EP0920359A1 - Valve and method for producing a valve seat for a valve - Google Patents

Valve and method for producing a valve seat for a valve

Info

Publication number
EP0920359A1
EP0920359A1 EP98931957A EP98931957A EP0920359A1 EP 0920359 A1 EP0920359 A1 EP 0920359A1 EP 98931957 A EP98931957 A EP 98931957A EP 98931957 A EP98931957 A EP 98931957A EP 0920359 A1 EP0920359 A1 EP 0920359A1
Authority
EP
European Patent Office
Prior art keywords
valve
perforated disk
area
seat
sheet metal
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
EP98931957A
Other languages
German (de)
French (fr)
Other versions
EP0920359B1 (en
Inventor
Wilhelm Hopf
Dieter Holz
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 EP0920359A1 publication Critical patent/EP0920359A1/en
Application granted granted Critical
Publication of EP0920359B1 publication Critical patent/EP0920359B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00Making other particular articles
    • B21D53/10Making other particular articles parts of bearings; sleeves; valve seats or the like
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1853Orifice plates
    • F02M61/186Multi-layered orifice plates
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • F02M51/0671Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto
    • F02M51/0682Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto the body being hollow and its interior communicating with the fuel flow
    • 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
    • F02M61/162Means to impart a whirling motion to fuel upstream or near discharging orifices
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, 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
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/188Spherical or partly spherical shaped valve member ends
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49298Poppet or I.C. engine valve or valve seat making
    • Y10T29/49306Valve seat making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49405Valve or choke making
    • Y10T29/49409Valve seat forming
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49405Valve or choke making
    • Y10T29/49412Valve or choke making with assembly, disassembly or composite article making
    • Y10T29/49416Valve or choke making with assembly, disassembly or composite article making with material shaping or cutting
    • Y10T29/49423Valve or choke making with assembly, disassembly or composite article making with material shaping or cutting including metal deforming

Definitions

  • the invention relates to a valve according to the preamble of claim 1 and a method for producing a valve seat for a valve according to the preamble of claim 13 and claim 14.
  • valve seat body is produced by means of a machining process.
  • the valve seat body must be subjected to a subsequent fine machining in the area of the valve seat after the machining preprocessing in order to achieve the accuracy required for the sealing function when interacting with a spherical valve closing body.
  • a separately manufactured spray orifice plate is sealingly connected by welding. The heat exposure during welding can disadvantageously lead to an undesirable deformation of the Guide the spray hole disc.
  • two components have to be produced separately from one another, which are only connected to one another subsequently and possibly still have to be reworked, which overall leads to a relatively high production outlay.
  • valve seat and perforated disk function are integrated in a simple manner in a single component, such a perforated disk element being particularly simple, inexpensive and material-saving to produce by mass production of large quantities.
  • the design of the perforated disc element with several functional areas as a sheet metal laminate element not only leads to easy workability and low weight due to the reduction in the number of components, but also to a reduction in the material requirement.
  • the multi-layer structure of the perforated disc element made of sandwich-like sheets allows the opening geometry to be designed in such a way that even, very fine atomization of the medium to be sprayed off is achieved without additional energy, a particularly high level
  • Atomization quality and a beam shaping adapted to the respective requirements is achieved.
  • An S stroke is advantageously achieved in the flow of the medium, for example a fuel.
  • the perforated disk element advantageously has functional areas for spraying off the medium and influencing its flow (bottom area), for opening and
  • valve Closing the valve (seat area), for guiding the axially movable valve closing body (guide area) and for fastening in the valve (holding area).
  • a large number of functions are therefore performed by a single valve component.
  • the S-blow in the flow achieved by the geometrical arrangement of the opening geometry allows the formation of strange jet shapes with a high atomization quality.
  • the perforated disc elements allow for one, two and
  • Multi-jet sprays Cross-sections in countless variants, such as B. rectangles, triangles, crosses, ellipses.
