EP2084393A1 - Screw connection for fuel injector - Google Patents

Screw connection for fuel injector

Info

Publication number
EP2084393A1
EP2084393A1 EP07788488A EP07788488A EP2084393A1 EP 2084393 A1 EP2084393 A1 EP 2084393A1 EP 07788488 A EP07788488 A EP 07788488A EP 07788488 A EP07788488 A EP 07788488A EP 2084393 A1 EP2084393 A1 EP 2084393A1
Authority
EP
European Patent Office
Prior art keywords
nozzle
fuel injector
clamping element
holding body
nozzle clamping
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
EP07788488A
Other languages
German (de)
French (fr)
Other versions
EP2084393B1 (en
Inventor
Dietmar Uhlmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP2084393A1 publication Critical patent/EP2084393A1/en
Application granted granted Critical
Publication of EP2084393B1 publication Critical patent/EP2084393B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/16Sealing of fuel injection apparatus not otherwise provided for
    • 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
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
    • 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
    • F02M2200/80Fuel injection apparatus manufacture, repair or assembly
    • F02M2200/8023Fuel injection apparatus manufacture, repair or assembly the assembly involving use of quick-acting mechanisms, e.g. clips
    • 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
    • F02M2547/00Special features for fuel-injection valves actuated by fluid pressure
    • F02M2547/001Control chambers formed by movable sleeves
    • 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
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0014Valves characterised by the valve actuating means
    • F02M63/0015Valves characterised by the valve actuating means electrical, e.g. using solenoid
    • F02M63/0026Valves characterised by the valve actuating means electrical, e.g. using solenoid using piezoelectric or magnetostrictive actuators
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/004Sliding valves, e.g. spool valves, i.e. whereby the closing member has a sliding movement along a seat for opening and closing
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0045Three-way valves

Definitions

  • DE 196 50 865 A1 relates to a solenoid valve for controlling the fuel pressure in a control chamber of an injection valve, such as a common rail high-pressure accumulator injection system. Via the fuel pressure in the control chamber, a stroke movement of a valve piston is controlled, with which an injection opening of the injection valve is opened or closed.
  • the solenoid valve comprises an electromagnet, a movable armature and a valve member which is moved with the armature and acted upon by a valve closing spring in the closing direction and which cooperates with the valve seat of the solenoid valve and thus controls the fuel drain from the control chamber.
  • a screw connection is realized by means of a union nut which connects a nozzle body, a throttle plate resting thereon and a valve plate of a fuel injector with the holding body of the fuel injector. It is initially of minor importance, whether the fuel injector is actuated by means of a piezoelectric actuator or by means of a solenoid valve.
  • a sealing ring which is preferably made of PTFE, is used to achieve a seal of the low pressure area of the fuel injector to the outside.
  • a thread is formed on the inside of the nozzle retaining nut.
  • a non-threaded sealing bandage made of holding body and nozzle retaining nut, by the geometric shape of the fixation a higher surface pressure can be realized and a sealing bandage is provided, in which unintentional opening is prevented by a radial locking of a sleeve-shaped sealing element.
  • the proposed connection between a holding body of a fuel injector and the components associated with a nozzle body of the fuel injector by means of a sleeve-shaped locking element has the advantage that higher surface pressures on the resulting sealing surfaces in the sealing compound are possible, such.
  • sleeve-shaped locking element the thread on the inside and the external thread on the holding body can be omitted. Instead, only a locking and mounting groove on the sleeve-shaped locking element and a corresponding locking groove on the holding body are provided.
  • the locking between the sleeve-shaped locking element and the holding body takes place via a number of locking segments, which are formed tongue-shaped on one of the end regions of the sleeve-shaped locking element.
  • a defined locking force can be generated.
  • the height of the axial force introduced into the sealing dressing depends on a height difference between the bearing surface of the nozzle body and locking lugs in combination with the rigidity of the resilient region.
  • sleeve-shaped locking element a circumferential position orientation of the previously used nozzle lock nut, which affects the assembly time low.
  • fixing pins Due to the avoidance of a relative movement in the circumferential direction by the elimination of the screw and the risk of shearing is omitted for fixing pins, which may be required for correct installation of the valve and the throttle plate. If, on the other hand, the valve plate and the throttle plate are oriented in the correct position relative to one another, the use of fixing pins can be completely dispensed with.
  • NEN low-pressure seals are integrated into the nozzle retaining nut, so that previously used, preferably made of PTFE seals for low pressure sealing can be omitted.
  • FIG. 1 shows a schematic representation of essential elements of a fuel injector according to the prior art
  • FIG. 3 a representation of a nozzle tensioning element of the fuel injector proposed according to the invention
  • Detail B shows a plan view of the locking elements arranged on the nozzle clamping element according to FIG. 3,
  • FIG. 4 shows a development of an expansion region on the nozzle clamping element according to the illustration in FIG. 3,
  • FIG. 5 shows a side view of the expansion region of the nozzle tensioning element, shown in unwound form in FIG. 4, with recesses, FIG.
  • FIG. 6.1 a locking segment before snapping into a latching groove
  • FIG. 6.2 shows a locking segment latched in a latching groove
  • Figure 6.3 shows a disassembly tool for mounting the nozzle clamping element from the holding body
  • Figure 7 is a representation of a erf ⁇ ndungshiel proposed fuel injector with mounted on the holder body according to the invention nozzle tensioning element.
  • FIG. 1 shows that the fuel injector 10 known from the prior art has an electrical contact 12 in the head region.
  • the fuel injector 10 comprises a holding body 14 and a nozzle retaining nut 16 provided with an internal thread.
  • a valve plate 18 and a throttle plate 20 and a nozzle body 22 are sealingly clamped to one another in the context of a screw connection 24 the fuel injector 10 forms a compact unit.
  • enlarged detail of the fuel injector 10 shows that the nozzle retaining nut 16 includes a fine thread 40 on the inside, which cooperates with a corresponding formed on the outer peripheral surface of the holding body 14 thread and the screw 24 forms. In the lower region of the nozzle retaining nut 16, this comprises at least one key surface 26, which serves for the attachment of a torque applying tool.
  • a high-pressure inlet 30 which extends through the valve plate 18 and through the throttle plate 20.
  • valve plate 18, throttle plate 20 are employed on the end face of the nozzle body 22 and form a screw connection.
  • a control chamber 32 is formed by a control space sleeve 34, which is employed by means of a spring 36 to the underside of the throttle plate 20.
  • the spring 36 surrounds a, preferably needle-shaped injection valve member 38, wherein the spring 36 is supported on a received by the injection valve member 38 ring.
  • the nozzle retaining nut 16 is screwed by means of the fine thread 40 with the holding body 14 of the fuel injector 10.
  • FIG. 2 shows a section through the nozzle retaining nut.
  • FIG. 2 shows that the nozzle retaining nut 16 shown in a perspective section comprises the fine thread 40 on the inside in the head region and has at least one key recess 26 on the outer circumference for attachment of a tool applying a torque.
  • the nozzle retaining nut 16 shown in FIG. 2 comprises a first diameter D 1J , a second inner diameter D 12 and a third inner diameter D 13 .
  • the wall thicknesses Sl, S2 and S3 pointing downwards in the direction of the at least one key area 26 increases.
