flows during the injection process from the annular space 52 in the nozzle body 22 over the Leakage gap between control piston 160 and needle guide bore 34 in the relief chamber 122.
  • the mode of operation of the fuel injection valve 3 is again analogous to that of the previous one Versions.
  • the design of the fuel injector 3 is particularly simple.
  • a throttle bore 168 may be between bore 152 and bore 48, however after the inlet to the bore 156. This throttle bore 168 causes during the injection process a pressure drop of, for example, 5-10% of the standing pressure and causes a faster closing movement of the nozzle needle 32 in a known manner.
  • FIG. 6 shows an alternative embodiment of the fuel injection valve 3 from FIG. 5 6, the needle spring 164 was in a bore 170 of the Intermediate plate 150 installed. 5 has been omitted, although it is also in Fig. 6 either on the bottom or on the top of the needle spring 164 could be installed.
  • the throttle bore 168 is now part of the intermediate plate 150.
  • the operation of the fuel injector 3a is the same as that of the fuel injector Third
  • control body 132 of the fuel injector 2 can either in the housing 14 or in the Intermediate plate 150 can be installed.
  • This control body can either only be the second Have control bore 106 or the first control bore 100.
  • the intermediate plate 150 of the fuel injector 3a can be shown with a dashed line Separation line 172 shown level are ended. in this case, the needle spring 164 of the side of the dividing line 172. Then the force of the needle spring 164 with transfer a narrow pin attached to the underside of the spring onto the needle piston 160, the underside 120 of the intermediate plate 150 facing the web 124 can be covered with a smaller bore than the bore 170 through which only the narrow pin protrudes. In this way you get, analogous to the design of the fuel injector 2 of FIG. 4, greater freedom in the radial dimensioning of the web 124.
  • the solenoid valve 6 can also be operated with the control valve stem 72 either as in FIGS. 5 and 6 on the longitudinal axis 116 or, as in the case of the fuel injector 1, out of alignment become.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

A fuel injection valve for intermittent injection of fuel into the combustion chamber of a diesel or other form of internal combustion engine. The valve achieves a shorter than usual injection valve member, while avoiding valve member oscillation but retaining precise closing by implementing a solenoid controlled piston that controls movement of the valve. The piston in turn is acted upon by fuel system pressure from a high pressure feed line and from a control chamber, alternatively, depending upon the position of an actuating element. The control piston has an annular land that faces the control chamber and the piston is connected to the high pressure feed line through a tight sliding fit in a piston guide bore establishing a leak gap. A relief chamber is formed between the outlet side of the gap and the land. When the injection valve is open, the land reduces fuel flow from the relief chamber into the control chamber. As a result, fuel pressure in the relief chamber rises compared to that in the control chamber.

Description

Die Erfindung betrifft ein Brennstoffeinspritzventil zur intermittierenden Brennstoffeinspritzung in den Brennraum einer Verbrennungskraftmaschine gemäss Oberbegriff des Anspruches 1. Dieses Einspritzventil kann beispielsweise bei sogenannten Common Rail Einspritzsystemen für Dieselmotoren verwendet werden.The invention relates to a fuel injection valve for intermittent fuel injection in the combustion chamber of an internal combustion engine according to the preamble of claim 1. This Injection valve can for example in so-called common rail injection systems Diesel engines are used.

Brennstoffeinspritzventile dieser Art sind beispielsweise aus den Patentschriften EP 0 262 539, DE 196 50 865, EP 0 603 616 oder US 5 685 483 bekannt. Bei diesen bekannten Brennstoffeinspritzventilen erfolgt die Steuerung der Öffnungs- und Schliessbewegung des Einspritzventilgliedes durch Steuerung des Steuerraum-Druckes in einem Steuerraum oberhalb eines Steuerkolbens, der mit dem Einspritzventilglied wirkverbunden ist. Am Ende seiner Öffnungsbewegung wird das Einspritzventilglied durch einen mechanischen Anschlag gestoppt.Fuel injection valves of this type are known, for example, from the patents EP 0 262 539, DE 196 50 865, EP 0 603 616 or US 5 685 483 are known. In these known fuel injection valves the opening and closing movement of the injection valve member is controlled by Control of the control room pressure in a control room above a control piston, with the the injection valve member is operatively connected. At the end of its opening movement, the injection valve member stopped by a mechanical stop.

In der EP 0 603 616 ist das Einspritzventilglied mehrteilig und lang. Die Länge des Einspritzventilgliedes ist je nach Anwendung des Einspritzsystems bei einem bestimmten Motortyp von der Motorkonstruktion abhängig. Bei dieser bekannten Lösung befindet sich der Anschlag in einer Entfernung vom oberen Ende des Einspritzventilgliedes. Dies verursacht ein Schwingen des freien, oberen Endes des Einspritzventilgliedes nach dem Stoppen seiner Öffnungsbewegung. Diese Schwingung verursacht unerwünschte, unpräzise Schliessbewegungen des Einspritzventilgliedes am Ende des Einspritzvorgangs.In EP 0 603 616, the injection valve member is multi-part and long. The length of the injector member is depending on the application of the injection system for a certain engine type depending on the engine design. In this known solution, the stop is in a distance from the top of the injector member. This causes a swing the free, upper end of the injection valve member after stopping its opening movement. This vibration causes undesired, imprecise closing movements of the injection valve member at the end of the injection process.

In der EP 0 262 539 ist das Einspritzventilglied ebenfalls lang. Die Öffnungsbewegung des Einspritzventilgliedes wird durch eine Anschlagfläche zwischen dem oberen Ende des Steuerkolbens und einer Unterseite eines Koibenführungsteils im Inneren des Steuerraumes gestoppt. Durch diese Anordnung wird die obenerwähnte Schwingung vermieden, aber zu Beginn der Schliessbewegung ist das Loslösen des Einspritzventilgliedes von der Anschlagfläche mit unkontrollierbaren zeitlichen Schwankungen verbunden, welche wiederum ein unpräzises schliessen verursachen.In EP 0 262 539 the injection valve member is also long. The opening movement of the injection valve member is by a stop surface between the upper end of the spool and a bottom of a Koibenführungteiles stopped inside the control room. With this arrangement, the above-mentioned vibration is avoided, but at the beginning of the Closing movement is the detachment of the injection valve member from the stop surface with uncontrollable temporal fluctuations, which in turn is an imprecise close cause.