  • Such unusual beam shapes allow an exact optimal adaptation to given geometries, e.g. B. to different intake manifold cross sections of internal combustion engines.
  • the exhaust gas emission of the internal combustion engine can consequently be reduced and the fuel consumption can also be reduced.
  • flow openings in the guide region of the perforated disk element, so that an unimpeded flow of the medium in the direction of the valve seat is made possible.
  • these flow openings have an orientation such that a medium flowing through them is subject to swirl.
  • the method according to the invention for the production of a valve seat for a valve with the characterizing features of claims 13 and 14 have the advantage that multilayer perforated disk elements made of metal can be produced very effectively and in large numbers at low cost through their use in a simple manner (line production). In a particularly advantageous manner, a simple and inexpensive location assignment of individual sheet foils or the sheet layers of the later one is possible
  • Perforated disk elements realized through auxiliary openings, so that there is a very high level of manufacturing reliability.
  • the sheet metal foils can be assigned automatically via optical scanning and image evaluation.
  • the material, the sheet thickness, the desired opening geometries and other parameters can be ideally adapted for the respective application.
  • the blanks which are initially in a band and later separated, are reshaped in such a way that perforated disk elements are formed which have at least one base region with the opening geometry and one seat region with a valve seat surface.
  • the perforated disk elements comprising several sheet metal layers thus combine valve seat and perforated disk functions in one component each.
  • Welding, soldering or gluing in all of their different forms of application ideally serve as an optional joining method for connecting several sheet metal foils inside or outside the circular blanks.
  • the blanks are separated in a particularly advantageous manner with a cutting tool of a deep-drawing tool, in which the blanks are also shaped into cup-shaped perforated disk elements.
  • FIG. 1 shows a partially illustrated injection valve with a first perforated disk element according to the invention
  • FIG. 2 shows a schematic diagram of the process sequence for producing a perforated disk element
  • FIG. 3 shows an exemplary embodiment of a film strip for a later sheet metal layer
  • FIGS. 4 and 5 in detail, two examples of perforated disk elements with differently shaped holding areas, FIGS. 6 to 8 a deep-drawing tool with a band to be processed in different processing stages, FIG. 9 schematically, a chronological sequence when forming a circular blank into a perforated disk element, a two-layer perforated disk element and FIG. 11 shows a second example of a two-layer perforated disk element.
  • FIG. 1 a valve in the form of an injection valve for fuel injection systems of mixture-compressing spark-ignition internal combustion engines is partially shown as an exemplary embodiment.
  • the injection valve has a tubular valve seat support 1, in which a longitudinal opening 3 is formed concentrically with a valve longitudinal axis 2.
  • a longitudinal opening 3 is formed concentrically with a valve longitudinal axis 2.
  • a z. B. tubular valve needle 5 arranged at its downstream end 6 with a z. B. spherical valve closing body 7 is connected.
  • the injection valve is actuated in a known manner, for example electromagnetically.
  • An indicated electromagnetic circuit with a magnet coil 10, an armature 11 and a core 12 serves for the axial movement of the valve needle 5 and thus for opening against the spring force of a return spring (not shown) or closing the injection valve.
  • the armature 11 is facing away from the valve closing body 7 End of the valve needle 5 by z. B. one produced by means of a laser
  • a guide opening 15 of a perforated disk element 16 is used to guide the valve closing body 7 during the axial movement.
  • the perforated disk element 16 is tightly mounted by welding in the downstream end of the valve seat carrier 1, which is remote from the core 12, in the longitudinal opening 3 which is concentric with the longitudinal axis 2 of the valve.
  • the perforated disk element 16 represents a combination of a perforated disk and a valve seat body of conventional valves, in particular fuel injection valves, and thus simultaneously fulfills the functions of both components that are otherwise used.
  • the perforated disc element 16 is made of at least two, in the exemplary embodiment according to FIG. 1, three metal ones having a small thickness
  • Sheet metal layers 20 are formed so that there is a so-called laminated perforated disk which also functions as a valve seat.
