EP1304476A2 - High pressure resistant injector body - Google Patents

High pressure resistant injector body Download PDF

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Publication number
EP1304476A2
EP1304476A2 EP02015756A EP02015756A EP1304476A2 EP 1304476 A2 EP1304476 A2 EP 1304476A2 EP 02015756 A EP02015756 A EP 02015756A EP 02015756 A EP02015756 A EP 02015756A EP 1304476 A2 EP1304476 A2 EP 1304476A2
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EP
European Patent Office
Prior art keywords
valve chamber
injector body
inlet opening
bulges
inlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP02015756A
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German (de)
French (fr)
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EP1304476B1 (en
EP1304476A3 (en
Inventor
Martin Grieb
Stefan Haug
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Robert Bosch GmbH
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Robert Bosch GmbH
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Publication date
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Publication of EP1304476A2 publication Critical patent/EP1304476A2/en
Publication of EP1304476A3 publication Critical patent/EP1304476A3/en
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Publication of EP1304476B1 publication Critical patent/EP1304476B1/en
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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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/168Assembling; Disassembling; Manufacturing; Adjusting
    • 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
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/008Arrangement of fuel passages inside of injectors
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/03Fuel-injection apparatus having means for reducing or avoiding stress, e.g. the stress caused by mechanical force, by fluid pressure or by temperature variations
    • 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 an injector body for a Fuel injection system, wherein the injector body one essentially cylindrical valve chamber has in the via an inlet bore in a Inlet opening in the valve compartment opens, fuel under High pressure can be introduced.
  • Such injector bodies for fuel injection systems have a substantially cylindrical shape Valve chamber, in the wall of which an inlet opening Inlet bore comes to rest.
  • the inlet bore is in place for its part in connection with a pressure connection at which the supply line for fuel under high pressure flows out of a high-pressure collecting space.
  • the High pressure resistance of the injector body depends on the The geometry of the inlet area is crucial.
  • the Intersection of the inlet bore with the valve chamber is the most stressed part.
  • One of the parameters is here the inlet angle of the inlet bore from High pressure manifold (common rail) in the injector body. Is this angle between the central axis of the Inlet bore and longitudinal axis of the valve chamber about 90 °, the stresses in the intersection area can be low being held.
  • the installation conditions on the cylinder head However, an internal combustion engine does not always allow Entry angle of 90 °.
  • the Valve space at least in the area of the inlet opening of the Inlet bore to the valve chamber in the circumferential direction adjacent to this inlet opening, a bulge of the Cross section on. So it comes from both sides of the Inlet opening in the valve chamber for an increase in volume.
  • Is the entry angle (angle between the central axis the inlet bore and the longitudinal axis of the valve chamber) 90 ° are the bulges proposed according to the invention of the valve chamber cross section advantageously in one Plane perpendicular to the longitudinal axis of the valve space.
  • the longitudinal direction of the valve chamber extends Bulge at least over the area of the inlet opening.
  • the plane in which the bulges lie in orientate in the same way as the inlet bore so that the center line of the inlet bore through this plane runs.
  • the bulges in the Cross section perpendicular to the longitudinal axis of the valve chamber to install.
  • valve chambers are cylindrical in shape accordingly have a circular cross section (perpendicular to the longitudinal axis of the valve chamber).