  • FIG. 3 shows a longitudinal section through the nozzle clamping element proposed according to the invention. From the sectional view according to FIG. 3 and the associated details A, B, C and D, it can be seen that the nozzle tensioning element 16 contains a fixing region 42 indicated by reference number 42 in its head region. Seen in the vertical direction, a number of locking tongues 44 extend within the fixing region 42 along the circumference of the nozzle clamping element 16 proposed according to the invention.
  • Each of the locking tongues 44 comprises on the inside, ie. H. on the outer circumference of the holding body 14 facing surface, a projection 46 which is preferably hook-shaped.
  • the locking tabs are separated from each other by gaps 48 to provide radial plasticity.
  • the gaps 48 between the individual locking tongues 44 in the fixing region 42 of the nozzle clamping element 16 are represented in detail "C" on an enlarged scale.
  • a first spherical shape 50 is formed on the inner peripheral surface of the nozzle chuck 16. This is within the range of the nozzle clamping element 16 (see illustration according to Figure 2), in which this the first inner diameter D 1; 1 has.
  • a mounting groove 58 is formed on the outer circumference of the nozzle clamping element 16 and the second spherical shape 52 on the inner circumferential surface.
  • FIG. 7 Details of the mounting groove 58 are shown in detail Below the second spherical shape 52 of the nozzle clamping element 16 there is a zone in which recesses 66 are annularly mounted in a perforation pattern 62, which in the schematic embodiment variant of the nozzle clamping element shown in FIG Eight have. Below the region provided with the perforation pattern 62 extends a bearing surface 54 on which the shoulder of the nozzle body 22 is supported in the mounted state (compare illustration according to FIG. 7).
  • the projection 46 of the locking tongue 44 is formed in a projection c with respect to the inner side of the locking tongue 44 and engages in a latching groove 46 formed on the outer circumference of the retaining body 14.
  • the angle of inclination is designated ⁇ in that the projection 46 extends on the locking tongue 44.
  • the strength of the resilient region of the locking tongue 44 is selected to an extent which exceeds the projection c.
  • the detailed representation "B” can be taken from the fact that a multiplicity of locking tongues 44 are arranged adjacent to one another in the circumferential direction along the circumference of the head region of the nozzle tensioning element 16 shown in Figure 3.
  • Each of the locking tongues 44 is comparable to the respectively adjacent locking tongue 44 via a gap 48 Detail “C”, separated.
  • a projection 46 is formed which engages in the locking groove 56 formed circumferentially on the holding body 14.
  • a mounting tool 60 can be latched into the mounting groove 58 shown in FIG. 3 on the outer peripheral surface of the nozzle clamping element 16.
  • the mounting tool 60 is inserted from below into the mounting groove 58 on the outer circumference of the nozzle clamping element 16 and e designates the mounting groove depth, in which the base of the mounting groove 58 is formed in comparison to the outer circumferential surface of the nozzle tensioning element 16.
  • the inner peripheral surface of the nozzle tensioning element is opposite the second spherical shape.
  • the nozzle clamping element 16 is locked at the upper end within the fixing region 42 by the locking tongues 44 with respect to the holding body 14.
  • the nozzle tensioning element 16 is pushed from below over the correctly positioned to each other injector components, nozzle body 22, throttle plate 20, valve plate 18 and holding body 14 during assembly of the injector composite.
  • the geometric coordination of the individual components relative to one another ensures that in the latched state of the locking tongues 44 within the fixing region 42 and the latching groove 56 on the holding body 14 a bias builds up.
  • the amount of this preload force can be determined by the geometry of the components over the slope. F ⁇ gkeit the nozzle clamping element 16 within the Lochungsmuster Kunststoffes 62 (Dehn Switzerland) are set with high process reliability.
  • FIG. 4 shows that the region illustrated in FIG. 3, in which the perforation pattern 62 is formed there, is shown unwound in the circumferential direction from 0 ° to 360 ° corresponding to the unwinding 64.
  • individual recesses 66 are offset relative to one another in the circumferential direction.
  • Each of the recesses 66 is arranged at a distance 68 to a preceding recess 66.
  • the length of each recess 68 is indicated by reference numeral 70. Size, shape, position and number of recesses 66 are based on the respectively required stiffness reduction within the provided with the Lochungsmuster 62 peripheral region of the nozzle clamping element 16.
  • the nozzle clamping element 16 has reached its mounting, ie locking position, as shown in FIG. 6.2, then the respective projections 46, which are formed on the inner side of the locking tongues 44 of the nozzle clamping element 16, snap into the locking groove 46. Furthermore, the first spherical shape 50 shown in FIG. 3 formed on the inside of the nozzle tensioning element 16 extends over the circumference of the holding body 14. The diameter of the first spherical shape 50 and that of the holding body 14 are oversized with each other so that they form a first pressure seal of the injector, so that can be dispensed with additional sealing rings.
  • the expansion element 16 Shortly before the locking of the locking tongues 44 with their projections 46 in the locking groove 56, the expansion element 16 comes to rest on the nozzle body 22, since the support surface 54 contacts the end face of the nozzle body 22.
  • the biasing force for elastic stretching of the expansion region 62 (hole pattern, cf. FIGS. 3 and 4) is applied via the assembly tool 60 to the mounting groove 58.
  • the locking tongues 44 After reaching the locking groove 56, the locking tongues 44 elastically spring back into their starting position (see illustration according to FIG. 6.2), latch into the locking groove 56 and lock the injector assembly. Thereafter, the mounting tool 60 can be removed.
  • the elastic restoring force of the expansion region 62, 72 of the nozzle tensioning element 16 permanently brings the desired biasing force of the injector components in relation to each other.
  • fixing pins for rotationally fixing the components relative to one another can be dispensed with. Also on the key surfaces 26 (see illustration according to Figure 2) on the outer circumference of the nozzle clamping element 16 may be omitted.
  • FIG. 6.3 shows how the locking tongues 44 are lifted out of the latching groove 56 on the holding body 14 with the aid of a dismantling tool 74 if the injector dressing is dismantled if necessary.
  • the locking tongues 44 formed inside the fixing area 42 are spaced apart by gaps with their respective projections 46 in the locking groove 56.
  • the locking groove 56 extends on the outer circumference of the holding body 14 the lower end of the vertically extending locking tongues 44 is the first spherical shape 50, which causes a low pressure seal and which rests on the circumference of the holding body 14.
  • the nozzle clamping element 16 also encloses the valve plate 18 and the throttle plate 20 and the nozzle body 22. According to FIG.
  • the nozzle body 22 is fixed by the nozzle tensioning element 16 to its bearing surface 54 and is pressed against the underside of the throttle plate 20 with its end face facing away from the combustion chamber end.
  • a circumferential surface 78 of the nozzle body 22 is set up with the second spherical formation 52, which is formed opposite the wall of the nozzle clamping element 16.
  • Below the mounting groove 58 or the second spherical shape 52 formed on the inside of the nozzle tensioning element 16 extends an area with reduced material thickness 72 or a region in which a perforation pattern 62 extends from the recesses 66 shown in connection with FIGS. 3 and 4.
  • the nozzle clamping element 16 In the mounted state 80 of the nozzle clamping element 16 shown in FIG. 7, the latter has an expansion region 72 or 62, which is shown only schematically, which can be formed either in a reduced material thickness or in which the perforation pattern 62 extends from recesses 66.