  • the perforated disk element 16 is produced from a plurality of flat sheet metal foils which are deformed, for example by deep drawing or cups, in such a way that differently oriented regions of the perforated disk element 16 arise.
  • the perforated disk element 16 has at least a central base region 22 with a desired opening geometry 23, a seat region 24 which adjoins radially outward with an inner valve seat surface 25, a subsequent guide region 26 with the inner guide opening 15 and an outer holding region 28 which forms the radial closure on.
  • a connection area 30 can optionally be provided, which, for example, runs parallel to the bottom area 22 and perpendicular to the longitudinal axis 2 of the valve, as in FIG.
  • the insertion depth of the perforated disk element 16 serving as the valve seat part into the longitudinal opening 3 determines the size of the stroke of the valve needle 5, since the one end position of the valve needle 5 when the magnet coil 10 is not energized due to the valve closing body 7 resting against the valve
  • Valve seat 25 of the seat area 24 is fixed.
  • the other end position of the valve needle 5 is when excited Magnetic coil 10 is fixed, for example, by the armature 11 bearing against the core 12.
  • the path between these two end positions of the valve needle 5 thus represents the stroke.
  • the spherical valve closing body 7 interacts with the valve seat surface 25 of the seat area 24 of the perforated disk element 16 which tapers in the shape of a truncated cone and is formed in the axial direction between the guide area 26 and the base area 22.
  • the guide area 26, the seat area 24 and the bottom area 22 together form an inner pot of the perforated disk element 16, which largely receives and encloses the spherical valve closing body 7.
  • FIG. 2 shows a basic diagram of the process sequence in the production of a perforated disk element 16 according to the invention, the individual production and processing stations being shown only symbolically. Individual processing steps are explained in more detail with the aid of the following figures.
  • A In the first station, denoted by A, there are sheet metal foils corresponding to the desired number of sheet metal layers 20 of the later perforated disk element 16 as, for example, rolled-up foil strips 35.
  • three film strips 35a, 35b and 35c for the production of a three sheet layers 20 comprising
  • Sheet metal laminated perforated disk element 16 for later processing, especially when joining, is expedient to coat the middle film strip 35b.
  • the film strips 35 a large number of identical opening geometries 23 per film strip 35 and
  • Auxiliary openings 54, 55 for centering and adjusting the film strips 35 or for later exposure of the Perforated disk elements 16 introduced from the film strip 35.
  • FIG. 3 illustrates an example of a film strip 35a processed in this way.
  • the film strips 35 pass through the station C, which is a heating device 37 in which the film strips 35 are inductively heated, for example in preparation for a soldering process.
  • Station C is only provided as an option, since at any time others, one
  • Heating methods not required for connecting the foil strips 35 can be used.
  • the individual film strips 35 are joined to one another, the film strips 35 being positioned exactly with respect to one another by means of centering devices and being pressed together and transported, for example by rotating pressure rollers 38.
  • a centering device (index pins, index bolts), which is not shown, engages in the auxiliary openings 54 and ensures that the round plates 58 of the individual film strips 35 are dimensionally accurate and one above the other brought before the film strips 35 are connected together.
  • Laser welding, light beam welding, electron beam welding, ultrasonic welding, pressure welding, induction soldering, laser beam soldering, electron beam soldering, gluing or other known processes can be used as joining processes.
  • the fixed connections of the film strips 35 can be made both inside the round plates 58 (eg in the area of the later seating area 24) and outside the round plates 58 near the film edges 56 or in central areas of the band 39 between two opposite auxiliary openings 54.
  • the band 39 comprising a plurality of layers of film strips 35 is processed in station E in such a way that perforated disk elements 16 are of the size and contour desired for installation in the injection valve.
  • the station E also separates the perforated disk elements 16, for example by punching them out of the band 39 or by tearing them off in a tool 40, in particular a deep-drawing tool.