  • the Bulges according to the invention run in the area of Inlet opening of the inlet hole in each case in the circumferential direction of the valve chamber adjacent to the inlet opening, so that the Bulges to deviate from the circular Cross section. It has been shown that a large Strength increases when there is a bulge extends at least to a level defined by the Inlet opening and parallel to the longitudinal axis of the valve chamber runs. Again, it is particularly advantageous if the bulges are arranged symmetrically to the inlet opening are. Extend the bulges over the above Level out, so that arise under internal pressure Bending compressive stresses in the area of the inlet opening Even better compensate for notch tension stresses that occur.
  • the invention proposed bulges up to the above Plane parallel to the longitudinal axis of the valve space and extends through the inlet opening, is it is advantageous if the valve chamber cross-section is even is continued up to the named level, the Diameter then the maximum diameter of the valve space can correspond. With such a configuration showed that a further increase in strength can be achieved if the inlet bore is eccentric in with respect to the valve chamber.
  • FIG. 1 The essential structure of an injector body 1 is shown in FIG. 1 in a section through the longitudinal axis of the injector body 1.
  • the injector body 1 essentially comprises one cylindrical valve chamber 3, in the wall of which one Inlet opening 7 for the supply of high pressure standing fuel. This inlet opening 7 forms the mouth of the inlet bore 2 in the valve chamber 3. Die Inlet bore 2 leads to the pressure connection 5 to which the High pressure manifold (common rail) connects.
  • the injector body in turn has an internal thread 4 Connection to the injection system.
  • the entry angle i.e. the angle between Longitudinal axis of the valve chamber 3 and central axis of the Inlet bore 2, in the illustration according to FIG. 1 Although less than 90 °, it is still in the area above 75 °, i.e. in an area in which one tension-reducing effect through the entry angle given is.
  • FIG. 2A is a highly schematized one according to the invention Injector body 1 in the same way as from Fig. 1 shown. The same elements are the same Provide reference numerals.
  • the inlet hole 2 leads here in the right angle to the valve chamber 3 of the injector body 1.
  • FIG. 2A are those in the plane Bulges 8 of the perpendicular to the plane of the drawing Valve chamber cross section hardly due to the type of representation recognizable.
  • FIG. 2B shows Section along the line A-A of Fig. 2A in a clear manner the bulges 8 according to the invention on both sides of the Inlet opening 7 of the inlet hole 2.
  • the bulges 8 of the valve chamber cross section are in this example symmetrical to the inlet opening 7 and are wide led back towards the inlet hole.
  • the bulges 8 change the Cross section of the valve chamber 3 at least in the area of Inlet opening 7 such that the original circular cross section only in the inlet opening 7 opposite half of the valve chamber 3 maintained while in the other half with the valve compartment maximum diameter up to a plane 9 that is parallel to the longitudinal axis 10 of the valve chamber 3 and through the Inlet opening 7 runs, is continued and above in addition two symmetrical to the center line of the inlet bore 2 and has indentations lying behind level 9.
  • the bulges 8 shown lead to a Deformation of the valve chamber 3 under internal pressure with a Training of bending pressure and circumferential tensile stresses in Area of the bulges 8, the notch tension in the Reduce intersection area 6. So overall it comes for a partial compensation of the occurring Voltages so that the maximum voltage in Intersection area 6 is reduced.
  • FIG. 2C shows a section along the line B-B from FIG. 2 B. This results in the course of the bulges 8 in Longitudinal direction of the valve chamber 3.
  • the bulges 8 focus on the area of the inlet opening 7 and take on both sides in the longitudinal direction of the valve chamber 3 off again, so that the valve chamber 3 there its original takes cylindrical shape again.
  • FIG. 3 Another embodiment of the invention is shown in FIG. 3 shown schematically.
  • the eccentric The arrangement of the inlet bore 2 has this Embodiment as a further strength-increasing Measure proven.
  • the invention can be different Geometries of valve chamber cross sections in the area of Inlet opening to be specified, leading to a reduction the stresses occurring in the intersection area and thus to an increase in the high pressure resistance of the Guide injector body. Especially at High-pressure fuel injectors can be used with it Achieve success.