Die vorliegende Erfindung bezweckt sowohl das Vermeiden des Schwingens als auch das Loslösen des Einspritzventilgliedes in einer exakt kontrollierbarer Art und Weise, womit die Einspritzvorgänge mit grosser Reproduzierbarkeit und Genauigkeit realisiert werden können.The present invention aims at both avoiding swinging and detaching of the injection valve member in a precisely controllable manner, with which the injection processes can be realized with great reproducibility and accuracy.

Diese Aufgabe wird erfindungsgemäss durch die im Kennzeichen des Anspruches 1 angegebene Merkmale gelöst. This object is achieved according to the invention by the characterizing part of claim 1 Features solved.

Die Erfindung wird nun im Folgenden anhand der Zeichnungen näher dargelegt.The invention will now be explained in more detail below with reference to the drawings.

Es zeigen:

Fig. 1
eine erste Ausführungsform eines Brennstofteinspritzventils 1 im Längsschnitt;
Fig. 2
einen vergrösserten, partiellen Längsschnitt durch das Brennstoffeinspritzventil nach Fig. 1 mit der Anordnung zur präzisen Steuerung des Schliessvorganges des Einspritzventilgliedes ;
Fig. 3a, 3b
drei Phasen des zeitlichen Ablaufs der Öffnungsbewegung des Einspritzventilund 3c gliedes des Brennstoffeinspritzventils nach Fig. 1 und 2 in vergrössertem Massstab;
Fig. 4
ein partieller Längsschnitt einer zweiten Ausführungsform eines Brennstoffeinspritzventils 2;
Fig. 5
ein partieller Längsschnitt einer dritten Ausführungsform eines Brennstoffeinspritzventils 3;
Fig. 6
ein partieller Längsschnitt einer alternativen Ausführungsform 3a des Brennstoffeinspritzventils 3 von Fig. 5.
Show it:
Fig. 1
a first embodiment of a fuel injection valve 1 in longitudinal section;
Fig. 2
an enlarged, partial longitudinal section through the fuel injector of Figure 1 with the arrangement for precise control of the closing process of the injection valve member.
3a, 3b
three phases of the timing of the opening movement of the injection valve and 3c member of the fuel injection valve according to Figures 1 and 2 on an enlarged scale;
Fig. 4
a partial longitudinal section of a second embodiment of a fuel injector 2;
Fig. 5
a partial longitudinal section of a third embodiment of a fuel injector 3;
Fig. 6
5 shows a partial longitudinal section of an alternative embodiment 3a of the fuel injection valve 3 from FIG. 5.

Gemäss Fig. 1 ist ein Brennstoffeinspritzventil 1 über einen Brennstoffhochdruckanschluss 10 mit einer Hochdruck-Fördereinrichtung für den Brennstoff und über elektrische Anschlüsse 12 mit einer elektronischen Steuerung verbunden. Die Hochdruck-Fördereinrichtung und die elektronische Steuerung sind in der Zeichnung nicht dargestellt.1 is a fuel injection valve 1 via a high-pressure fuel connection 10 with a high-pressure delivery device for the fuel and via electrical connections 12 connected to an electronic control. The high pressure conveyor and the electronic Controls are not shown in the drawing.

Das Gehäuse des Brennstoffeinspritzventils 1 ist mit 14 bezeichnet. Am unteren Ende ist das Gehäuse 14 mit einem als Überwurfmutter ausgebildeten Halteteil 16 festgeschraubt. Die Überwurfmutter 16 drückt auf dichte Weise ein Mittelteil 18 an eine Dichtfläche 20 an, welche sich zwischen dem Gehäuse 14 und dem Mittelteil 18 befindet. Zugleich wird von der Überwurfmutter 16 ein Düsenkörper 22 an eine Dichtfläche 24 zwischen dem Mittelteil 18 und dem Düsenkörper 22 auf dichte Weise angedrückt. Die Düsenspitze 26 ragt aus der Überwurfmutter 16 hinaus.The housing of the fuel injector 1 is designated 14. At the bottom is that Housing 14 screwed with a retaining part 16 designed as a union nut. The cap nut 16 presses a middle part 18 against a sealing surface 20 in a sealed manner is located between the housing 14 and the middle part 18. At the same time, the union nut 16 a nozzle body 22 on a sealing surface 24 between the middle part 18 and the nozzle body 22 pressed tightly. The nozzle tip 26 protrudes from the union nut 16.

Die Düsenspitze 26 ist mit einem Düsennadelsitz 28 und mit mehreren Einspritzöffnungen 30 versehen. Im Düsenkörper 22 ist eine ein Einspritzventilglied bildende, axial verstellbare Düsennadel 32 in einer Nadelführungsbohrung 34 eng gleitend geführt. Die Einspritzöffnungen 30 der Düsenspitze 26 sind durch ein unteres Ende 36 der Düsennadel 32 abschliessbar. The nozzle tip 26 has a nozzle needle seat 28 and a plurality of injection openings 30 Mistake. In the nozzle body 22 there is an axially adjustable nozzle needle forming an injection valve member 32 closely guided in a needle guide bore 34. The injection ports 30 of the Nozzle tip 26 can be closed by a lower end 36 of the nozzle needle 32.

Stirnseitig ist die Düsennadel 32 mit einem im Mittelteil 18 in einer Kolbenführungsbohrung 40 eng gleitend geführten, axial verstellbaren Steuerkolben 38 wirkverbunden. Die Bewegung des Steuerkolbens 38 und somit auch der Düsennadel 32 wird mittels einer mit dem Magnetventil 6 zusammenwirkenden Steuervorrichtung 8 gesteuert, welche weiter unten anhand von Fig. 2 näher beschrieben werden.On the face side, the nozzle needle 32 is in the middle part 18 in a piston guide bore 40 closely sliding, axially adjustable control piston 38 operatively connected. The movement of the Control piston 38 and thus also the nozzle needle 32 is by means of a solenoid valve 6 cooperating control device 8, which is further below with reference to FIG. 2nd are described in more detail.