  • Perforated disk elements 16 are separated from the band 39, for example by tearing, and are thus separated, the perforated disk elements 16 at the same time being provided directly with a pot-shaped shape. If punching out is carried out differently than in a deep-drawing tool, deep-drawing or cuping is still required after punching out.
  • the perforated disk elements 16 are subsequently installed in the valve seat support 1.
  • the perforated disk elements 16 are made with the aid of a joining device (not shown) attached, a laser welding device is advantageously used to achieve a firm and tight connection.
  • FIG. 3 shows a specific exemplary embodiment of a film strip 35a for a perforated disk element 16.
  • the film strip 35a represents the upper sheet metal layer 20a which will later face the valve closing body 7.
  • two to five film strips 35, each with a thickness, are arranged one above the other for the sheet metal laminate perforated disk elements 16 from 0.05 mm to 0.3 mm, in particular approximately 0.1 mm.
  • Each film strip 35 is provided in station B with an opening geometry 23 which is repeated in large numbers over the length of the film strips 35.
  • Film strips 35a have an opening geometry 23 in the form of a double H-shaped inlet opening 23a. At the same time, openings, such as passage openings 23b or spray openings 23c, are formed in the other film strips, each with different opening contours. In addition to the opening geometries 23, the flow openings 50 and auxiliary openings 54 and 55 are introduced in station B.
  • Opening geometries 23 are formed at equal intervals near the film edges 56, auxiliary openings 54 as centering openings, which can be angular or circular, depending on the shape of the tools or aids that will later intervene there.
  • the auxiliary openings 54 can also be provided as groove-like centering and feed recesses directly on the film edges 56.
  • Other Auxiliary openings 55 are crescent-shaped, the respective opening geometries 23 and, in the upper sheet metal layer 20a, the flow openings 50 surrounding the film strips 35 are provided as openings.
  • the four crescent-shaped auxiliary openings 55 enclose with their inner contour a circle with a diameter with which the size of the perforated disk element 16 is determined.
  • the circular areas enclosed by the auxiliary openings 55 in the film strips 35 are referred to as round plates 58.
  • the auxiliary openings 55 taper to a point at their ends, narrow webs 59 being formed between the individual auxiliary openings 55 and having a width of only 0.2 to 0.3 mm in the region of the round diameter.
  • the webs 59 tear, as a result of which the perforated disk elements 16 are exposed.
  • a plurality of film strips 35 can also be combined to form a larger film carpet, on which the round plates 58 are arranged in two dimensions.
  • Sheet metal layers 20b, 20c facing away from valve closing body 7 in the inner pot only the central opening geometries 23b, 23c and the auxiliary openings 54, 55 are formed, the upper sheet metal layer 20a facing valve closing body 7 is additionally inserted
  • the flow openings 50 are, for example, drop-shaped and surround the inner inlet opening 23a in a ring shape.
  • the individual flow openings 50 do not run exactly radially in the direction of the center of the disk, but instead have a certain degree of rotation. So is a medium flowing through in a very simple way a swirl component can be impressed.
  • the inclined position of the flow openings 50 determines the swirl of the flow.
  • the flow openings 50 can also be introduced in such a way that a medium flowing through them reaches the seat area 24 or the floor area 22 radially and without swirl.
  • the flow openings 50 are located in the guide region 26 in the perforated disk element 16, as is clearly illustrated in FIGS. 4 and 5.
  • the material areas of the upper sheet-metal layer 20a remaining between the flow openings 50 represent narrow, web-like guide surfaces 60 for guiding the valve needle 5 or the valve closing body 7. Due to the flow openings 50 provided in the perforated disk element 16, one can advantageously be introduced
  • FIGS. 4 and 5 show sections of two examples of perforated disk elements 16, all areas 22, 24, 26, 28 and 30 being at least partially recognizable.
  • At least the upper sheet metal layer 20a should consist of a hardenable material in order to harden the valve seat surface 25 of the seat area 24 after the deep drawing. This can be done, for example, in a ring in a circumferential strip 62, as indicated in FIG. 5. However, hardening can also be carried out over a larger area. Induction hardening, induction pulse hardening, laser beam hardening and electron beam hardening are particularly suitable. There is no need for hardening if the strain hardening is already sufficient due to the forming.