Abstract

The high pressure injector body (1) has an essentially cylindrical valve chamber (3) into which fuel can be introduced at high pressure via a feed bore (2) opening into a feed opening (7) in the valve chamber. The valve chamber has a bulge in its cross-section, at least near the feed opening and adjacent to the feed opening in the peripheral direction.

Description

Die Erfindung betrifft einen Injektorkörper für ein Kraftstoffeinspritzsystem, wobei der Injektorkörper einen im wesentlichen zylindrisch ausgestalteten Ventilraum aufweist, in den über eine Zulaufbohrung, die in einer Zulauföffnung im Ventilraum mündet, Kraftstoff unter Hochdruck einleitbar ist.The invention relates to an injector body for a Fuel injection system, wherein the injector body one essentially cylindrical valve chamber has in the via an inlet bore in a Inlet opening in the valve compartment opens, fuel under High pressure can be introduced.

Stand der TechnikState of the art

Derartige Injektorkörper für Kraftstoffeinspritzsysteme besitzen einen im wesentlichen zylindrisch ausgeformten Ventilraum, in dessen Wandung die Zulauföffnung einer Zulaufbohrung zu liegen kommt. Die Zulaufbohrung steht ihrerseits mit einem Druckanschluß in Verbindung, an dem die Zuleitung für unter hohem Druck stehenden Kraftstoff aus einem Hochdrucksammelraum mündet. Die Hochdruckfestigkeit des Injektorkörpers hängt von der Geometrie des Zulaufbereichs entscheidend ab. Die Verschneidung der Zulaufbohrung mit dem Ventilraum stellt die höchstbelastete Stelle dar. Einer der Parameter ist hier der Einlaufwinkel der Zulaufbohrung vom Hochdrucksammelraum (Common Rail) in den Injektorkörper. Beträgt dieser Winkel zwischen Mittelachse der Zulaufbohrung und Längsachse des Ventilraums etwa 90°, können die Beanspruchungen im Verschneidungsbereich gering gehalten werden. Die Einbauverhältnisse am Zylinderkopf einer Verbrennungskraftmaschine erlaubt jedoch nicht immer Einlaufwinkel von 90°.Such injector bodies for fuel injection systems have a substantially cylindrical shape Valve chamber, in the wall of which an inlet opening Inlet bore comes to rest. The inlet bore is in place for its part in connection with a pressure connection at which the supply line for fuel under high pressure flows out of a high-pressure collecting space. The High pressure resistance of the injector body depends on the The geometry of the inlet area is crucial. The Intersection of the inlet bore with the valve chamber is the most stressed part. One of the parameters is here the inlet angle of the inlet bore from High pressure manifold (common rail) in the injector body. Is this angle between the central axis of the Inlet bore and longitudinal axis of the valve chamber about 90 °, the stresses in the intersection area can be low being held. The installation conditions on the cylinder head However, an internal combustion engine does not always allow Entry angle of 90 °.

Die Hauptbeanspruchung der Verschneidungsstelle wird durch den anliegenden Innendruck hervorgerufen. Unter diesem Innendruck führt die Kerbwirkung der Zulaufbohrung im Verschneidungsbereich der Bohrungen zu hohen lokalen Kerbzugspannungen in Umfangsrichtung des Ventilraumes. Auch bei optimalem Einlaufwinkel sind die genannten Zugspannungen der begrenzende Faktor für die Hochdruckfestigkeit des Injektorkörpers.The main stress on the intersection is by the applied internal pressure. Under this Internal pressure leads to the notch effect of the inlet bore in the Intersection area of the holes to high local Notch tension in the circumferential direction of the valve space. Also with an optimal entry angle, these are Tension is the limiting factor for the High pressure resistance of the injector body.

Es stellt sich folglich das Problem, die Kerbzugspannungen in Umfangsrichtung des Ventilraumes bei einem gattungsgemäßen Injektorkörper herabzusetzen, um diesen für höhere Druckbelastungen auslegen zu können.The problem then arises, the notch tension in the circumferential direction of the valve chamber at one Generic injector body to reduce this for to be able to design higher pressure loads.

Vorteile der ErfindungAdvantages of the invention

Bei der erfindungsgemäß vorgeschlagenen Lösung weist der Ventilraum zumindest im Bereich der Zulauföffnung der Zulaufbohrung zum Ventilraum jeweils in Umfangsrichtung benachbart zu dieser Zulauföffnung eine Ausbuchtung des Querschnitts auf. Somit kommt es beiderseits der Zulauföffnung im Ventilraum zu einer Volumenvergrößerung. Hierdurch verformt sich der Ventilraum im Verschneidungsbereich der Bohrungen unter Innendruck derart, daß es durch die stärkere Krümmung im Bereich der Hochdruckverschneidung zu einer Überlagerung von Biegedruck- und Umfangszugspannungen kommt, welche wiederum die Kerbzugspannungen im Verschneidungsbereich der beiden Bohrungen (Zulaufbohrung und Ventilraumbohrung) verringert.In the solution proposed according to the invention, the Valve space at least in the area of the inlet opening of the Inlet bore to the valve chamber in the circumferential direction adjacent to this inlet opening, a bulge of the Cross section on. So it comes from both sides of the Inlet opening in the valve chamber for an increase in volume. This deforms the valve chamber in the Intersection area of the holes under internal pressure such that it is due to the greater curvature in the area of High pressure blending to an overlay of Bending pressure and circumferential tensile stresses come, which in turn the notch tensile stresses in the intersection area of the two Bores (inlet bore and valve chamber bore) reduced.