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The invention relates to a fuel injector (10) for injecting fuel into the combustion chamber of an internal combustion engine, having a holding body (14) and at least one nozzle body (22), wherein the nozzle body (22) is fastened to the holding body (14) of the fuel injector (10) under preload by means of a nozzle clamping element (16), characterized in that the nozzle clamping element (16) is connected to the holding body (14) by means of a latching connection (46, 56).

Description

Beschreibung description
Titeltitle
Schraubverbindung für KraftstoffinjektorScrew connection for fuel injector
Stand der TechnikState of the art
DE 196 50 865 Al bezieht sich auf ein Magnetventil zur Steuerung des Kraftstoffdruckes in einem Steuerraum eines Einspritzventiles, etwa eines Common-Rail-Hochdruck- speichereinspritzsystems. Über den Kraftstoffdruck im Steuerraum wird eine Hubbewegung eines Ventilkolbens gesteuert, mit dem eine Einspritzöffnung des Einspritzventiles geöffnet oder geschlossen wird. Das Magnetventil umfasst einen Elektromagneten, einen beweglichen Anker und ein mit dem Anker bewegtes und von einer Ventilschließfeder in Schließrichtung beaufschlagtes Ventilglied, das mit dem Ventilsitz des Magnetventiles zusammenwirkt und so den Kraftstoffabfluss aus dem Steuerraum steuert.DE 196 50 865 A1 relates to a solenoid valve for controlling the fuel pressure in a control chamber of an injection valve, such as a common rail high-pressure accumulator injection system. Via the fuel pressure in the control chamber, a stroke movement of a valve piston is controlled, with which an injection opening of the injection valve is opened or closed. The solenoid valve comprises an electromagnet, a movable armature and a valve member which is moved with the armature and acted upon by a valve closing spring in the closing direction and which cooperates with the valve seat of the solenoid valve and thus controls the fuel drain from the control chamber.
Bei bisher eingesetzten Kraftstoffinjektoren wird eine Schraub Verbindung mittels einer Ü- berwurfmutter verwirklicht, welche einen Düsenkörper, eine auf diesem aufliegende Drosselplatte sowie eine Ventilplatte eines Kraftstoffinjektors mit dem Haltekörper des Kraftstoffinjektors verbindet. Dabei ist es zunächst von untergeordneter Bedeutung, ob der Kraftstoffinjektor mittels eines Piezoaktors oder mittels eines Magnetventils betätigt wird. Im Allgemeinen kommt ein Dichtring, der bevorzugt aus PTFE gefertigt wird, zum Einsatz, um eine Abdichtung des Niederdruckbereiches des Kraftstoffinjektors nach außen zu erzielen. Zur Verbindung der Düsenspannmutter, die in der Regel einen Düsenkörper, eine Drosselplatte sowie eine Ventilplatte aufnimmt, und dem Haltekörper, ist an der Innenseite der Düsenspannmutter ein Gewinde ausgebildet. Über dieses Gewinde wird die Vorspannkraft in den Verbund aus Haltekörper und Düsenkörper sowie den darin eingelegten Bauteilen erreicht. Die Fertigung des Gewindes einerseits an der Innenseite der Düsenspannmutter und andererseits an der Außenumfangsfläche des Haltekörpers ist aufwändig und teuer, ferner kann es zu unerwünschter Leckage am Gewinde kommen sowie zu einer ungleich- mäßig verteilten Wirkung der durch das Gewindeanzugsmoment in den Schraubverband eingeleiteten Vorspannkraft. Offenbarung der ErfindungIn previously used fuel injectors, a screw connection is realized by means of a union nut which connects a nozzle body, a throttle plate resting thereon and a valve plate of a fuel injector with the holding body of the fuel injector. It is initially of minor importance, whether the fuel injector is actuated by means of a piezoelectric actuator or by means of a solenoid valve. In general, a sealing ring, which is preferably made of PTFE, is used to achieve a seal of the low pressure area of the fuel injector to the outside. To connect the nozzle retaining nut, which usually receives a nozzle body, a throttle plate and a valve plate, and the holding body, a thread is formed on the inside of the nozzle retaining nut. About this thread, the biasing force is achieved in the composite of holding body and nozzle body and the components inserted therein. The production of the thread on the one hand on the inside of the nozzle retaining nut and on the other hand on the outer peripheral surface of the holding body is complex and expensive, it can also lead to undesirable leakage at the thread and to a non-uniformly distributed effect of introduced by the Gewindeanzugsmoment in the Schraubverband biasing force. Disclosure of the invention
Erfindungsgemäß wird vorgeschlagen, einen Dichtverband ohne Gewinde aus Haltekörper und Düsenspannmutter bereitzustellen, durch dessen geometrische Ausformung der Fixie- rung eine höhere Flächenpressung realisierbar ist und ein Dichtverband bereitgestellt wird, bei dem ein unbeabsichtigtes Öffnen durch eine radiale Verriegelung eines hülsenförmig ausgebildeten Dichtelementes verhindert ist.According to the invention, it is proposed to provide a non-threaded sealing bandage made of holding body and nozzle retaining nut, by the geometric shape of the fixation a higher surface pressure can be realized and a sealing bandage is provided, in which unintentional opening is prevented by a radial locking of a sleeve-shaped sealing element.
Die vorgeschlagene Verbindung zwischen einem Haltekörper eines Kraftstoffinjektors sowie den einem Düsenkörper des Kraftstoffinjektors zugeordneten Komponenten mittels eines hülsenförmig ausgebildeten Verriegelungselementes bietet den Vorteil, dass höhere Flächenpressungen an den sich ergebenden Dichtflächen im Dichtverband möglich sind, so z. B. zwischen einem in das hülsenförmig ausgebildete Verriegelungselement eingelegten Düsenkörper, einer auf diesem aufliegenden Drosselplatte sowie einer auf der Drosselplatte aufliegenden Ventilplatte. Bei Einsatz des erfindungsgemäß vorgeschlagenen, hülsenförmig ausgebildeten Verriegelungselementes kann das Gewinde an der Innenseite und das Außengewinde am Haltekörper entfallen. Stattdessen sind lediglich eine Arretier- und Montagenut am hülsenförmigen Verriegelungselement sowie eine dazu korrespondierende Arretiernut am Haltekörper vorzusehen. Die Verriegelung zwischen dem hülsenförmigen Verriege- lungselement und dem Haltekörper erfolgt über eine Anzahl von Arretiersegmenten, die zungenförmig an einem der Endbereiche des hülsenförmig ausgebildeten Arretierelementes ausgebildet sind. Durch den Entfall des Gewindes können Plastifizierungsvorgänge und Setzvorgänge bei hohen Axialkräften ausgeschlossen werden. Ferner kann ein schnelles Schließen der Verbindung zwischen dem Haltekörper und dem hülsenförmig ausgebildeten Verriegelungselement durch eine einfache Schnappverriegelung erfolgen, was eine aufwändige Anzugsdrehmomentbestimmung, wie sie bisher üblich war, ebenfalls überflüssig macht.The proposed connection between a holding body of a fuel injector and the components associated with a nozzle body of the fuel injector by means of a sleeve-shaped locking element has the advantage that higher surface pressures on the resulting sealing surfaces in the sealing compound are possible, such. B. between an inserted into the sleeve-shaped locking element nozzle body, a resting on this throttle plate and a resting on the throttle plate valve plate. When using the inventively proposed, sleeve-shaped locking element, the thread on the inside and the external thread on the holding body can be omitted. Instead, only a locking and mounting groove on the sleeve-shaped locking element and a corresponding locking groove on the holding body are provided. The locking between the sleeve-shaped locking element and the holding body takes place via a number of locking segments, which are formed tongue-shaped on one of the end regions of the sleeve-shaped locking element. By eliminating the thread plasticizing operations and setting operations can be excluded at high axial forces. Furthermore, a rapid closing of the connection between the holding body and the sleeve-shaped locking element can be done by a simple snap lock, which also makes a complex tightening torque determination, as has been customary, superfluous.
Durch die geometrische Form der Arretiersegmente, die bevorzugt als voneinander getrennte, in Umfangsrichtung geteilt ausgebildete Arretierzunge dargestellt wird, kann eine defi- nierte Verriegelungskraft erzeugt werden. Die Höhe der in den Dichtverband eingebrachten Axialkraft richtet sich nach einer Höhendifferenz zwischen der Auflagefläche des Düsenkörpers und von Arretiernasen in Kombination mit der Steifigkeit des federnden Bereiches. Des Weiteren kann durch das erfindungsgemäß vorgeschlagene, hülsenförmig ausgebildete Verriegelungselement eine Umfangslageorientierung der bisher eingesetzten Düsenspannmutter entfallen, was die Montagezeit günstig beeinflusst. Die durch das erfϊndungsgemäß vorgeschlagene, hülsenförmige Verriegelungselement dargestellte Verbindung zwischen einem Düsenkörper und diesem zugeordneten Komponenten sowie dem Haltekörper des Kraftstoffϊnjektors kann auch wieder geöffnet werdenDue to the geometric shape of the locking segments, which is preferably shown as a separate, circumferentially divided formed locking tongue, a defined locking force can be generated. The height of the axial force introduced into the sealing dressing depends on a height difference between the bearing surface of the nozzle body and locking lugs in combination with the rigidity of the resilient region. Furthermore, can be omitted by the inventively proposed, sleeve-shaped locking element a circumferential position orientation of the previously used nozzle lock nut, which affects the assembly time low. The connection between a nozzle body and components associated therewith and the holding body of the fuel injector, as proposed by the invention, can also be opened again