Der Brennstoff wird durch die Hochdruck-Fördereinrichtung über den Brennstoffhochdruckanschluss 10 in eine Brennstoffzufuhrbohrung 42 und von da in eine nach unten gerichtete Bohrung 44 des Gehäuses 14 gefördert. Die Bohrung 44 mündet in eine in Mittelteil 18 angefertigte Bohrung 46. Die Bohrung 46 mündet am unteren Ende in eine Düsenkörperbohrung 48. Im Mittelteil 18 verbindet eine weitere, kurze Bohrung 50 die Steuervorrichtung 8 mit der Bohrung 46. Die Düsenkörperbohrung 48 mündet in einen Ringraum 52 im Düsenkörper 22. Vom Ringraum 52 gelangt der Brennstoff über nicht näher dargestellte Durchgänge zum Düsennadelsitz 28 bzw. zu den Einspritzöffnungen 30.The fuel is fed through the high-pressure delivery device via the high-pressure fuel connection 10 into a fuel supply bore 42 and from there into a downward bore 44 of the housing 14 promoted. The bore 44 opens into a made in the middle part 18 Bore 46. The bore 46 opens at the lower end into a nozzle body bore 48. In the middle part 18 connects a further, short bore 50 to the control device 8 with the bore 46. The nozzle body bore 48 opens into an annular space 52 in the nozzle body 22. From the annular space 52, the fuel reaches the nozzle needle seat 28 via passages (not shown) or to the injection openings 30.

Am oberen Ende des Gehäuses 14 ist eine Halteschraube 54 angeschraubt, welche mit dem verlängerten Teilstück 56, das sich in eine Aufnahmebohrung 58 erstreckt, das Magnetventil 6 im Gehäuse 14 festhält. Das Magnetventil 6 ist in der Aufnahmebohrung 58 radial geführt.At the upper end of the housing 14, a retaining screw 54 is screwed, which with the extended portion 56, which extends into a receiving bore 58, the solenoid valve 6 holds in the housing 14. The solenoid valve 6 is guided radially in the receiving bore 58.

Das Magnetventil 6 weist gemäss Fig. 2 einen Magnetkörper 60 auf, in dem eine Polscheibe 62 fest eingebaut ist. Im Magnetkörper 60 befindet sich die Spule 64, welche über die elektrischen Anschlüsse 12 mit der nicht dargestellten elektronischen Steuerung verbunden ist. Ferner befinden sich im Magnetkörper 60 eine Magnetventilfeder 66 und ein Federspannelement 68. Durch Wahl der Länge des Federspannelementes 68 wird eine optimale Vorspannung der Magnetventilfeder 66 eingestellt. Der Magnetanker 70 ist fest mit dem Steuerventilschaft 72 verbunden, so dass diese beiden Elemente ein Steuerventil 74 bilden.2, the magnetic valve 6 has a magnetic body 60 in which a pole disk 62 is permanently installed. In the magnetic body 60 there is the coil 64, which is the electrical Connections 12 is connected to the electronic control, not shown. Also located a magnetic valve spring 66 and a spring tensioning element 68 are located in the magnetic body 60 Choice of the length of the spring tensioning element 68 is an optimal bias of the solenoid valve spring 66 set. The magnet armature 70 is firmly connected to the control valve stem 72, so that these two elements form a control valve 74.

In einer Bohrung 76 des Gehäuses 14 ist ein Steuerkörper 78 eingesetzt und an der unteren Fläche 80 des Bundes 82 abgestützt. Der Steuerkörper 78 wird vorzugsweise mit einem Pressoder einem engem Schiebesitz in der Bohrung 76 eingebaut, so dass keine nennenswerte Leckage stattfinden kann. Allerdings könnten auch andere brennstoffdichte Verbindungen, beispielsweise unter Verwendung von geeigneten Dichtungsringen realisiert werden.A control body 78 is inserted in a bore 76 of the housing 14 and on the lower one Supported area 80 of the federal government 82. The control body 78 is preferably provided with a press or a narrow sliding seat in the bore 76, so that no significant Leakage can take place. However, other fuel-tight connections could also be used, for example can be realized using suitable sealing rings.

Der im Mittelteil 18 in der Kolbenführungsbohrung 40 eng gleitend geführte Steuerkolben 38 weist eine Nute 84 und eine mit der Nute 84 verbundene Querbohrung 86 auf. Die Nute 84 ist mit der kurzen Bohrung 50, die Querbohrung 86 mit einer axial im Steuerkolben 38 angefertigte The control piston 38, which is guided in the piston guide bore 40 in the middle part 18 so as to slide closely has a groove 84 and a transverse bore 86 connected to the groove 84. The groove is 84 with the short bore 50, the transverse bore 86 with an axially made in the control piston 38

Bohrung 88 verbunden. In der Bohrung 88 befinden sich eine Nadelfeder 90, ein Federspannelement 92 und eine im Steuerkolben 38 eng gleitend geführte Steuerhülse 94. Analog wie bei der Magnetventilfeder 66, dient das Federspannelement 92 zum Einstellen einer bestimmten Kraft der Nadelfeder 90. Die Nadelfeder 90 hält einerseits auf bekannte Weise die Düsennadel 32 in Anlage an den Düsennadelsitz 28 wenn keine Einspritzung stattfindet und bei drucklosem Einspritzsystem. Andererseits drückt sie, zusammen mit dem Brennstoffdruck, das obere Ende 96 der Steuerhülse 94 dauernd an den Steuerkörper 78 an.Bore 88 connected. A needle spring 90, a spring tensioning element, is located in the bore 88 92 and a control sleeve 94 guided in a narrow sliding manner in the control piston 38. Analogous to the solenoid valve spring 66, the spring tensioning element 92 serves to set a specific one Force of the needle spring 90. On the one hand, the needle spring 90 holds the nozzle needle in a known manner 32 in contact with the nozzle needle seat 28 when there is no injection and when there is no pressure Injection system. On the other hand, together with the fuel pressure, it pushes the upper end 96 of the control sleeve 94 continuously on the control body 78.