Vorteilhaft sind hierbei zu beiden Seiten der Zulauföffnung symmetrisch geformte Ausbuchtungen. Durch diese Symmetrie können sich auftretende Spannungen optimal kompensieren.This is advantageous on both sides of the inlet opening symmetrically shaped bulges. Because of this symmetry can optimally compensate for occurring tensions.

Beträgt der Einlaufwinkel (Winkel zwischen der Mittelachse der Zulaufbohrung und der Längsachse des Ventilraums) 90°, liegen die erfindungsgemäß vorgeschlagenen Ausbuchtungen des Ventilraumquerschnitts vorteilhafterweise in einer Ebene senkrecht zur Längsachse des Ventilraums. In Längsrichtung des Ventilraums erstreckt sich die Ausbuchtung zumindest über den Bereich der Zulauföffnung. Bei anderen Einlaufwinkeln als 90°, kann es vorteilhaft sein, die Ebene, in der die Ausbuchtungen liegen, in gleicher Weise wie die Zulaufbohrung zu orientieren, so daß die Mittellinie der Zulaufbohrung durch diese Ebene verläuft. Meist ist es jedoch ausreichend und herstellungstechnisch einfacher, die Ausbuchtungen im Querschnitt senkrecht zur Längsachse des Ventilraums anzubringen.Is the entry angle (angle between the central axis the inlet bore and the longitudinal axis of the valve chamber) 90 °, are the bulges proposed according to the invention of the valve chamber cross section advantageously in one Plane perpendicular to the longitudinal axis of the valve space. In The longitudinal direction of the valve chamber extends Bulge at least over the area of the inlet opening. With entry angles other than 90 °, it can be advantageous be, the plane in which the bulges lie, in orientate in the same way as the inlet bore so that the center line of the inlet bore through this plane runs. However, it is usually sufficient and technically simpler, the bulges in the Cross section perpendicular to the longitudinal axis of the valve chamber to install.

Die in den meisten Fällen zylindrisch geformten Ventilräume besitzen demgemäß einen kreisförmigen Querschnitt (senkrecht zur Längsachse des Ventilraums). Die erfindungsgemäßen Ausbuchtungen verlaufen im Bereich der Zulauföffnung der Zulaufbohrung jeweils in Umfangsrichtung des Ventilraums benachbart zur Zulauföffnung, so daß die Ausbuchtungen zu einem Abweichen vom kreisförmigen Querschnitt führen. Es hat sich gezeigt, daß eine große Festigkeitssteigerung eintritt, wenn eine Ausbuchtung sich mindestens bis zu einer Ebene erstreckt, die durch die Zulauföffnung sowie parallel zur Längsachse des Ventilraums verläuft. Hierbei ist es wieder besonders vorteilhaft, wenn die Ausbuchtungen symmetrisch zur Zulauföffnung angeordnet sind. Erstrecken sich die Ausbuchtungen über die genannte Ebene hinaus, so können die unter Innendruck entstehenden Biegedruckspannungen im Bereich der Zulauföffnung die auftretenden Kerbzugspannungen noch besser kompensieren.In most cases the valve chambers are cylindrical in shape accordingly have a circular cross section (perpendicular to the longitudinal axis of the valve chamber). The Bulges according to the invention run in the area of Inlet opening of the inlet hole in each case in the circumferential direction of the valve chamber adjacent to the inlet opening, so that the Bulges to deviate from the circular Cross section. It has been shown that a large Strength increases when there is a bulge extends at least to a level defined by the Inlet opening and parallel to the longitudinal axis of the valve chamber runs. Again, it is particularly advantageous if the bulges are arranged symmetrically to the inlet opening are. Extend the bulges over the above Level out, so that arise under internal pressure Bending compressive stresses in the area of the inlet opening Even better compensate for notch tension stresses that occur.