Aufgrund der Vermeidung einer Relativbewegung in Umfangsrichtung durch den Entfall der Schraubverbindung ist auch die Abschergefahr für Fixierstifte entfallen, die gegebenenfalls zur lagerichtigen Montage der Ventil- und der Drosselplatte erforderlich sind. Sind hingegen die Ventil- und die Drosselplatte lagerichtig zueinander orientiert, kann auf den Einsatz von Fixierstiften vollständig verzichtet werden.Due to the avoidance of a relative movement in the circumferential direction by the elimination of the screw and the risk of shearing is omitted for fixing pins, which may be required for correct installation of the valve and the throttle plate. If, on the other hand, the valve plate and the throttle plate are oriented in the correct position relative to one another, the use of fixing pins can be completely dispensed with.
Des Weiteren ist durch den Entfall der Schraub Verbindung bei Einsatz des erfindungsgemäß vorgeschlagenen, hülsenförmig ausgebildeten Verriegelungselements keine Schlüsselfläche mehr an diesem erforderlich, was dessen Fertigung erheblich vereinfacht. Ein weiterer vorteilhafter, mit dem Einsatz der erfindungsgemäß vorgeschlagenen Lösung erzielbarer Effekt liegt darin, dass der bisher eingesetzte PTFE-Dichtring zur Abdichtung des Hochdruckbereiches vom Niederdruckbereich des Kraftstoffinjektors entfallen kann, wenn eine Niederdruckabdichtung über eine leicht ballige Ausformung der Innenseite des hülsenförmig ausgebildeten Verriegelungselementes an mindestens zwei Positionen durchgeführt wird.Furthermore, by eliminating the screw connection when using the inventively proposed, sleeve-shaped locking element no key surface more of this required, which greatly simplifies its production. Another advantageous, with the use of the proposed solution according to the invention achievable effect is that the previously used PTFE sealing ring for sealing the high-pressure region of the low-pressure region of the fuel injector can be omitted if a low-pressure seal on a slightly convex shape of the inside of the sleeve-shaped locking element at least two positions is performed.
Durch die geometrische Ausgestaltung der Arretiersegmente, die insbesondere als Arretierzungen ausgestaltet werden, können höhere Flächenpressungen, verglichen mit einer Schraubverbindung und damit höheren Vorspannkräften in der Schraubverbindung, realisiert werden. Feingewinde im Rahmen der Schraubverbindung an der Düsenspannmutter sowie am Haltekörper sowie zum Anlegen eines Sechskantschlüssels erforderliche Schlüs- selflächen können entfallen. Der Montagevorgang wird in Richtung auf eine einfache Schnappverbindung vereinfacht, so dass auf drehmoment- oder drehwinkelgesteuerte An- zugsverfahren und deren Überwachung verzichtet werden kann. Da beim Zusammenbau des erfindungsgemäß vorgeschlagenen Kraftstoffinjektors kein Verdrehen beziehungsweise Ver- schrauben erfolgt, kann ein Abscheren von Fixierstiften, die Ventil- und Drosselplatte zu- einander positionieren, verhindert werden. Sind Ventil- und Drosselplatte bei der Montage des Kraftstoffinjektors lagerichtig zueinander orientiert, werden die Fixierstifte im Übrigen überflüssig. Der montierte Injektorverband kann einfach mit Hilfe eines Hilfswerkzeugs entriegelt werden, wobei eine Umfangslageorientierung der Düsenspannmutter nicht mehr erforderlich ist. Durch eine spezielle Ausbildung des Bereiches E der Düsenspannmutter als Dehnbereich (vergleiche mögliche Ausführungsform des Dehnbereiches gemäß Figur 4) ist eine definierte Axialkraft als Vorspannkraft für den Dichtungsverbund über die Steifigkeit dieses Bereiches und die Geometrie der Düsenspannmutter einstellbar. Durch die geometrische Ausbildung der Düsenspannmutter mit mindestens zwei balligen Ausformungen kön- nen Niederdruckabdichtungen in die Düsenspannmutter integriert werden, so dass bisher eingesetzte, bevorzugt als PTFE gefertigte Dichtringe zur Niederdruckabdichtung entfallen können.Due to the geometric configuration of the locking segments, which are designed in particular as locking tongues, higher surface pressures, compared with a screw connection and thus higher biasing forces in the screw can be realized. Fine threads within the scope of the screw connection on the nozzle retaining nut as well as on the holding body as well as for the application of a hexagonal key required key surfaces can be omitted. The assembly process is simplified in the direction of a simple snap connection, so that it is possible to dispense with torque or angle-controlled tightening methods and their monitoring. Since no twisting or screwing takes place during the assembly of the fuel injector proposed according to the invention, a shearing off of fixing pins which position the valve plate and throttle plate relative to one another can be prevented. Are valve and throttle plate oriented in the correct position when mounting the fuel injector to each other, the fixing pins are otherwise superfluous. The assembled injector bandage can be easily unlocked with the aid of an auxiliary tool, with a circumferential position orientation of the nozzle retaining nut is no longer required. By a special design of the region E of the nozzle retaining nut as Dehnbereich (see possible embodiment of the expansion according to Figure 4) is a defined axial force as a biasing force for the sealing compound on the stiffness of this range and the geometry of the nozzle retaining nut adjustable. Due to the geometrical design of the nozzle retaining nut with at least two crowned formations NEN low-pressure seals are integrated into the nozzle retaining nut, so that previously used, preferably made of PTFE seals for low pressure sealing can be omitted.
Zeichnungdrawing
Anhand der Zeichnung wird die Erfindung nachstehend eingehender beschrieben.With reference to the drawing, the invention will be described below in more detail.
Es zeigt:It shows:
Figur 1 eine schematische Darstellung wesentlicher Elemente eines Kraftstoffinjektors gemäß des Standes der Technik,1 shows a schematic representation of essential elements of a fuel injector according to the prior art,
Figur 2 eine Schnittdarstellung durch eine bisher verwendete Düsenspannmutter,2 shows a sectional view through a previously used nozzle retaining nut,
Figur 3 eine Darstellung eines erfindungsgemäß vorgeschlagenen Düsenspannelementes des Kraftstoffinjektors,FIG. 3 a representation of a nozzle tensioning element of the fuel injector proposed according to the invention,
Detail A in verrasteter Stellung dargestellte Arretierelemente,Detail A locking elements shown in latched position,
Detail B eine Draufsicht auf die am Düsenspannelement gemäß Figur 3 angeordneten Arretiersegmente,Detail B shows a plan view of the locking elements arranged on the nozzle clamping element according to FIG. 3,
Detail C ein Ausführungsdetail zwischen den Arretiersegmenten,Detail C an execution detail between the locking segments,
Detail D ein Detail einer Montagenut des Düsenspannelementes mit Montagewerkzeug,Detail D a detail of a mounting groove of the nozzle clamping element with assembly tool,
Figur 4 eine Abwicklung eines Dehnbereiches am Düsenspannelement gemäß der Dar- Stellung in Figur 3,FIG. 4 shows a development of an expansion region on the nozzle clamping element according to the illustration in FIG. 3,
Figur 5 eine Seitenansicht des in Figur 4 in abgewickelter Form dargestellten, mit Aussparungen versehenen Dehnbereiches des Düsenspannelementes,FIG. 5 shows a side view of the expansion region of the nozzle tensioning element, shown in unwound form in FIG. 4, with recesses, FIG.
Figur 6.1 ein Arretiersegment vor dem Einschnappen in einer Rastnut,FIG. 6.1 a locking segment before snapping into a latching groove, FIG.
Figur 6.2 einen in einer Rastnut verrastetes Arretiersegment, Figur 6.3 ein Demontagewerkzeug zum Montieren des Düsenspannelementes vom Haltekörper undFIG. 6.2 shows a locking segment latched in a latching groove; Figure 6.3 shows a disassembly tool for mounting the nozzle clamping element from the holding body and
Figur 7 eine Darstellung eines erfϊndungsgemäß vorgeschlagenen Kraftstoffinjektors mit an dessen Haltekörper montiertem erfindungsgemäßen Düsenspannelement.Figure 7 is a representation of a erfϊndungsgemäß proposed fuel injector with mounted on the holder body according to the invention nozzle tensioning element.
Ausführungsvariantenvariants