Die Steuerhülse 94 weist eine in die Bohrung 88 mündende Längsbohrung 98 auf. Eine erste Steuerbohrung 100 verbindet die Längsbohrung 98 mit dem Steuerraum 102. Mit einer Verbindung 104 ist der Steuerraum 102 mit der zweiten Steuerbohrung 106 verbunden. Mittels eines Flachsitzes 108 zwischen Steuerkörper 78 und Steuerventil 74 wird die Steuerbohrung 106 bei stromlosem Magnetventil 6 vom Steuerventil 74 gegen den hohen Systemdruck geschlossen gehalten. Der beim Anheben des Steuerventils 74 aus der zweiten Steuerbohrung 106 austretende Brennstoff wird, zusammen mit dem Leckbrennstoff, welcher von den beiden Führungsbohrungen 34 und 40 in den Ringraum 110 gelangt, mittels der Bohrung 112 (Fig. 1) auf bekannte Weise bei niedrigem Druck der Hochdruck-Fördereinrichtung zurückgeführt.The control sleeve 94 has a longitudinal bore 98 opening into the bore 88. A first one Control bore 100 connects the longitudinal bore 98 to the control chamber 102. With a connection 104, the control chamber 102 is connected to the second control bore 106. By means of a Flat seat 108 between the control body 78 and control valve 74, the control bore 106 at de-energized solenoid valve 6 closed by the control valve 74 against the high system pressure held. The one emerging from the second control bore 106 when the control valve 74 is raised Fuel is, together with the leak fuel, which from the two guide holes 34 and 40 enters the annular space 110, by means of the bore 112 (FIG. 1) to known ones Returned way at low pressure of the high pressure conveyor.

Wie in den Fig. 1 und 2 gezeigt, ist die Längsachse 114 der Aufnahmebohrung 58 des Magnetventils 6 gegenüber der dem Steuerkolben 38 und der Düsennadel 32 gemeinsamen Längsachse 116 desachsiert. Dies ist nur bei den gezeigten Dimensionen des Gehäuses 14 und des Magnetventils 6 erforderlich, um genügend Wandstärke für die Hochdruckbohrung 44 zur Verfügung zu stellen. Bei grösserer Dimensionierung des Gehäuses 14, oder kleinerer Dimensionierung des Magnetventils 6, können die zwei Längsachsen 114 und 116 auch übereinstimmen. Die Verbindung 104 im Steuerkörper 78 entfällt in diesem Fall.As shown in FIGS. 1 and 2, the longitudinal axis 114 is the receiving bore 58 of the solenoid valve 6 with respect to the longitudinal axis common to the control piston 38 and the nozzle needle 32 116 disaxed. This is only in the dimensions of the housing 14 and shown Solenoid valve 6 required to have enough wall thickness for the high pressure bore 44 available to deliver. With larger dimensions of the housing 14, or smaller dimensions of the solenoid valve 6, the two longitudinal axes 114 and 116 can also match. The connection 104 in the control body 78 is omitted in this case.

Gemäss den Fig. 2, 3a, 3b und 3c befindet sich zwischen der Stirnseite 118 des Steuerkolbens 38 und der Unterseite 120 des Steuerkörpers 78 ein ringförmiger Entlastungsraum 122. Der Steuerkolben 38 weist einen ringförmigen, auf dem Umfang nicht unterbrochenen Steg 124 auf. Ferner sind in den Fig. 3a, 3b und 3c die zwei ringförmige Leckspalte 126 (zwischen Steuerhülse 94 und Steuerkolben 38) und 128 (zwischen Steuerkolben 38 und Mittelteil 18) zur Verdeutlichung der Funktionsweise des Brennstoffeinspritzventils 1 übertrieben gross dargestellt.2, 3a, 3b and 3c is located between the front side 118 of the control piston 38 and the underside 120 of the control body 78 an annular relief chamber 122 Control piston 38 has an annular web 124 which is not interrupted on the circumference. 3a, 3b and 3c, the two annular leak gaps 126 (between the control sleeve 94 and control piston 38) and 128 (between control piston 38 and middle part 18) for clarification the operation of the fuel injector 1 shown exaggerated.

Die Funktionsweise des Brennstoffeinspritzventils 1 ist nun anhand der Fig. 1, 2, 3a, 3b und 3c wie folgt: bei Bestromung des Magnetventils 6 mit einem Stromimpuls bewegt sich der Steuerventilschaft 72 nach kurzer Zeit vom Flachsitz 108 weg und gibt die zweite Steuerbohrung 106 frei. Der Brennstoff-Steuerdruck in der Verbindung 104, im Steuerraum 102 und im Entlastungsraum 122 fällt ab. Dadurch kann einerseits die Einspritzung durch Anheben des Steuerkolbens 38 und der Düsennadel 32 weg vom Düsennadelsitz 28 beginnen. Dabei bewegt sich der Steuerkolben 38 relativ zum Mittelteil 18 und zur ortsfesten Steuerhülse 94 nach oben. Andererseits fliesst wegen dem nun tiefen Steuerdruck durch die erste Steuerbohrung 100 und durch die Leckspalte 126 und 128 Brennstoff in den Steuerraum 102, da der Brennstoffdruck in der Längsbohrung 98, in der Bohrung 88 und in der Nute 84 wesentlich höher als der Steuerdruck ist. Der gesamte in den Steuerraum 102 fliessende Brennstoff, fliesst durch die zweite Steuerbohrung 106 ab. Diese Phase wird in Fig. 3b gezeigt.The mode of operation of the fuel injection valve 1 is now based on FIGS. 1, 2, 3a, 3b and 3c as follows: when the solenoid valve 6 is energized with a current pulse, the control valve shaft moves 72 after a short time away from the flat seat 108 and gives the second control bore 106 free. The fuel control pressure in the connection 104, in the control chamber 102 and in the relief chamber 122 drops. On the one hand, this enables injection by lifting the control piston 38 and the nozzle needle 32 start away from the nozzle needle seat 28. The control piston moves 38 relative to the middle part 18 and the stationary control sleeve 94 upwards. on the other hand flows because of the now low control pressure through the first control bore 100 and through the Leakage gaps 126 and 128 fuel in the control room 102 because the fuel pressure in the Longitudinal bore 98, in the bore 88 and in the groove 84 significantly higher than the control pressure is. All of the fuel flowing into the control chamber 102 flows through the second control bore 106 onwards. This phase is shown in Fig. 3b.