  • valve seat surface 25 of the seat area 24 is, for example so that the valve closing body 7 of the original valve needle 5 is provided with a thin, slightly abrasive, ideally detachable layer with which the valve seat is “ground in.” The applied layer is then loosened (under pressure) and rinsed out. Crystalline layers are ideal Salt, soda or the like, which can be loosened and rinsed out after the processing without leaving any residues.
  • the inner pot and the outer holding edge of the perforated disk element 16 are formed in the desired shape by deep-drawing or cuping the rounds 58 in the station E. If the blank diameters in the individual film strips 35 are selected to be the same size, the deep-drawing of the sheet-metal layers 20 creates the holding area 28, which is stepped at its free end.
  • the diameters of the round blanks 58 can, however, also be set in different sizes from the outset, so that after deep drawing e.g. the outer
  • Sheet metal layers 20 of the holding area 28 end in one plane at the free end and the inner sheet metal layer 20c of the holding area 28 further downstream on local.
  • the protruding end 63 of the sheet metal layer 20c can be folded over, for example by bending or flanging, under the other sheet metal layer ends (FIG. 5), as a result of which a simpler attachment, for example to the valve seat support 1, can be achieved by means of the weld seam 32.
  • the deep-drawing tool 40 which is traversed by the belt 39, is shown schematically in FIGS. 6 to 8.
  • the band 39 rests with the edge areas outside the auxiliary openings 55 near the film edges 56, for example on a workpiece support 65, against which it is pressed by means of a hold-down device 66.
  • the workpiece supports 65 belong to a die 67 as part of the deep-drawing tool 40.
  • the die 67 has an at least partially frustoconical or curved opening 68, which takes over the actual die function for shaping the round plates 58 into perforated disk elements 16.
  • An opening 69 is also provided in the hold-down device 66, which opening is predetermined by the inner wall of a sleeve-shaped cutting tool 70.
  • a punch 71 is arranged to be movable perpendicular to the plane of the band 39 and is surrounded by the cutting tool 70, which is also movable.
  • a stamp counterpart 72 is provided on the side of the band 39 opposite the stamp 71, a stamp counterpart 72 is provided in the partially curved but also partially cylindrical opening 68 of the die 67, which follows the movement of the stamp 71, the cylindrical portion of the opening 68 guiding the stamp counterpart 72 serves.
  • the cutting tool 70 moves perpendicular to the plane of the band 39, as indicated by the arrows in FIG. 7. Due to the precisely centered and defined movement of the punch 71 and the cutting tool 70 against the punch counterpart 72 in the opening 68 of the die 67 at a high surface pressure with a force which is greater than the counterforce of the punch counterpart 72, the blank 58 is cut out very precisely from the band 39 by a cutting edge of the cutting tool 70.
  • the cutting tool 70 comes to a standstill on a shoulder 73 of the opening 68 in the die 67, and at the same time it fixes the round plate 58 in the subsequent step
  • a sheet edge 75 remains torn from the round blank 58 as waste in the deep-drawing tool 40, which, however, can be recycled and used in the production of new sheet metal foils.
  • a firm connection of the film strips 35 in station D can be completely dispensed with if the holding area 28 of the
  • Perforated disk element 16 in a strongly bent shape e.g. is generated almost perpendicular to the bottom region 22 (as shown in FIG. 1), as a result of which sufficiently strong connections are created in the bending regions.
  • FIG. 9 shows an exemplary embodiment of a chronological sequence when a round blank 58 is formed into a Perforated disk element 16 shown. It can be seen that several deep-drawing or bending processes are necessary in order to obtain a desired shape of the perforated disk element 16 with the areas 22, 24, 26, 28 and 30.
  • the round blank 58 can also be shaped in a different order than that shown in FIG.