Aus der Darstellung gemäß Figur 1 geht hervor, dass der aus dem Stand der Technik bekannte Kraftstoffinjektor 10 im Kopfbereich eine elektrische Kontaktierung 12 aufweist. Darüber hinaus umfasst der Kraftstoffinjektor 10 gemäß der Darstellung in Figur 1 einen Haltekörper 14 sowie eine mit einem Innengewinde versehene Düsenspannmutter 16. Über diese werden eine Ventilplatte 18 und eine Drosselplatte 20 sowie ein Düsenkörper 22 im Rahmen einer Schraub Verbindung 24 dichtend ineinander verspannt, so dass der Kraftstoffinjektor 10 eine kompakte Baueinheit bildet. Aus dem in Figur 1 dargestellten, vergrößert dargestellten Ausschnitt des Kraftstoffinjektors 10 geht hervor, dass die Düsenspannmutter 16 an der Innenseite ein Feingewinde 40 enthält, welches mit einem korrespondierend an der Außenumfangsfläche des Haltekörpers 14 ausgebildeten Gewinde zusammenwirkt und die Schraubverbindung 24 bildet. Im unteren Bereich der Düsenspannmutter 16 umfasst diese mindestens eine Schlüsselfläche 26, welche zum Ansatz eines ein Drehmoment aufbringenden Werkzeuges dient.The illustration according to FIG. 1 shows that the fuel injector 10 known from the prior art has an electrical contact 12 in the head region. In addition, as shown in FIG. 1, the fuel injector 10 comprises a holding body 14 and a nozzle retaining nut 16 provided with an internal thread. A valve plate 18 and a throttle plate 20 and a nozzle body 22 are sealingly clamped to one another in the context of a screw connection 24 the fuel injector 10 forms a compact unit. From the illustrated in Figure 1, enlarged detail of the fuel injector 10 shows that the nozzle retaining nut 16 includes a fine thread 40 on the inside, which cooperates with a corresponding formed on the outer peripheral surface of the holding body 14 thread and the screw 24 forms. In the lower region of the nozzle retaining nut 16, this comprises at least one key surface 26, which serves for the attachment of a torque applying tool.
Durch den Haltekörper 14 verläuft ein Hochdruckzulauf 30, der sich durch die Ventilplatte 18 sowie durch die Drosselplatte 20 erstreckt. Durch die Düsenspannmutter 16 werden die Stirnseiten von Haltekörper 14, Ventilplatte 18, Drosselplatte 20 an die Stirnseite des Düsenkörpers 22 angestellt und bilden einen Schraubverbund.Through the holding body 14 extends a high-pressure inlet 30, which extends through the valve plate 18 and through the throttle plate 20. By the nozzle lock nut 16, the front sides of the holding body 14, valve plate 18, throttle plate 20 are employed on the end face of the nozzle body 22 and form a screw connection.
Im Düsenkörper 22 des Kraftstoffinjektors 10 wird ein Steuerraum 32 durch eine Steuer- raumhülse 34 gebildet, der mittels einer Feder 36 an die Unterseite der Drosselplatte 20 angestellt ist. Die Feder 36 umgibt ein, bevorzugt nadeiförmig ausgebildetes Einspritzventilglied 38, wobei die Feder 36 sich an einem vom Einspritzventilglied 38 aufgenommenen Ring abstützt. Die Düsenspannmutter 16 ist mittels des Feingewindes 40 mit dem Haltekörper 14 des Kraftstoffinjektors 10 verschraubt.In the nozzle body 22 of the fuel injector 10, a control chamber 32 is formed by a control space sleeve 34, which is employed by means of a spring 36 to the underside of the throttle plate 20. The spring 36 surrounds a, preferably needle-shaped injection valve member 38, wherein the spring 36 is supported on a received by the injection valve member 38 ring. The nozzle retaining nut 16 is screwed by means of the fine thread 40 with the holding body 14 of the fuel injector 10.
Aus der Darstellung gemäß Figur 2 geht ein Schnitt durch die Düsenspannmutter hervor. Figur 2 ist entnehmbar, dass die in perspektivischem Schnitt dargestellte Düsenspannmutter 16 an der Innenseite im Kopfbereich das Feingewinde 40 umfasst und am Fußbereich am Außenumfang mindestens eine Schlüsselfiäche 26 zum Ansatz eines ein Drehmoment aufbringenden Werkzeuges aufweist. Die in Figur 2 dargestellte Düsenspannmutter 16 umfasst einen ersten Durchmesser D1J, einen zweiten Innendurchmesser D12 sowie einen dritten Innendurchmesser D13. Des Weiteren geht aus der perspektivischen Schnittdarstellung gemäß Figur 2 durch die Düsenspannmutter 16 hervor, dass die Düsenspannmutter 16 im Bereich der genannten Durchmesser jeweils unterschiedliche Wandstärken Si, S2 sowie S3 aufweist, wobei die Wandstärken Sl, S2 und S3 nach unten hin in Richtung auf die mindes- tens eine Schlüsselfiäche 26 hin zunehmen.The illustration according to FIG. 2 shows a section through the nozzle retaining nut. FIG. 2 shows that the nozzle retaining nut 16 shown in a perspective section comprises the fine thread 40 on the inside in the head region and has at least one key recess 26 on the outer circumference for attachment of a tool applying a torque. The nozzle retaining nut 16 shown in FIG. 2 comprises a first diameter D 1J , a second inner diameter D 12 and a third inner diameter D 13 . Furthermore, it is apparent from the perspective sectional illustration according to FIG. 2 through the nozzle retaining nut 16 that the nozzle retaining nut 16 has different wall thicknesses Si, S 2 and S3 in the region of the mentioned diameters, the wall thicknesses Sl, S2 and S3 pointing downwards in the direction of the at least one key area 26 increases.
Der Darstellung gemäß Figur 3 ist ein Längsschnitt durch das erfindungsgemäß vorgeschlagene Düsenspannelement zu entnehmen. Aus der Schnittdarstellung gemäß Figur 3 sowie den dazugehörigen Details A, B, C und D geht hervor, dass das Düsenspannelement 16 in seinem Kopfbereich einen durch Bezugszeichen 42 kenntlich gemachten Fixierbereich 42 enthält. In vertikale Richtung gesehen erstrecken sich innerhalb des Fixierbereiches 42 entlang des Umfangs des erfindungsgemäß vorgeschlagenen Düsenspannelementes 16 eine Anzahl von Arretierzungen 44. Jede der Arretierzungen 44 umfasst an der Innenseite, d. h. auf der dem Außenumfang des Haltekörpers 14 zuweisenden Fläche, einen Vorsprung 46, der bevorzugt hakenförmig ausgebildet ist. Die Arretierzungen sind zur Erzeugung einer radialen Plastizität durch Spalte 48 voneinander getrennt. Die Spalte 48 zwischen den einzelnen Arretierzungen 44 im Fixierbereich 42 des Düsenspannelementes 16 sind im Detail „C" in vergrößertem Maßstab darstellt.The illustration according to FIG. 3 shows a longitudinal section through the nozzle clamping element proposed according to the invention. From the sectional view according to FIG. 3 and the associated details A, B, C and D, it can be seen that the nozzle tensioning element 16 contains a fixing region 42 indicated by reference number 42 in its head region. Seen in the vertical direction, a number of locking tongues 44 extend within the fixing region 42 along the circumference of the nozzle clamping element 16 proposed according to the invention. Each of the locking tongues 44 comprises on the inside, ie. H. on the outer circumference of the holding body 14 facing surface, a projection 46 which is preferably hook-shaped. The locking tabs are separated from each other by gaps 48 to provide radial plasticity. The gaps 48 between the individual locking tongues 44 in the fixing region 42 of the nozzle clamping element 16 are represented in detail "C" on an enlarged scale.
Unterhalb des durch Bezugszeichen 42 kenntlich gemachten Fixierbereiches ist an der In- nenumfangsfiäche des Düsenspannelementes 16 eine erste ballige Ausformung 50 ausgebildet. Diese liegt innerhalb des Bereiches des Düsenspannelementes 16 (vergleiche Darstellung gemäß Figur 2), in dem dieses den ersten Innendurchmesser D1; 1 aufweist. Im Übergangsbereich der Wand des Düsenspannelementes 16 gemäß der Darstellung in Figur 3 vom ersten Innendurchmesser D1J zum zweiten Innendurchmesser D12 ist am Außenumfang des Düsenspannelementes 16 eine Montagenut 58 ausgebildet und an der Innenumfangsfiäche die zweite ballige Ausformung 52. Details der Montagenut 58 sind der Detaildarstellung „D" zu entnehmen. Unterhalb der zweiten balligen Ausformung 52 des Düsenspannelementes 16 befindet sich eine Zone, in der in einem Lochungsmuster 62 Aussparungen 66 ring- förmig angebracht werden, die in der in Figur 3 dargestellten schematischen Ausführungsvariante des Düsenspannelementes ein Außenprofil ähnlich einer liegenden Acht aufweisen. Unterhalb des mit dem Lochungsmuster 62 versehenen Bereiches verläuft eine Auflagefläche 54, auf der sich im montierten Zustand die Schulter des Düsenkörpers 22 abstützt (vergleiche Darstellung gemäß Figur 7).Below the fixing region identified by reference numeral 42, a first spherical shape 50 is formed on the inner peripheral surface of the nozzle chuck 16. This is within the range of the nozzle clamping element 16 (see illustration according to Figure 2), in which this the first inner diameter D 1; 1 has. In the transition region of the wall of the nozzle clamping element 16 as shown in FIG. 3 from the first inner diameter D 1J to the second inner diameter D 12 , a mounting groove 58 is formed on the outer circumference of the nozzle clamping element 16 and the second spherical shape 52 on the inner circumferential surface. Details of the mounting groove 58 are shown in detail Below the second spherical shape 52 of the nozzle clamping element 16 there is a zone in which recesses 66 are annularly mounted in a perforation pattern 62, which in the schematic embodiment variant of the nozzle clamping element shown in FIG Eight have. Below the region provided with the perforation pattern 62 extends a bearing surface 54 on which the shoulder of the nozzle body 22 is supported in the mounted state (compare illustration according to FIG. 7).