In einer Ausgestaltung, bei der die erfindungsgemäß vorgeschlagenen Ausbuchtungen sich bis zu der obengenannten Ebene, die parallel zur Längsachse des Ventilraums und durch die Zulauföffnung hindurch verläuft, erstrecken, ist es vorteilhaft, wenn der Ventilraumquerschnitt gleichmäßig bis zu der genannten Ebene fortgeführt wird, wobei der Durchmesser dann dem maximalen Durchmesser des Ventilraums entsprechen kann. Bei einer derartigen Ausgestaltung hat sich gezeigt, daß eine weitere Festigkeitssteigerung erzielt werden kann, wenn die Zulaufbohrung exzentrisch in bezug auf den Ventilraum verläuft.In an embodiment in which the invention proposed bulges up to the above Plane parallel to the longitudinal axis of the valve space and extends through the inlet opening, is it is advantageous if the valve chamber cross-section is even is continued up to the named level, the Diameter then the maximum diameter of the valve space can correspond. With such a configuration showed that a further increase in strength can be achieved if the inlet bore is eccentric in with respect to the valve chamber.

Zeichnungdrawing

Im folgenden sollen Ausführungsbeispiele die Erfindung anhand der beigefügten Figuren näher erläutern.The following are exemplary embodiments of the invention explain in more detail with reference to the accompanying figures.

Es zeigenShow it

Fig. 1Fig. 1
den Schnitt durch die Längsachse eines Injektorkörpers für ein Kraftstoff-Hochdruckeinspritzsystem,the section through the longitudinal axis of a Injector body for a high-pressure fuel injection system,
Fig. 2 AFig. 2A
einen erfindungsgemäßen Injektorkörper in stark schematisierter Form im Längsschnitt, an injector body according to the invention in strong schematic form in longitudinal section,
Fig. 2 BFig. 2B
den Schnitt durch die Linie A-A aus Fig. 2 A,the section through the line A-A of Fig. 2 A,
Fig. 2 CFig. 2C
den Schnitt durch die Linie B-B aus Fig. 2 B undthe section through the line B-B of Fig. 2 B and
Fig. 3Fig. 3
eine weitere Ausführungsform des erfindungsgemäßen Injektorkörpers in der gleichen Darstellung wie Fig. 3.a further embodiment of the injector body according to the invention in the same Representation as Fig. 3rd
Bevorzugte AusführungsbeispielePreferred embodiments

Den wesentlichen Aufbau eines Injektorkörpers 1 zeigt Fig. 1 in einem Schnitt durch die Längsachse des Injektorkörpers 1.The essential structure of an injector body 1 is shown in FIG. 1 in a section through the longitudinal axis of the injector body 1.

Der Injektorkörper 1 umfaßt einen im wesentlichen zylindrischen Ventilraum 3, in dessen Wandung sich eine Zulauföffnung 7 für die Zuleitung von unter hohem Druck stehenden Kraftstoff befindet. Diese Zulauföffnung 7 bildet die Mündung der Zulaufbohrung 2 in den Ventilraum 3. Die Zulaufbohrung 2 führt zum Druckanschluß 5, an den sich der Hochdrucksammelraum (Common Rail) anschließt. Der Injektorkörper weist seinerseits ein Innengewinde 4 zum Anschluß an das Einspritzsystem auf.The injector body 1 essentially comprises one cylindrical valve chamber 3, in the wall of which one Inlet opening 7 for the supply of high pressure standing fuel. This inlet opening 7 forms the mouth of the inlet bore 2 in the valve chamber 3. Die Inlet bore 2 leads to the pressure connection 5 to which the High pressure manifold (common rail) connects. The The injector body in turn has an internal thread 4 Connection to the injection system.