  • the spray openings 23c with an offset to the inlet opening 23a, so that the inlet opening 23a does not cover the spray openings 23c at any point in the projection.
  • the offset can be different in different directions.
  • the passage opening 23b is designed as a channel (cavity) connecting the inlet opening 23a with the spray openings 23c.
  • the S impact within the perforated disk element 16 with several strong flow deflections imparts a strong, atomization-demanding turbulence to the flow.
  • the velocity gradient across the flow is therefore particularly pronounced. It is an expression of the change in speed across the flow, with the speed in the middle of the flow being significantly greater than near the walls.
  • the increased shear stresses in the fluid resulting from the speed differences promote the disintegration into fine droplets near the spray openings 23c. Since the flow in the outlet is detached on one side due to the impressed radial component, it experiences this due to the lack of contour guidance no flow calming.
  • the fluid has a particularly high speed on the detached side. The turbulence and shear stresses required for atomization are therefore not destroyed in the outlet.
  • the transverse impulses across the flow caused by the turbulence lead, among other things, to the
  • Droplet distribution density in the sprayed spray has great uniformity. This results in a reduced likelihood of droplet coagulation, that is, of associations of small droplets into larger drops.
  • the result of the advantageous reduction in the average droplet diameter in the spray is a relatively homogeneous spray distribution.
  • the S blow creates a fine-scale (high-frequency) turbulence in the fluid, which causes the jet to disintegrate into correspondingly fine droplets immediately after emerging from the perforated disk element 16.
  • FIGS. 10 and 11 show two examples of simple, two-layer perforated disk elements 16 according to the invention, in which the parts which are the same or have the same effect as the embodiment shown in FIG. 1 are identified by the same reference numerals.
  • the perforated disc element 16 in FIG. 10 has two sheet-metal layers 20a and 20c, which, starting from the circular blank 58, were shaped in such a way that the central base region 22 with the opening geometry 23, the seat region 24 with the valve seat surface 25 and the guide region 26 with the flow openings 50 are provided are. These three areas 22, 24 and 26 in turn form a pot.
  • the guide area 26 serves at the same time as a holding area 28; a connection area 30 is not provided at all.
  • the guide region 26 is therefore already in contact with the wall of the valve seat carrier 1 in the longitudinal opening 3 with its sheet metal layer 20c facing away from the valve closing body 7.
  • Perforated disk element 16 and valve seat carrier 1 is achieved by the weld seam 32, which is attached to the valve seat carrier 1, for example, in the angled transition from the guide region 26 and the seat region 24.
  • the inlet openings 23a of the sheet metal layer 20a have a partial offset to the spray openings 23c of the sheet metal layer 20c.
  • the exemplary embodiment according to FIG. 11 has a differently designed seating area 24.
  • the seating area 24 is provided with a bulge 77 from its frustoconical contour, which is directed towards the valve closing body 7 and which faces the valve closing body 7
  • Sheet metal layer 20a has the annular valve seat surface 25.
  • the bead 77 also serves to stiffen the perforated disk element 16. The introduction of the bead 77 also simplifies the attachment of the weld seam 32, since tool access is facilitated in the connection area.

Abstract

The valve provided for in the invention is characterized in that it comprises a perforated disk (16) having at least two metallic sheet layers (20) contacting each other in a sandwich-like manner. Said perforated disk (16) comprises at least one floor area (22) having an opening geometry (23) required for injecting the medium and a seat area (24) with a valve seat surface (25) in such a way that the functions of the valve seat and the perforated disk are combined in one laminated sheet element. The invention also provides for a method for producing a valve seat for such a valve from metal sheets arranged in a sandwich-like manner. Said valve is especially suited for use in fuel injection units of spark-ignited internal combustion engines with mixture compression.