Dem Detail ,,A" ist zu entnehmen, dass der Vorsprung 46 der Arretierzunge 44 in einem Überstand c in Bezug auf die Innenseite der Arretierzunge 44 ausgebildet ist und in eine am Außenumfang des Haltekörpers 14 eingebrachte Rastnut 46 eingreift. Mit α ist der Steigungswinkel bezeichnet, in dem der Vorsprung 46 an der Arretierzunge 44 verläuft. Die Stärke des federnden Bereiches der Arretierzunge 44 ist in einem Maß gewählt, das den Überstand c übersteigt.It can be seen from the detail "A" that the projection 46 of the locking tongue 44 is formed in a projection c with respect to the inner side of the locking tongue 44 and engages in a latching groove 46 formed on the outer circumference of the retaining body 14. The angle of inclination is designated α in that the projection 46 extends on the locking tongue 44. The strength of the resilient region of the locking tongue 44 is selected to an extent which exceeds the projection c.
Der Detaildarstellung „B" ist entnehmbar, dass entlang des Umfangs des Kopfbereiches des in Figur 3 dargestellten Düsenspannelementes 16 eine Vielzahl von Arretierzungen 44 in Umfangsrichtung nebeneinander liegend angeordnet sind. Jede der Arretierzungen 44 ist von der jeweils benachbarten Arretierzunge 44 über einen Spalt 48, vergleiche Detail „C", getrennt. Bevorzugt ist an der Innenseite einer jeden der im Fixierbereich 42 des Düsenspannelementes 16 ausgebildeten Arretierzungen 44 ein Vorsprung 46 ausgebildet, der in die sich umfänglich am Haltekörper 14 ausgebildete Rastnut 56 eingreift.The detailed representation "B" can be taken from the fact that a multiplicity of locking tongues 44 are arranged adjacent to one another in the circumferential direction along the circumference of the head region of the nozzle tensioning element 16 shown in Figure 3. Each of the locking tongues 44 is comparable to the respectively adjacent locking tongue 44 via a gap 48 Detail "C", separated. Preferably, on the inside of each of the locking tongues 44 formed in the fixing region 42 of the nozzle clamping element 16, a projection 46 is formed which engages in the locking groove 56 formed circumferentially on the holding body 14.
Detail „D" ist zu entnehmen, dass in die in Figur 3 dargestellte Montagenut 58 an der Au- ßenumfangsfläche des Düsenspannelementes 16 ein Montagewerkzeug 60 verrastbar ist. Das Montagewerkzeug 60 wird von unten her in die Montagenut 58 am Außenumfang des Düsenspannelementes 16 eingeführt wird und verrastet in dieser. Mit e ist die Montagenut- Tiefe bezeichnet, in welcher der Grund der Montagenut 58 im Vergleich zur Außenum- fangsfläche des Düsenspannelementes 16 ausgebildet ist. Im Bereich der Montagenut 58 liegt der Innenumfangsfläche des Düsenspannelementes die zweite ballige Ausformung gegenüber.3, a mounting tool 60 can be latched into the mounting groove 58 shown in FIG. 3 on the outer peripheral surface of the nozzle clamping element 16. The mounting tool 60 is inserted from below into the mounting groove 58 on the outer circumference of the nozzle clamping element 16 and e designates the mounting groove depth, in which the base of the mounting groove 58 is formed in comparison to the outer circumferential surface of the nozzle tensioning element 16. In the region of the mounting groove 58, the inner peripheral surface of the nozzle tensioning element is opposite the second spherical shape.
Bei der in Figur 3 und den zu dieser gehörenden Detaildarstellungen A, B, C und D wird das Düsenspannelement 16 am oberen Ende innerhalb des Fixierbereiches 42 durch die Arretierzungen 44 gegenüber dem Haltekörper 14 verriegelt. Hierzu wird bei der Montage des Injektorverbundes das Düsenspannelement 16 von unten her über die lagerichtig zueinander positionierten Injektorkomponenten, Düsenkörper 22, Drosselplatte 20, Ventilplatte 18 und Haltekörper 14 geschoben. Die geometrische Abstimmung der einzelnen Komponenten rela- tiv zueinander stellt sicher, dass sich im verrasteten Zustand der Arretierzungen 44 innerhalb des Fixierbereiches 42 und der Rastnut 56 am Haltekörper 14 eine Vorspannung aufbaut. Die Höhe dieser Vorspannkraft kann über die Geometrie der Komponenten über die Stei- fϊgkeit des Düsenspannelementes 16 innerhalb des Lochungsmusterbereiches 62 (Dehnbereich) mit hoher Prozesssicherheit eingestellt werden.In the detailed representations A, B, C and D belonging to FIG. 3, the nozzle clamping element 16 is locked at the upper end within the fixing region 42 by the locking tongues 44 with respect to the holding body 14. For this purpose, the nozzle tensioning element 16 is pushed from below over the correctly positioned to each other injector components, nozzle body 22, throttle plate 20, valve plate 18 and holding body 14 during assembly of the injector composite. The geometric coordination of the individual components relative to one another ensures that in the latched state of the locking tongues 44 within the fixing region 42 and the latching groove 56 on the holding body 14 a bias builds up. The amount of this preload force can be determined by the geometry of the components over the slope. Fϊgkeit the nozzle clamping element 16 within the Lochungsmusterbereiches 62 (Dehnbereich) are set with high process reliability.
Der Darstellung gemäß Figur 4 ist entnehmbar, wie durch eine gezielte Lochung des Düsen- spannelementes die Steifigkeit auf ein gewünschtes Maß reduziert werden kann.It can be seen from the illustration according to FIG. 4 how the stiffness can be reduced to a desired degree by targeted perforation of the nozzle tensioning element.
Aus der Darstellung gemäß Figur 4 geht hervor, dass der in Figur 3 dargestellte Bereich, indem dort das Lochungsmuster 62 ausgebildet ist, in Umfangsrichtung von 0° bis 360° entsprechend der Abwicklung 64 abgewickelt dargestellt ist. Innerhalb des Lochungsmus- terbereiches 62 in der abgewickelten Darstellung gemäß Figur 4 liegen einzelne Aussparungen 66 versetzt zueinander in Umfangsrichtung. Jede der Aussparungen 66 ist in einem Abstand 68 zu einer vorhergehenden Aussparung 66 angeordnet. Die Länge einer jeden Aussparung 68 ist durch Bezugszeichen 70 angedeutet. Größe, Form, Lage und Anzahl der Aussparungen 66 orientieren sich an der jeweils geforderten Steifigkeitsminderung innerhalb des mit dem Lochungsmuster 62 versehenen Umfangsbereiches des Düsenspannelementes 16. Aus der Darstellung gemäß Figur 5 geht hervor, dass der in Figur 4 in Abwicklung 64 dargestellte Bereich der Wandstärke des Düsenspannelementes 16 in einer reduzierten Materialdicke 72 ausgebildet werden kann. Wird am Düsenspannelement 16, wie in Figur 5 dargestellt, ein Bereich mit reduzierter Materialstärke 72 ausgebildet, so kann auf die in Figur 4 und Figur 3 dargestellten Aussparungen 68 verzichtet werden, da allein durch die Querschnittsverminderung 72 im Düsenspannelement 16, ähnlich dem Prinzip einer Dehn- schraube, die gewünschte Steifigkeitsreduzierung erzielt werden kann.The illustration according to FIG. 4 shows that the region illustrated in FIG. 3, in which the perforation pattern 62 is formed there, is shown unwound in the circumferential direction from 0 ° to 360 ° corresponding to the unwinding 64. Within the perforation pattern region 62 in the unwound representation according to FIG. 4, individual recesses 66 are offset relative to one another in the circumferential direction. Each of the recesses 66 is arranged at a distance 68 to a preceding recess 66. The length of each recess 68 is indicated by reference numeral 70. Size, shape, position and number of recesses 66 are based on the respectively required stiffness reduction within the provided with the Lochungsmuster 62 peripheral region of the nozzle clamping element 16. From the illustration in Figure 5 shows that the illustrated in Figure 4 in settlement 64 range of wall thickness of the nozzle clamping element 16 can be formed in a reduced material thickness 72. If an area with reduced material thickness 72 is formed on the nozzle clamping element 16, as shown in FIG. 5, the recesses 68 shown in FIG. 4 and FIG. 3 can be dispensed with, since the cross section reduction 72 alone in the nozzle clamping element 16, similar to the principle of a stretching - Screw, the desired stiffness reduction can be achieved.
Der Figurensequenz der Figuren 6.1, 6.2 und 6.3 sind Montage und Demontage des Düsen- spannelementes am Haltekörper zu entnehmen.The figure sequence of Figures 6.1, 6.2 and 6.3 are shown assembly and disassembly of the nozzle tensioning element on the holding body.