Im Verschneidungsbereich 6 der Zulaufbohrung 2 zum Ventilraum 3 kommt es aufgrund der hohen Kraftstoffdrücke zu starken Belastungen. Bei hohen Innendrücken führt die Kerbwirkung der Zulaufbohrung 2 im Verschneidungsbereich 6 zu hohen lokalen Kerbzugspannungen in Umfangrichtung des Ventilraums 3, so daß die Gefahr von Rissbildung besteht. Sich ausbildende Risse führen letztendlich zu einem Ausfall des Injektors. Der Einlaufwinkel, also der Winkel zwischen Längsachse des Ventilraums 3 und Mittelachse der Zulaufbohrung 2, beträgt in der Darstellung nach Fig. 1 zwar weniger als 90°, liegt jedoch noch im Bereich oberhalb 75°, also in einem Bereich, in dem eine spannungsreduzierende Wirkung durch den Einlaufwinkel gegeben ist.In the intersection area 6 of the inlet bore 2 to Valve space 3 occurs due to the high fuel pressures too heavy loads. At high internal pressures, the Notch effect of the inlet bore 2 in the intersection area 6 too high local notch tensile stresses in the circumferential direction of the Valve chamber 3, so that there is a risk of cracking. Cracks that form ultimately lead to failure of the injector. The entry angle, i.e. the angle between Longitudinal axis of the valve chamber 3 and central axis of the Inlet bore 2, in the illustration according to FIG. 1 Although less than 90 °, it is still in the area above 75 °, i.e. in an area in which one tension-reducing effect through the entry angle given is.

In Fig. 2 A ist stark schematisiert ein erfindungsgemäßer Injektorkörper 1 in der gleichen Betrachtungsweise wie aus Fig. 1 dargestellt. Gleiche Elemente sind mit gleichen Bezugszeichen versehen. Die Zulaufbohrung 2 führt hier im rechten Winkel zum Ventilraum 3 des Injektorkörpers 1. In der Darstellung der Fig. 2 A sind die in der Ebene senkrecht zur Zeichenebene liegenden Ausbuchtungen 8 des Ventilraumquerschnitts aufgrund der Darstellungsart kaum erkennbar. Hingegen zeigt der in Fig. 2 B dargestellte Schnitt entlang der Linie A-A aus Fig. 2 A in klarer Weise die erfindungsgemäßen Ausbuchtungen 8 zu beiden Seiten der Zulauföffnung 7 der Zulaufbohrung 2. Die Ausbuchtungen 8 des Ventilraumquerschnitts sind in diesem Beispiel symmetrisch zur Zulauföffnung 7 ausgebildet und sind weit nach hinten in Richtung Zulaufbohrung geführt. Wie aus Fig. 2 B ersichtlich, verändern die Ausbuchtungen 8 den Querschnitt des Ventilraums 3 zumindest im Bereich der Zulauföffnung 7 dergestalt, daß der ursprünglich kreisförmige Querschnitt nur noch in der der Zulauföffnung 7 gegenüberliegenden Hälfte des Ventilraums 3 beibehalten wird, während in der anderen Hälfte der Ventilraum mit maximalem Durchmesser bis zu einer Ebene 9, die parallel zur Längsachse 10 des Ventilraums 3 und durch die Zulauföffnung 7 verläuft, fortgeführt wird und darüber hinaus zwei symmetrisch zur Mittellinie der Zulaufbohrung 2 und hinter der Ebene 9 liegende Einbuchtungen aufweist.2A is a highly schematized one according to the invention Injector body 1 in the same way as from Fig. 1 shown. The same elements are the same Provide reference numerals. The inlet hole 2 leads here in the right angle to the valve chamber 3 of the injector body 1. In the representation of FIG. 2A are those in the plane Bulges 8 of the perpendicular to the plane of the drawing Valve chamber cross section hardly due to the type of representation recognizable. In contrast, the one shown in FIG. 2B shows Section along the line A-A of Fig. 2A in a clear manner the bulges 8 according to the invention on both sides of the Inlet opening 7 of the inlet hole 2. The bulges 8 of the valve chamber cross section are in this example symmetrical to the inlet opening 7 and are wide led back towards the inlet hole. As from Fig. 2 B visible, the bulges 8 change the Cross section of the valve chamber 3 at least in the area of Inlet opening 7 such that the original circular cross section only in the inlet opening 7 opposite half of the valve chamber 3 maintained while in the other half with the valve compartment maximum diameter up to a plane 9 that is parallel to the longitudinal axis 10 of the valve chamber 3 and through the Inlet opening 7 runs, is continued and above in addition two symmetrical to the center line of the inlet bore 2 and has indentations lying behind level 9.