Description

Ventil und Verfahren zur Herstellung eines Ventilsitzes für ein VentilValve and method for manufacturing a valve seat for a valve
Stand der TechnikState of the art
Die Erfindung geht aus von einem Ventil nach der Gattung des Anspruchs 1 sowie von einem Verfahren zur Herstellung eines Ventilsitzes für ein Ventil nach der Gattung des Anspruchs 13 bzw. des Anspruchs 14.The invention relates to a valve according to the preamble of claim 1 and a method for producing a valve seat for a valve according to the preamble of claim 13 and claim 14.
Aus der DE-OS 42 21 185 ist bereits ein Einspritzventil zum Einspritzen von Brennstoff in ein Saugrohr bekannt, bei dem der Ventilsitzkörper mittels eines spanenden Fertigungsverfahrens hergestellt ist. Der Ventilsitzkörper muß im Bereich des Ventilsitzes nach der spanenden Vorbearbeitung einer sich anschließenden Feinstbearbeitung unterzogen werden, um die für die Dichtfunktion notwendige Genauigkeit beim Zusammenwirken mit einem kugelförmig ausgebildeten Ventilschließkörper zu erreichen. Mit dem Ventilsitzkörper ist an dessen stromabwärtiger Stirnseite eine separat gefertigte Spritzlochscheibe durch Schweißen dichtend verbunden. Die Wärmeeinwirkung beim Schweißen kann dabei nachteilig zu einer unerwünschten Deformation der Spritzlochscheibe führen. Für dieses zweiteilige Ventilsitzteil müssen zwei Bauteile getrennt voneinander hergestellt werden, die erst nachfolgend miteinander verbunden werden und eventuell gemeinsam noch nachbearbeitet werden müssen, was insgesamt zu einem relativ hohen Fertigungsaufwand führt.From DE-OS 42 21 185 an injection valve for injecting fuel into an intake manifold is already known, in which the valve seat body is produced by means of a machining process. The valve seat body must be subjected to a subsequent fine machining in the area of the valve seat after the machining preprocessing in order to achieve the accuracy required for the sealing function when interacting with a spherical valve closing body. On the downstream end face of the valve seat body, a separately manufactured spray orifice plate is sealingly connected by welding. The heat exposure during welding can disadvantageously lead to an undesirable deformation of the Guide the spray hole disc. For this two-part valve seat part, two components have to be produced separately from one another, which are only connected to one another subsequently and possibly still have to be reworked, which overall leads to a relatively high production outlay.
Vorteile der ErfindungAdvantages of the invention
Das erfindungsgemäße Ventil mit den kennzeichnendenThe valve according to the invention with the characteristic
Merkmalen des Anspruchs 1 hat den Vorteil, daß Ventilsitz- und Lochscheibenfunktion auf einfache Art und Weise in einem einzigen Bauteil integriert sind, wobei ein solches Lochscheibenelement besonders einfach, kostengünstig und materialsparend durch eine Serienfertigung großer Stückzahlen herstellbar ist. Die Gestaltung des Lochscheibenelements mit mehreren Funktionsbereichen als Blechlaminat-Element führt nicht nur zu einer leichten Bearbeitbarkeit und einem geringen Gewicht durch die Reduzierung der Bauteile, sondern auch zu einer Verringerung des Materialbedarfs . Außerdem kann auf Verbindungen von Ventilsitzkörper und Lochscheibe, wie Schweißnähte, verzichtet werden, wodurch eine Ersparnis an Material und Zeit erzielt wird und Dichtheitsprobleme vermieden werden.Features of claim 1 has the advantage that the valve seat and perforated disk function are integrated in a simple manner in a single component, such a perforated disk element being particularly simple, inexpensive and material-saving to produce by mass production of large quantities. The design of the perforated disc element with several functional areas as a sheet metal laminate element not only leads to easy workability and low weight due to the reduction in the number of components, but also to a reduction in the material requirement. In addition, there is no need for connections between the valve seat body and the perforated disk, such as weld seams, which saves material and time and avoids sealing problems.