Es ist von Vorteil, wenn der Brennstoffdurchfluss durch die Leckspalte 128 und 126 mengenmässig kleiner ist als jener durch die erste Steuerbohrung 100. Dies wird durch Realisation einer engen Gleitpassung (mit beispielsweise 1 bis 3 Mikrometer Spiel) zwischen den Teilen erzielt.It is advantageous if the fuel flow through the leakage gaps 128 and 126 is quantitative is smaller than that through the first control bore 100. This is achieved by realizing a tight sliding fit (with, for example, 1 to 3 micrometers of play) between the parts.

Bei grösser werdendem Hub der Düsennadel 32 nähert sich der Steg 124 des Steuerkolbens 38 der Unterseite 120 des Steuerkörpers 78. Damit wird der Brennstoffdurchfluss vom Entlastungsraum 122 über den Steg 124 in den Steuerraum 102 gedrosselt und bei vollem Hub der Düsennadel 32 stark reduziert. Der Druck im Entlastungsraum 122 steigt praktisch ohne Zeitverzögerung an und dementsprechend reduziert sich auch der Brennstoffdurchfluss des Leckspalts 128. Diese Phase bei voller Öffnung wird in Fig. 3c gezeigt. Im Grenzfall bildet der Steg 124 den mechanischen Hubanschlag von Düsennadel 32 und Steuerkolben 38. Durch Wahl des Aussenund Innendurchmessers sowie der Höhe des Steges 124 kann eine gewünschte Dämpfung am Ende der Öffnungsbewegung erzielt werden. Insbesondere kann die Höhe des Steges 124 nur wenige Hundertstel Millimeter betragen (beispielsweise 2 bis 10 Hundertstel). Das damit realisierte, sehr kleine Volumen des Entlastungsraumes 122 bewirkt, trotz geringer Zuströmmenge durch den Leckspalt 124, ein verzögerungsfreies Ansteigen des Druckes im Entlastungsraum 122.When the stroke of the nozzle needle 32 increases, the web 124 of the control piston 38 approaches the underside 120 of the control body 78. This means that the fuel flow from the relief chamber 122 throttled via the web 124 into the control chamber 102 and with a full stroke of the nozzle needle 32 greatly reduced. The pressure in the relief chamber 122 increases practically without a time delay and accordingly the fuel flow of the leakage gap 128 is also reduced. This full opening phase is shown in Fig. 3c. In the limit case, the web 124 forms the mechanical one Stroke stop of nozzle needle 32 and control piston 38. By selecting the outside and Internal diameter and the height of the web 124 can be a desired damping End of the opening movement can be achieved. In particular, the height of the web 124 can only amount to a few hundredths of a millimeter (for example 2 to 10 hundredths). That was realized causes very small volume of the relief space 122, despite the small inflow amount through the leakage gap 124, an instantaneous increase in the pressure in the relief space 122nd

Durch die erfindungsgemässe Ausführung mit dem Steg 124 am oberen Ende des Steuerkolbens 38 existiert das freie Ende des Steuerkolbens der früheren Konstruktionen nicht mehr. Ein Schwingen dieses freien Endes verschwindet damit. Da der Druck im Entlastungsraum 122 am Ende der Öffnungsbewegung wegen der Drosselwirkung des Steges 124 und der Leckspaltströmung über den Leckspalt 128 ohne Zeitverzögerung ansteigt, wird ein druckmässiger Kraftausgleich von Steuerkolben 38 und Düsennadel 32 sofort gewährleistet. Damit wird auch ein sicherer Beginn der Schliessbewegung möglich. Dies geschieht, wenn der Stromimpuls zum Magnetventil 6 unterbrochen wird und der Steuerventilschaft 72 die zweite Steuerbohrung 106 abschliesst. Die Nachteile der früheren Lösungen werden vermieden.Due to the design according to the invention with the web 124 at the upper end of the control piston 38 the free end of the spool of earlier designs no longer exists. On Swinging of this free end disappears with it. Since the pressure in the relief chamber 122 at End of the opening movement due to the throttling action of the web 124 and the leakage gap flow Rise over the leakage gap 128 without a time delay, a pressure equalization of force of control piston 38 and nozzle needle 32 guaranteed immediately. It also becomes a safe start of the closing movement possible. This happens when the current pulse to the Solenoid valve 6 is interrupted and the control valve stem 72, the second control bore 106 concludes. The disadvantages of the previous solutions are avoided.

Fig. 4 zeigt ein partieller Längsschnitt einer zweiten Ausführungsform eines Brennstoffeinspritzventils 2. Die nicht gezeigten Elemente können gleich sein, wie jene des Brennstoffeinspritzventils 1 nach Fig. 1. Gleiche Elemente wie in den Fig. 1 bis 3c oder solche, welche die exakt gleiche Funktion erfüllen, wurden in Fig. 4 mit denselben Ziffern versehen.Fig. 4 shows a partial longitudinal section of a second embodiment of a fuel injector 2. The elements not shown can be the same as those of the fuel injector 1 according to Fig. 1. Same elements as in Figs. 1 to 3c or those which are the exact perform the same function have been given the same numbers in FIG. 4.

Beim Brennstoffeinspritzventil 2 befindet sich der Steuerventilschaft 72 (und folglich das nicht gezeigte Magnetventil 6) auf der gleichen Längsachse 116 wie der Steuerkolben 130 und die Düsennadel 32. Der Steuerkörper 132 ist im Mittelteil 18 in analoger Art und Weise wie beim Brennstoffeinspritzventil 1 eingebaut. Die Steuerhülse 94 des Brennstoffeinspritzventils 1 entfällt beim Brennstoffeinspritzventil 2. Eine kurze Bohrung 142 verbindet die Nut 84 mit der ersten Steuerbohrung 100. Die Steuerbohrung 100 mündet in eine im Steuerkolben 130 angefertigte Längsbohrung 136, welche zusammen mit der Bohrung 134 im Steuerkörper 132 und dem Scheibenraum 138 den Steuerraum 140 bildet. Die Nadelfeder 144 befindet sich im unteren, verjüngten Teilstück 146 des Steuerkolbens 130 in einer Region bei niedrigem Brennstoffdruckpegel. Zwei Elemente 148a und 148b positionieren und spannen die Nadelfeder 144. Das verjüngte Teilstück 146 drückt auf die Stirnseite der Düsennadel 32.The control valve stem 72 is located in the fuel injector 2 (and therefore not shown solenoid valve 6) on the same longitudinal axis 116 as the control piston 130 and the Nozzle needle 32. The control body 132 is in the middle part 18 in an analogous manner to the Fuel injector 1 installed. The control sleeve 94 of the fuel injector 1 is omitted in the fuel injector 2. A short bore 142 connects the groove 84 with the first Control bore 100. The control bore 100 opens into a made in the control piston 130 Longitudinal bore 136, which together with the bore 134 in the control body 132 and the Disk space 138 forms the control space 140. The needle spring 144 is in the lower tapered portion 146 of spool 130 in a region with low fuel pressure level. Two elements 148a and 148b position and tension the needle spring 144. The tapered one Section 146 presses on the end face of the nozzle needle 32.