Der Darstellung gemäß Figur 6.1 ist entnehmbar, dass bei Montage des Düsenspannelementes 16 dieses nach oben auf den Haltekörper 14 aufgeschoben wird. Aufgrund der elastischen Eigenschaften der im Fixierbereich 42 des Düsenspannelementes 16 angeordneten Arretierzungen 44 spreizen diese leicht auf, so dass der Vorsprung 46, wie in Figur 6.1 dargestellt, leicht nach außen gedrückt ist.It can be seen from the illustration according to FIG. 6.1 that, when the nozzle clamping element 16 is mounted, it is slid upwards onto the holding body 14. Due to the elastic properties of the locking tongues 44 arranged in the fixing region 42 of the nozzle clamping element 16, they spread open slightly, so that the projection 46, as shown in FIG. 6.1, is pressed slightly outward.
Hat das Düsenspannelement 16 seine Montage, d. h. Verriegelungsposition, erreicht - wie in Figur 6.2 dargestellt -, so schnappen die jeweiligen Vorsprünge 46, die an der Innenseite der Arretierzungen 44 des Düsenspannelementes 16 ausgebildet sind, in die Rastnut 46 ein. Des Weiteren erstreckt sich die in Figur 3 dargestellte, an der Innenseite des Düsenspannelementes 16 ausgebildete erste ballige Ausformung 50 über den Umfang des Haltekörpers 14. Der Durchmesser der ersten balligen Ausformung 50 und der des Haltekörpers 14 sind mit Übermaß so aufeinander abgestimmt, dass diese eine erste Druckabdichtung des Injektorverbandes bilden, so dass auf zusätzliche Dichtringe verzichtet werden kann.If the nozzle clamping element 16 has reached its mounting, ie locking position, as shown in FIG. 6.2, then the respective projections 46, which are formed on the inner side of the locking tongues 44 of the nozzle clamping element 16, snap into the locking groove 46. Furthermore, the first spherical shape 50 shown in FIG. 3 formed on the inside of the nozzle tensioning element 16 extends over the circumference of the holding body 14. The diameter of the first spherical shape 50 and that of the holding body 14 are oversized with each other so that they form a first pressure seal of the injector, so that can be dispensed with additional sealing rings.
Kurz vor der Verrastung der Arretierzungen 44 mit ihren Vorsprüngen 46 in der Rastnut 56 kommt das Dehnelement 16 zur Anlage am Düsenkörper 22, da die Auflagefläche 54 die Stirnfläche des Düsenkörpers 22 berührt. Bei weiterem Vorschieben des Düsenspannele- mentes 16 in Richtung auf die Rastnut 56 bis zur Verrastung der Arretierzungen 44 in dieser wird über das Montagewerkzeug 60 an der Montagenut 58 die Vorspannkraft zur elastischen Dehnung des Dehnbereiches 62 (Lochmuster, vergleiche Figur 3 und 4) aufgebracht. Nach Erreichen der Rastnut 56 federn die Arretierzungen 44 elastisch in ihre Ausgangslage zurück (vergleiche Darstellung gemäß Figur 6.2), rasten in die Rastnut 56 ein und verriegeln der Injektorverband. Danach kann das Montagewerkzeug 60 entfernt werden. Die elastische Rückstellkraft des Dehnbereiches 62, 72 des Düsenspannelementes 16 bringt dauerhaft die gewünschte Vorspannkraft der Injektorkomponenten in Bezug zueinander auf.Shortly before the locking of the locking tongues 44 with their projections 46 in the locking groove 56, the expansion element 16 comes to rest on the nozzle body 22, since the support surface 54 contacts the end face of the nozzle body 22. Upon further advancement of the nozzle clamping element 16 in the direction of the latching groove 56 until latching of the locking tongues 44, the biasing force for elastic stretching of the expansion region 62 (hole pattern, cf. FIGS. 3 and 4) is applied via the assembly tool 60 to the mounting groove 58. After reaching the locking groove 56, the locking tongues 44 elastically spring back into their starting position (see illustration according to FIG. 6.2), latch into the locking groove 56 and lock the injector assembly. Thereafter, the mounting tool 60 can be removed. The elastic restoring force of the expansion region 62, 72 of the nozzle tensioning element 16 permanently brings the desired biasing force of the injector components in relation to each other.
Da während des Montagevorgangs keine Verdrehung der Komponenten des Kraftstoffinjek- tors 10 zueinander erfolgt, kann auf Fixierstifte zur Drehfixierung der Komponenten relativ zueinander verzichtet werden. Auch auf die Schlüsselflächen 26 (vergleiche Darstellung gemäß Figur 2) am Außenumfang des Düsenspannelementes 16 kann verzichtet werden.Since no rotation of the components of the fuel injector 10 takes place relative to one another during the assembly process, fixing pins for rotationally fixing the components relative to one another can be dispensed with. Also on the key surfaces 26 (see illustration according to Figure 2) on the outer circumference of the nozzle clamping element 16 may be omitted.
Figur 6.3 zeigt, wie bei einer gegebenenfalls erforderlichen Demontage des Injektorverbandes die Arretierzungen 44 mit Hilfe eines Demontagewerkzeuges 74 aus der Rastnut 56 am Haltekörper 14 gehoben werden. Nach einem in radialer Richtung erfolgenden Herausstellen der Vorsprünge 46 aus der Rastnut 56 am Umfang des Haltekörpers 14 kann das Dü- senspannelement 16 in Abzugsrichtung 76 nach unten vom Haltekörper 14 des Kraftstoffinjektors 10 abgezogen werden, wie in Figur 6.3 dargestellt.FIG. 6.3 shows how the locking tongues 44 are lifted out of the latching groove 56 on the holding body 14 with the aid of a dismantling tool 74 if the injector dressing is dismantled if necessary. After a pointing out in the radial direction of the projections 46 from the locking groove 56 on the circumference of the holding body 14, the Dü- can be peeled tension member 16 in the withdrawal direction 76 downward from the holding body 14 of the fuel injector 10, as shown in Figure 6.3.
Der Darstellung gemäß Figur 7 ist schließlich entnehmbar, wie das erfindungsgemäß vorgeschlagene Düsenspannelement im Injektorverbund im montierten Zustand angeordnet ist.Finally, it can be seen from the illustration according to FIG. 7 how the nozzle clamping element proposed according to the invention is arranged in the assembled state of the injector.
Im in Figur 7 dargestellten montierten Zustand 80 des Düsenspannelementes 16 am Haltekörper 14 liegen die innerhalb des Fixierbereiches 42 ausgebildeten, durch Spalte voneinander getrennten Arretierzungen 44 mit ihren jeweiligen Vorsprüngen 46 in der Rastnut 56. Die Rastnut 56 erstreckt sich am Außenumfang des Haltekörpers 14. Am unteren Ende der sich in vertikale Richtung erstreckenden Arretierzungen 44 befindet sich die erste ballige Ausformung 50, welche eine Niederdruckabdichtung bewirkt und die am Umfang des Haltekörpers 14 anliegt. Das Düsenspannelement 16 umschließt darüber hinaus die Ventilplatte 18 sowie die Drosselplatte 20 und den Düsenkörper 22. Des Weiteren geht aus der Darstel- lung gemäß Figur 7 hervor, dass der Düsenkörper 22 durch das Düsenspannelement 16 an dessen Auflagefläche 54 fixiert wird und mit seiner dem brennraumseitigen Ende abgewandten Stirnseite gegen die Unterseite der Drosselplatte 20 gedrückt wird. An eine Umfangsflä- che 78 des Düsenkörpers 22 wird gemäß der Darstellung in Figur 7 die zweite ballige Aus- formung 52 angestellt, die gegenüberliegend in der Wand des Düsenspannelementes 16 ausgebildet ist. Unterhalb der Montagenut 58 beziehungsweise der an der Innenseite des Düsenspannelementes 16 ausgebildeten, zweiten balligen Ausformung 52 verläuft ein Bereich mit reduzierter Materialstärke 72 oder ein Bereich, in dem ein Lochungsmuster 62 aus den im Zusammenhang mit Figur 3 und 4 dargestellten Aussparungen 66 verläuft.In the mounted state 80 of the nozzle clamping element 16 on the holding body 14 shown in FIG. 7, the locking tongues 44 formed inside the fixing area 42 are spaced apart by gaps with their respective projections 46 in the locking groove 56. The locking groove 56 extends on the outer circumference of the holding body 14 the lower end of the vertically extending locking tongues 44 is the first spherical shape 50, which causes a low pressure seal and which rests on the circumference of the holding body 14. The nozzle clamping element 16 also encloses the valve plate 18 and the throttle plate 20 and the nozzle body 22. According to FIG. 7, it can be seen that the nozzle body 22 is fixed by the nozzle tensioning element 16 to its bearing surface 54 and is pressed against the underside of the throttle plate 20 with its end face facing away from the combustion chamber end. As shown in FIG. 7, a circumferential surface 78 of the nozzle body 22 is set up with the second spherical formation 52, which is formed opposite the wall of the nozzle clamping element 16. Below the mounting groove 58 or the second spherical shape 52 formed on the inside of the nozzle tensioning element 16 extends an area with reduced material thickness 72 or a region in which a perforation pattern 62 extends from the recesses 66 shown in connection with FIGS. 3 and 4.
Im in Figur 7 dargestellten montierten Zustand 80 des Düsenspannelementes 16 weist dieses einen nur schematisch dargestellten Dehnbereich 72 beziehungsweise 62 auf, der entweder in einer reduzierten Materialstärke ausgebildet sein kann oder in den das Lochungsmuster 62 aus Aussparungen 66 verläuft. In the mounted state 80 of the nozzle clamping element 16 shown in FIG. 7, the latter has an expansion region 72 or 62, which is shown only schematically, which can be formed either in a reduced material thickness or in which the perforation pattern 62 extends from recesses 66.