Die dargestellten Ausbuchtungen 8 führen zu einer Verformung des Ventilraums 3 unter Innendruck mit einer Ausbildung von Biegedruck- und Umfangszugspannungen im Bereich der Ausbuchtungen 8, die die Kerbzugspannungen im Verschneidungsbereich 6 verringern. Insgesamt kommt es also zu einer teilweisen Kompensation der auftretenden Spannungen, so daß die Maximalspannung im Verschneidungsbereich 6 reduziert wird.The bulges 8 shown lead to a Deformation of the valve chamber 3 under internal pressure with a Training of bending pressure and circumferential tensile stresses in Area of the bulges 8, the notch tension in the Reduce intersection area 6. So overall it comes for a partial compensation of the occurring Voltages so that the maximum voltage in Intersection area 6 is reduced.

Fig. 2 C zeigt einen Schnitt entlang der Linie B-B aus Fig. 2 B. Hieraus ergibt sich der Verlauf der Ausbuchtungen 8 in Längsrichtung des Ventilraums 3. Die Ausbuchtungen 8 konzentrieren sich auf den Bereich der Zulauföffnung 7 und nehmen zu beiden Seiten in Längsrichtung des Ventilraums 3 wieder ab, so daß der Ventilraum 3 dort seine ursprüngliche zylinderförmige Gestalt wieder einnimmt.FIG. 2C shows a section along the line B-B from FIG. 2 B. This results in the course of the bulges 8 in Longitudinal direction of the valve chamber 3. The bulges 8 focus on the area of the inlet opening 7 and take on both sides in the longitudinal direction of the valve chamber 3 off again, so that the valve chamber 3 there its original takes cylindrical shape again.

Eine weitere Ausführungsform der Erfindung ist in Fig. 3 schematisch dargestellt. Auch hier weist der Ventilraum 3 Ausbuchtung 8 zu beiden Seiten der Zulauföffnung 7 auf, so daß insgesamt ein symmetrischer Querschnitt des Ventilinnenraums 3 entsteht, wobei hier eine Verbreiterung des ursprünglich kreisförmigen Querschnitts auf einen Querschnitt mit konstantem Durchmesser, der dem des kreisförmigen Ventilraums 3 entspricht, bis zu der Ebene 9 stattfindet, die parallel zur Längsachse 10 des Ventilraums 3 und durch die Zulauföffnung 7 verläuft. Die exzentrische Anordnung der Zulaufbohrung 2 hat sich bei diesem Ausführungsbeispiel als weitere festigkeitssteigernde Maßnahme bewährt.Another embodiment of the invention is shown in FIG. 3 shown schematically. Here too, the valve chamber 3 Bulge 8 on both sides of the inlet opening 7, see above that overall a symmetrical cross section of the Valve interior 3 arises, with a widening here of the originally circular cross-section to one Cross section with constant diameter, that of the corresponds to circular valve chamber 3, up to level 9 takes place, which is parallel to the longitudinal axis 10 of the valve chamber 3 and runs through the inlet opening 7. The eccentric The arrangement of the inlet bore 2 has this Embodiment as a further strength-increasing Measure proven.

Insgesamt können durch die Erfindung verschiedene Geometrien von Ventilraumquerschnitten im Bereich der Zulauföffnung angegeben werden, die zu einer Verminderung der auftretenden Spannungen im Verschneidungsbereich und somit zu einer Steigerung der Hochdruckfestigkeit des Injektorkörpers führen. Insbesondere bei Hochdruckkraftstoffinjektoren lassen sich damit gute Erfolge erzielen.Overall, the invention can be different Geometries of valve chamber cross sections in the area of Inlet opening to be specified, leading to a reduction the stresses occurring in the intersection area and thus to an increase in the high pressure resistance of the Guide injector body. Especially at High-pressure fuel injectors can be used with it Achieve success.