Durch das Wegfallen der Steuerhülse 94 wird dieser Bereich des Brennstoffeinspritzventils 2 vereinfacht. Das Anbringen der Nadelfeder 144 ausserhalb des Steuerkolben-Hochdruckbereichs ermöglicht eine freiere Gestaltung des Volumens des Steuerraumes 140 und der radialen Dimensionierung des Steges 124. Andererseits muss eine längere Ausführung des Mittelteils 18 in Kauf genommen werden. Die Funktionsweise des Brennstoffeinspritzventils 2 ist analog jener des Brennstoffeinspritzventils 1.By omitting the control sleeve 94, this area of the fuel injection valve 2 becomes simplified. Attaching the needle spring 144 outside the high pressure spool area enables a freer design of the volume of the control room 140 and the radial dimensioning of the web 124. On the other hand, a longer version of the middle part 18 are accepted. How the fuel injector works 2 is analogous to that of the fuel injection valve 1.

In einer alternativen, nicht gezeichnete Ausführungsform von Fig. 4, weist das Mittelteil 18 im unteren Bereich ein Gewinde auf, worauf die Überwurfmutter 16 geschraubt wird. Mit einer weiteren Mutter wird das Mittelteil 18 an das Gehäuse 14 geschraubt. Das Mittelteil 18 weist in diesem oberen Bereich einen Bund auf. Diese Ausführungsform ist günstig, wenn ein langes Brennstoffeinspritzventil verwendet werden muss.In an alternative, not shown embodiment of FIG. 4, the middle part 18 in the a lower thread on which the union nut 16 is screwed. With another The middle part 18 is screwed onto the housing 14. The middle part 18 points in this top a waistband. This embodiment is cheap if a long one Fuel injector must be used.

Fig. 5 zeigt ein partieller Längsschnitt einer dritten Ausführungsform eines Brennstoffeinspritzventils 3. Wiederum sind die nicht gezeigten Elemente gleich, wie jene des Brennstoffeinspritzventils 1 nach Fig. 1. Gleiche Elemente wie in den vorangehenden Figuren oder solche, welche die exakt gleiche Funktion erfüllen, wurden auch in Fig. 5 mit denselben Ziffern wie in den vorangehenden Figuren versehen.Fig. 5 shows a partial longitudinal section of a third embodiment of a fuel injector 3. Again, the elements not shown are the same as those of the fuel injector 1 according to Fig. 1. The same elements as in the preceding figures or those which perform exactly the same function, were also in Fig. 5 with the same digits as in the preceding Figures.

Wie in Fig. 4 befindet sich der Steuerventilschaft 72 auf der Längsachse 116. Eine scheibenförmige Zwischenplatte 150 befindet sich zwischen dem unteren Ende des Gehäuses 14 und dem Düsenkörper 22. Wie in Fig. 1 werden die Zwischenplatte 150 und der Düsenkörper 22 mittels der beiden Dichtflächen 20 und 24 von der Überwurfmutter 16 auf dichte Weise zusammengehalten. Die Brennstoffzufuhrbohrung 44 mündet in eine Bohrung 152 in der Zwischenplatte 150. Mit einer Aussparung 154 und einer schrägen Bohrung 156 wird in der Zwischenplatte 150 die erste Steuerbohrung 100 mit der Bohrung 152 verbunden. Anderseits mündet die erste Steuerbohrung 100 in eine auf der Längsachse 116 in der Zwischenplatte 150 angefertigten Bohrung 158. Die Bohrung 158 ist mit der zweiten Steuerbohrung 106 und mit einer im Steuerkolben 160 angefertigten Bohrung 162 verbunden.As in FIG. 4, the control valve stem 72 is located on the longitudinal axis 116. A disk-shaped one Intermediate plate 150 is located between the lower end of the housing 14 and the nozzle body 22. As in FIG. 1, the intermediate plate 150 and the nozzle body 22 held together by the union nut 16 in a sealed manner by means of the two sealing surfaces 20 and 24. The fuel supply bore 44 opens into a bore 152 in the intermediate plate 150. With a recess 154 and an oblique bore 156 is in the intermediate plate 150 the first control bore 100 is connected to the bore 152. On the other hand, the first control bore 100 in a on the longitudinal axis 116 in the intermediate plate 150 Bore 158. Bore 158 is with the second control bore 106 and with an in Control piston 160 connected bore 162 connected.

In einer nicht näher gezeigten Ausführungsform kann an Stelle der Zwischenplatte 150 ein eingepresstes Teil, ähnlich dem Steuerkörper 78 von Fig. 2 oder dem Steuerkörper 132 von Fig. 4, verwendet werden.In an embodiment not shown in detail, a pressed-in can be used instead of the intermediate plate 150 Part, similar to the control body 78 of FIG. 2 or the control body 132 of FIG. 4, be used.

Anders als bei den Brennstoffeinspritzventilen 1 und 2 ist nun der Steuerkolben 160 ein Stück mit der Düsennadel 32. Eine Nadelfeder 164 befindet sich, zusammen mit dem Federspannelement 166, in der Bohrung 162. Das Federspannelement 166 hat eine Nase 167, welche als Füllstück dient. Ohne die Nase 167 ist das Gesamtvolumen des Steuerraumes bestehend aus dem Brennstoffvolumen in der Bohrungen 158 und 162 je nach der Dimensionierung dieser Elemente ungünstig gross. Mit der Nase 167 kann es verkleinert werden. Abgesehen davon ist die Funktion dieser Elemente gleich wie vorhin.In contrast to fuel injection valves 1 and 2, control piston 160 is now one piece with the nozzle needle 32. A needle spring 164 is located together with the spring tensioning element 166, in the bore 162. The spring tensioning element 166 has a nose 167, which as Filler piece is used. Without the nose 167, the total volume of the control room consists of the fuel volume in the bores 158 and 162 depending on the dimensioning of these Elements unfavorably large. With the nose 167 it can be reduced. That being said the function of these elements the same as before.