Claims

Patentansprüche claims
1. Kraftstoffϊnjektor (10) zum Einspritzen von Kraftstoff in den Brennraum einer Verbrennungskraftmaschine, mit einem Haltekörper (14) und zumindest einem Düsen- körper (22), wobei der Düsenkörper (22) mittels eines Düsenspannelementes (16) unterA fuel injector (10) for injecting fuel into the combustion chamber of an internal combustion engine, comprising a holding body (14) and at least one nozzle body (22), wherein the nozzle body (22) by means of a nozzle clamping element (16) under
Vorspannung am Haltekörper (14) des Kraftstoffinjektors (10) befestigt ist, dadurch gekennzeichnet, dass das Düsenspannelement (16) mit dem Haltekörper (14) durch eine Rastverbindung (46, 56) verbunden ist.Preload on the holding body (14) of the fuel injector (10) is fixed, characterized in that the nozzle clamping element (16) with the holding body (14) by a latching connection (46, 56) is connected.
2. Kraftstoffinjektor gemäß der Darstellung gemäß Anspruch 1, dadurch gekennzeichnet, dass das Düsenspannelement (16) einen Fixierbereich (42) aufweist, in welchem eine Anzahl von Arretierzungen (44) ausgebildet sind, die voneinander durch Spalte (48) getrennt sind.2. Fuel injector according to the illustration according to claim 1, characterized in that the nozzle clamping element (16) has a fixing region (42) in which a number of locking tongues (44) are formed, which are separated from each other by gaps (48).
3. Kraftstoffinjektor (10) gemäß Anspruch 2, dadurch gekennzeichnet, dass innerhalb des Fixierbereiches (42) des Düsenspannelementes (16) an Arretierzungen (44) Vorsprünge (46) ausgebildet sind.3. fuel injector (10) according to claim 2, characterized in that within the fixing region (42) of the nozzle clamping element (16) on locking tongues (44) projections (46) are formed.
4. Kraftstoffinjektor (10) gemäß Anspruch 2, dadurch gekennzeichnet, dass das Düsen- spannelement (16) unterhalb des Fixierbereiches (42) an einer Innenumfangsfläche mindestens eine ballige Ausformung (50, 52) aufweist.4. fuel injector (10) according to claim 2, characterized in that the nozzle tensioning element (16) below the fixing region (42) on an inner circumferential surface at least one spherical shape (50, 52).
5. Kraftstoffinjektor (10) gemäß Anspruch 1, dadurch gekennzeichnet, dass das Düsenspannelement (16) an seiner Innenumfangsfläche bevorzugt zwei ballige Ausformungen (50, 52) aufweist, die im montierten Zustand (80) des Düsenspannelementes (16) am5. fuel injector (10) according to claim 1, characterized in that the nozzle clamping element (16) on its inner peripheral surface preferably has two spherical formations (50, 52) in the mounted state (80) of the nozzle clamping element (16) on
Haltekörper (14) mindestens eine Abdichtfläche bilden.Holding body (14) form at least one sealing surface.
6. Kraftstoffinjektor (10) gemäß Anspruch 5, dadurch gekennzeichnet, dass die erste ballige Ausformung (50) und die zweite ballige Ausformung (52) in Bezug auf die Außen- umfangsfläche des Haltekörpers (14) zur Erzeugung von radialen Vorspannungen mit6. Fuel injector (10) according to claim 5, characterized in that the first spherical shape (50) and the second spherical shape (52) with respect to the outer circumferential surface of the holding body (14) for generating radial biases with
Übermaß gefertigt sind.Oversize are made.
7. Kraftstoffinjektor (10) gemäß Anspruch 1, dadurch gekennzeichnet, dass das Düsenspannelement (16) einen Umfangsabschnitt (62, 72) mit definiert einstellbarer axialer Steifigkeit aufweist. 7. fuel injector (10) according to claim 1, characterized in that the nozzle clamping element (16) has a peripheral portion (62, 72) with defined adjustable axial stiffness.
8. Kraftstoffϊnjektor (10) gemäß Anspruch 7, dadurch gekennzeichnet, dass innerhalb des Bereiches mit definiert einstellbarer axialer Steifigkeit ein Lochungsmuster (62) aus ringförmig verteilt angeordneten Aussparungen (66) ausgebildet ist.8. Kraftstoffϊnjektor (10) according to claim 7, characterized in that within the range with defined adjustable axial stiffness, a perforation pattern (62) of annularly distributed arranged recesses (66) is formed.
9. Kraftstoffinjektor (10) gemäß Anspruch 7, dadurch gekennzeichnet, dass innerhalb des Bereiches mit definiert einstellbarer axialer Steifigkeit des Düsenspannelementes (16) das Düsenspannelement (16) mit reduzierter Materialstärke (72) ausgeführt ist.9. fuel injector (10) according to claim 7, characterized in that within the range defined with adjustable axial stiffness of the nozzle clamping element (16), the nozzle clamping element (16) with reduced material thickness (72) is executed.
10. Kraftstoffinjektor (10) gemäß Anspruch 1, dadurch gekennzeichnet, dass das Düsen- spannelement (16) im montierten Zustand (80) am Haltekörper (14) mit Arretierzungen10. Fuel injector (10) according to claim 1, characterized in that the nozzle tensioning element (16) in the mounted state (80) on the holding body (14) with locking tongues
(44) in der Rastnut (56) verrastet ist und das Düsenspannelement (16) mit einer Auflagefläche (54) den Düsenkörper (22) gegen den Haltekörper (14) vorspannt und die erste ballige Ausformung (50) eine erste Abdichtung zum Haltekörper (14) und die zweite ballige Ausformung (52) eine zweite Abdichtfläche am Umfang (78) des Düsenkörpers (22) bildet. (44) is latched in the latching groove (56) and the nozzle tensioning element (16) with a bearing surface (54) biases the nozzle body (22) against the holding body (14) and the first spherical shape (50) forms a first seal to the holding body (14 ) and the second spherical shape (52) forms a second sealing surface on the circumference (78) of the nozzle body (22).
EP07788488A 2006-10-20 2007-08-20 Fuel injector Not-in-force EP2084393B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006049532A DE102006049532A1 (en) 2006-10-20 2006-10-20 Screw connection for fuel injector
PCT/EP2007/058598 WO2008046680A1 (en) 2006-10-20 2007-08-20 Screw connection for fuel injector

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Publication Number Publication Date
EP2084393A1 true EP2084393A1 (en) 2009-08-05
EP2084393B1 EP2084393B1 (en) 2010-01-20

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EP07788488A Not-in-force EP2084393B1 (en) 2006-10-20 2007-08-20 Fuel injector

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EP (1) EP2084393B1 (en)
CN (1) CN101529084B (en)
AT (1) ATE455956T1 (en)
DE (2) DE102006049532A1 (en)
WO (1) WO2008046680A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011086005A1 (en) * 2011-11-09 2013-05-16 Robert Bosch Gmbh Fuel injector, method for mounting a fuel injector and clamping device for mounting a fuel injector
DE102012217991A1 (en) * 2012-10-02 2014-04-03 Continental Automotive Gmbh Nozzle assembly for a fluid injector and fluid injector
DE102013018177B4 (en) * 2013-11-29 2016-01-28 L'orange Gmbh Fuel injector module and fuel injector and test arrangement with it
DE102018217768A1 (en) * 2018-10-17 2020-04-23 Robert Bosch Gmbh Injector arrangement
EP3935276A4 (en) * 2019-04-15 2022-10-19 Cummins, Inc. Fuel injector with radially orientable nozzle holes using splines
DE102020113609A1 (en) 2020-03-31 2021-09-30 Liebherr-Components Deggendorf Gmbh Fuel injector

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2024315A (en) * 1978-07-01 1980-01-09 Lucas Industries Ltd Fuel injection nozzle
US5724946A (en) * 1996-11-22 1998-03-10 Siemens Automotive Corporation Fuel rail and injector assembly
US5735555A (en) * 1996-12-18 1998-04-07 Siemens Automotive Corporation Fuel rail to fuel tube end compact connector
US6511004B2 (en) * 2000-01-19 2003-01-28 Delphi Technologies, Inc. Fuel injector cover
US6676044B2 (en) * 2000-04-07 2004-01-13 Siemens Automotive Corporation Modular fuel injector and method of assembling the modular fuel injector
DE10103933A1 (en) * 2001-01-30 2002-08-14 Bosch Gmbh Robert Fuel injector
DE10148874C2 (en) * 2001-10-04 2003-12-24 Siemens Ag Nozzle device, in particular for fuel injection

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2008046680A1 *

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WO2008046680A1 (en) 2008-04-24
EP2084393B1 (en) 2010-01-20
DE502007002705D1 (en) 2010-03-11
CN101529084B (en) 2011-08-24
CN101529084A (en) 2009-09-09
ATE455956T1 (en) 2010-02-15
DE102006049532A1 (en) 2008-04-24

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