Claims (6)

Injektorkörper für ein Kraftstoffeinspritzsystem, wobei der Injektorkörper (1) einen im wesentlichen zylindrisch geformten Ventilraum (3) aufweist, in den über eine Zulaufbohrung (2), die in einer Zulauföffnung (7) im Ventilraum (3) mündet, Kraftstoff unter Hochdruck einleitbar ist,
dadurch gekennzeichnet, daß der Ventilraum (3) zumindest im Bereich der Zulauföffnung (7) jeweils in Umfangsrichtung benachbart zur Zulauföffnung (7) eine Ausbuchtung (8) seines Querschnitts aufweist.
Injector body for a fuel injection system, the injector body (1) having an essentially cylindrically shaped valve chamber (3) into which fuel can be introduced under high pressure via an inlet bore (2) which opens into an inlet opening (7) in the valve chamber (3) .
characterized in that the valve chamber (3) has a bulge (8) in its cross section at least in the area of the inlet opening (7) in the circumferential direction adjacent to the inlet opening (7).
Injektorkörper nach Anspruch 1, dadurch gekennzeichnet, daß die Ausbuchtungen (8) symmetrisch zur Mittellinie der Zulaufbohrung (2) liegen.Injector body according to claim 1, characterized in that the bulges (8) are symmetrical to the center line of the inlet bore (2). Injektorkörper nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß sich die Ausbuchtung (8) bis zu einer Ebene (9), die parallel zur Längsachse (10) des Ventilraums (3) und durch die Zulauföffnung (7) hindurch verläuft, oder über diese Ebene (9) hinaus erstreckt. Injector body according to claim 1 or 2, characterized in that the bulge (8) extends up to or over a plane (9) which runs parallel to the longitudinal axis (10) of the valve chamber (3) and through the inlet opening (7) Level (9) extends. Injektorkörper nach Anspruch 3, dadurch gekennzeichnet, daß beide Ausbuchtungen (8) sich symmetrisch und gleichmäßig bis zur Ebene (9) erstrecken, so daß die Breite des Ventilraumquerschnitts im Bereich der Ausbuchtungen (8) dem Innendurchmesser des zylindrischen Ventilraums (3) entspricht.Injector body according to claim 3, characterized in that both bulges (8) extend symmetrically and evenly to the plane (9) so that the width of the valve chamber cross-section in the region of the bulges (8) corresponds to the inside diameter of the cylindrical valve chamber (3). Injektorkörper nach Anspruch 4, dadurch gekennzeichnet, daß die Zulaufbohrung (2) exzentrisch zum Ventilraum (3) angeordnet ist.Injector body according to claim 4, characterized in that the inlet bore (2) is arranged eccentrically to the valve chamber (3). Injektorkörper nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß in Längsrichtung des Ventilraums (3) über den Bereich der Zulauföffnung (7) die Ausbuchtungen (8) zu einer konstanten Querschnitterweiterung des Ventilraums (3) führen.Injector body according to one of claims 1 to 5, characterized in that in the longitudinal direction of the valve chamber (3) over the area of the inlet opening (7) the bulges (8) lead to a constant cross-sectional expansion of the valve chamber (3).
EP02015756A 2001-10-20 2002-07-13 High pressure resistant injector body Expired - Lifetime EP1304476B1 (en)

Applications Claiming Priority (2)

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DE10152230A DE10152230A1 (en) 2001-10-20 2001-10-20 High pressure resistant injector body
DE10152230 2001-10-20

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EP1304476A2 true EP1304476A2 (en) 2003-04-23
EP1304476A3 EP1304476A3 (en) 2004-05-19
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WO2012103899A1 (en) * 2011-02-01 2012-08-09 Robert Bosch Gmbh Housing for a pressure-loaded component
EP2960486A1 (en) * 2014-06-25 2015-12-30 Robert Bosch Gmbh Method for reducing the tension at a connection between two channels which open into one another

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DE10152230A1 (en) 2003-04-30
JP4227393B2 (en) 2009-02-18
EP1304476B1 (en) 2011-09-14
US20030089793A1 (en) 2003-05-15
EP1304476A3 (en) 2004-05-19
US6796512B2 (en) 2004-09-28
JP2003139013A (en) 2003-05-14

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