Der Entlastungsraum 122 befindet sich wiederum zwischen dem am oberen Ende des Steuerkolbens 160 vorhandenen Steg 124 und der Nadelführungsbohrung 34. Der Leckbrennstoff fliesst nun während dem Einspritzvorgang vom Ringraum 52 im Düsenkörper 22 über den Leckspalt zwischen Steuerkolben 160 und Nadelführungsbohrung 34 in den Entlastungsraum 122. Die Funktionsweise des Brennstoffeinspritzventils 3 ist wiederum analog zu jener der vorherigen Ausführungen. Die Ausführung der Brennstoffeinspritzventils 3 ist besonders einfach.The relief chamber 122 is in turn between that at the upper end of the control piston 160 existing web 124 and the needle guide bore 34. The leak fuel now flows during the injection process from the annular space 52 in the nozzle body 22 over the Leakage gap between control piston 160 and needle guide bore 34 in the relief chamber 122. The mode of operation of the fuel injection valve 3 is again analogous to that of the previous one Versions. The design of the fuel injector 3 is particularly simple.

Eine Drosselbohrung 168 kann sich zwischen Bohrung 152 und Bohrung 48 befinden, jedoch nach dem Zulauf zur Bohrung 156. Diese Drosselbohrung 168 verursacht während dem Einspritzvorgang einen Druckabfall von beispielsweise 5-10% des Standdruckes und bewirkt auf bekannte Weise eine raschere Schliessbewegung der Düsennadel 32. A throttle bore 168 may be between bore 152 and bore 48, however after the inlet to the bore 156. This throttle bore 168 causes during the injection process a pressure drop of, for example, 5-10% of the standing pressure and causes a faster closing movement of the nozzle needle 32 in a known manner.

Fig. 6 stellt eine alternative Ausführungsform des Brennstoffeinspritzventils 3 von Fig. 5 dar. In dem Brennstoffeinspritzventil 3a von Fig. 6 wurde die Nadelfeder 164 in eine Bohrung 170 der Zwischenplatte 150 eingebaut. Das Federspannelement 166 von Fig. 5 wurde weggelassen, obschon es auch bei Fig. 6 entweder auf der Unterseite oder auf der Oberseite der Nadelfeder 164 eingebaut werden könnte. Die Drosselbohrung 168 ist nun Bestandteil der Zwischenplatte 150. Die Funktionsweise des Brennstoffeinspritzventils 3a ist gleich, wie jene des Brennstoffeinspritzventils 3.FIG. 6 shows an alternative embodiment of the fuel injection valve 3 from FIG. 5 6, the needle spring 164 was in a bore 170 of the Intermediate plate 150 installed. 5 has been omitted, although it is also in Fig. 6 either on the bottom or on the top of the needle spring 164 could be installed. The throttle bore 168 is now part of the intermediate plate 150. The operation of the fuel injector 3a is the same as that of the fuel injector Third

Bei weiteren, nicht gezeigte Ausführungsformen der Brennstoffeinspritzventile 3 und 3a kann ein Steuerkörper, analog wie der Steuerkörper 78 des Brennstoffeinspritzventils 1 oder wie der Steuerkörper 132 des Brennstoffeinspritzventils 2, entweder in das Gehäuse 14 oder in die Zwischenplatte 150 eingebaut werden. Dieser Steuerkörper kann entweder nur die zweite Steuerbohrung 106 oder auch die erste Steuerbohrung 100 aufweisen.In further, not shown embodiments of the fuel injection valves 3 and 3a can a control body, analogous to the control body 78 of the fuel injector 1 or like that Control body 132 of the fuel injector 2, either in the housing 14 or in the Intermediate plate 150 can be installed. This control body can either only be the second Have control bore 106 or the first control bore 100.

Wird ein Steuerkörper mit beiden Steuerbohrungen 100 und 106 in das Gehäuse 14 eingebaut, so kann die Zwischenplatte 150 des Brennstoffeinspritzventils 3a bei der mit einer gestrichelten Trennlinie 172 gezeigten Ebene beendet werden. in diesem Fall kann die Nadelfeder 164 von der Seite der Trennlinie 172 eingebaut werden. Wird sodann die Kraft der Nadelfeder 164 mit einem auf der Federunterseite angebrachten, schmalen Zapfen auf den Nadelkolben 160 übertragen, so kann die dem Steg 124 zugewandte Unterseite 120 der Zwischenplatte 150 mit einer kleineren Bohrung als die Bohrung 170 versehen werden, durch welche nur der schmale Zapfen ragt. Auf diese Weise erhält man, analog wie bei der Ausführung des Brennstoffeinspritzventils 2 von Fig. 4, eine grössere Freiheit bei der radialen Dimensionierung des Steges 124.If a control body with both control bores 100 and 106 is installed in the housing 14, the intermediate plate 150 of the fuel injector 3a can be shown with a dashed line Separation line 172 shown level are ended. in this case, the needle spring 164 of the side of the dividing line 172. Then the force of the needle spring 164 with transfer a narrow pin attached to the underside of the spring onto the needle piston 160, the underside 120 of the intermediate plate 150 facing the web 124 can be covered with a smaller bore than the bore 170 through which only the narrow pin protrudes. In this way you get, analogous to the design of the fuel injector 2 of FIG. 4, greater freedom in the radial dimensioning of the web 124.

Auch kann das Magnetventil 6 mit dem Steuerventilschaft 72 entweder wie bei den Figuren 5 und 6 auf der Längsachse 116 oder wie beim Brennstoffeinspritzventil 1 desachsiert ausgeführt werden.The solenoid valve 6 can also be operated with the control valve stem 72 either as in FIGS. 5 and 6 on the longitudinal axis 116 or, as in the case of the fuel injector 1, out of alignment become.

Claims (14)

  1. A fuel injection valve (1; 2; 3; 3a) for intermittent fuel injection into the combustion chamber of an internal combustion engine, with a housing (14), with a valve seat element (26) provided with injection apertures (30), with a longitudinally adjustable injection valve member (32) for closing or opening the injection apertures (30), with a control device for controlling the adjusting movement of the injection valve member (32), the control device having a longitudinally displaceable control piston (38; 130; 160) at least operatively connected to the injection valve member (32), which piston is acted upon by the fuel system pressure from a high-pressure feed line (42, 44, 46, 48) on the one hand and by the fuel control pressure in a control chamber (102, 104; 140; 158, 162; 170) on the other, the control chamber (102, 104; 140; 158, 162; 170) being connected by way of at least one first control aperture (100) to the high pressure feed line (42, 44, 46, 48), and the control pressure in the control chamber (102, 104; 140; 158, 162; 170) being controllable by opening or closing of at least one second control aperture (106), for which purpose an electrically controllable actuating element (6) is assigned to the control device, which element has an axially adjustable control valve element (72), which in its closed position seals off the second control aperture (106) and the opening movement of which, on activation of the actuating element (6), opens the second control aperture (106), and the control piston (38; 130; 160) is guided at its circumference by a tight sliding fit in a piston guide bore (40; 34) characterized in that the end of the control piston (38; 130; 160) facing the control chamber (102, 104; 140; 158, 162; 170) has an annular land (124), the control piston (38; 130; 160) is connected to the high-pressure feed line (42, 44, 46, 48) by way of the tight sliding fit in the piston guide bore (40; 34), and the tight sliding fit forms a leak gap (128), a relief chamber (122) is formed between the outlet side of the leak gap (128) and the land (124), and in that with the injection valve member (32) open, the land (124) reduces the flow of fuel from the relief chamber (122) into the control chamber (102, 104; 140; 158, 162; 170) by reducing the passage cross section, as a result of which the fuel pressure in the relief chamber (122) rises compared to the fuel pressure in the control chamber (102, 104; 140; 158, 162; 170).
  2. The fuel injection valve (1; 2) as claimed in claim 1, characterized in that the control piston (38; 130) is fitted in a middle part (18), which is situated between housing (14) and nozzle body (22) and is pressed tightly against the housing (14) and the nozzle body (22) by at least one retaining part (16).
  3. The fuel injection valve (1; 2) as claimed in claim 2, characterized in that the middle part (18) is provided with at least one high-pressure bore (46), which carries the fuel from the high-pressure bore (44) in the housing (14) to the high-pressure bore (48) in the nozzle body (22) and to the first control bore (100).
  4. The fuel injection valve (1; 2) as claimed in claim 2, characterized in that the middle part (18) has passages (112), in order to drain off leakage fuel, which collects in an annular chamber (110) below the control piston (38; 130), at low pressure from the annular chamber (110).
  5. The fuel injection valve (1; 2) as claimed in claims 1 or 2, characterized in that a control body (78; 132) is tightly fitted in the housing (14) or in the middle part (18), the control body (78; 132) is provided with an underside (120), which together with the land (124) forms the stroke limit of the control piston (38; 130).
  6. The fuel injection valve (1; 2) as claimed in claim 5, characterized in that the control body (78; 132) is provided with the second control bore (106).
  7. The fuel injection valve (1) as claimed in claim 1, characterized in that the actuating element (6) is axially offset in relation to a longitudinal axis (116) common to the control piston (38) and the injection valve member (32).
  8. The fuel injection valve (3, 3a) as claimed in claim 1, characterized in that the control piston (160) is integral with the nozzle needle (32) and is guided in a guide bore (34) with tight slide fit in the nozzle body (22).
  9. The fuel injection valve (3) as claimed in claim 8, characterized in that the control piston (160) is provided with a bore (162) containing a spring (164), acting in the closing direction of the injection valve member, and a spring tensioning element (166) for setting the required spring loading.
  10. The fuel injection valve (3, 3a) as claimed in claim 1, characterized in that a restriction (168) is situated between the high-pressure bore (44) and the high-pressure bore (48), but downstream of the admission inlet (156) to the first control bore (100).
  11. The fuel injection valve (3, 3a) as claimed in claim 1, characterized in that an intermediate plate (150) is located between housing (14) and nozzle body (22) and is tightly pressed against the housing (14) and the nozzle body (22) by a retaining part (16), the intermediate plate (150) has at least one fuel passage (152) from the high-pressure bore (44) to the high-pressure bore (48) and the second control bore (106).
  12. The fuel injection valve (3, 3a) as claimed in claims 10 and 11, characterized in that the restriction (168) is situated in the intermediate plate (150).
  13. The fuel injection valve (3, 3a) as claimed in claim 11, characterized in that the intermediate plate (150) has the first control bore (100).
  14. The fuel injection valve as claimed in claim 11, characterized in that an underside (120) of the intermediate plate (150) forms the stroke limit of the control piston (160).
EP99947182A 1998-11-10 1999-10-21 Fuel injection valve for internal combustion engines Expired - Lifetime EP1131552B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH225198 1998-11-10
CH225198 1998-11-10
PCT/CH1999/000499 WO2000028205A1 (en) 1998-11-10 1999-10-21 Fuel injection valve for internal combustion engines

Publications (2)

Publication Number Publication Date
EP1131552A1 EP1131552A1 (en) 2001-09-12
EP1131552B1 true EP1131552B1 (en) 2002-11-27

Family

ID=4229407

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99947182A Expired - Lifetime EP1131552B1 (en) 1998-11-10 1999-10-21 Fuel injection valve for internal combustion engines

Country Status (6)

Country Link
US (1) US6405941B2 (en)
EP (1) EP1131552B1 (en)
JP (1) JP2002529654A (en)
AT (1) ATE228614T1 (en)
DE (1) DE59903599D1 (en)
WO (1) WO2000028205A1 (en)

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WO2008046238A2 (en) * 2006-10-16 2008-04-24 Ganser-Hydromag Ag Fuel injection valve for internal combustion engines
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Also Published As

Publication number Publication date
US6405941B2 (en) 2002-06-18
JP2002529654A (en) 2002-09-10
WO2000028205A1 (en) 2000-05-18
ATE228614T1 (en) 2002-12-15
US20020008156A1 (en) 2002-01-24
DE59903599D1 (en) 2003-01-09
EP1131552A1 (en) 2001-09-12

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