Der mehrlagige Aufbau des Lochscheibenelements aus sandwichartig angeordneten Blechen erlaubt ein Ausbilden der Öffnungsgeometrie derart, daß eine gleichmäßige Feinstzerstäubung des abzuspritzenden Mediums ohne Zusatzenergie erreicht wird, wobei eine besonders hoheThe multi-layer structure of the perforated disc element made of sandwich-like sheets allows the opening geometry to be designed in such a way that even, very fine atomization of the medium to be sprayed off is achieved without additional energy, a particularly high level
Zerstäubungsgüte und eine an die jeweiligen Erfordernisse angepaßte Strahlformung erzielt wird. In besonders vorteilhafter Weise wird ein S-Schlag in der Strömung des Mediums, z.B. eines Brennstoffs erreicht.Atomization quality and a beam shaping adapted to the respective requirements is achieved. Especially An S stroke is advantageously achieved in the flow of the medium, for example a fuel.
Durch die in den Unteransprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen des im Anspruch 1 angegebenen Ventils möglich.Advantageous further developments and improvements of the valve specified in claim 1 are possible through the measures listed in the subclaims.
In vorteilhafter Weise besitzt das Lochscheibenelement Funktionsbereiche zum Abspritzen des Mediums und dessen Strömungsbeeinflussung (Bodenbereich) , zum Öffnen undThe perforated disk element advantageously has functional areas for spraying off the medium and influencing its flow (bottom area), for opening and
Schließen des Ventils (Sitzbereich) , zum Führen des axial bewegbaren Ventilschließkörpers (Führungsbereich) und zum Befestigen im Ventil (Haltebereich) . Eine Vielzahl von Funktionen führt damit ein einziges Ventilbauteil aus.Closing the valve (seat area), for guiding the axially movable valve closing body (guide area) and for fastening in the valve (holding area). A large number of functions are therefore performed by a single valve component.
Der durch die geometrische Anordnung der Öffnungsgeometrie (Versatz von Abspritzöffnungen zur Einlaßöffnung) erzielte S-Schlag in der Strömung erlaubt die Ausbildung bizarrer Strahlformen mit einer hohen Zerstäubungsgüte. Die Lochscheibenelemente ermöglichen für Ein-, Zwei- undThe S-blow in the flow achieved by the geometrical arrangement of the opening geometry (offset of spray openings to the inlet opening) allows the formation of bizarre jet shapes with a high atomization quality. The perforated disc elements allow for one, two and
Mehrstrahlsprays Strahlquerschnitte in unzähligen Varianten, wie z. B. Rechtecke, Dreiecke, Kreuze, Ellipsen. Solche ungewöhnlichen Strahlformen erlauben eine genaue optimale Anpassung an vorgegebene Geometrien, z. B. an verschiedene Saugrohrquerschnitte von Brennkraftmaschinen. Daraus ergeben sich die Vorteile einer formangepaßten Ausnutzung des verfügbaren Querschnitts zur homogen verteilten, abgasmindernden Gemischeinbringung und einer Vermeidung von abgasschädlichen Wandfilmanlagerungen an der Saugrohrwandung. Mit einem solchen Ventil kann folglich die Abgasemission der Brennkraftmaschine reduziert und ebenso eine Verringerung des Brennstoffverbrauchs erzielt werden. Ganz allgemein ist als sehr bedeutender Vorteil des erfindungsgemäßen Ventils festzuhalten, daß in einfacher Art und Weise Strahlbildvariationen möglich sind.Multi-jet sprays Cross-sections in countless variants, such as B. rectangles, triangles, crosses, ellipses. Such unusual beam shapes allow an exact optimal adaptation to given geometries, e.g. B. to different intake manifold cross sections of internal combustion engines. This results in the advantages of a shape-adapted utilization of the available cross-section for the homogeneously distributed, exhaust-reducing mixture introduction and the avoidance of emissions-harmful wall film deposits on the intake manifold wall. With such a valve, the exhaust gas emission of the internal combustion engine can consequently be reduced and the fuel consumption can also be reduced. In general, it can be stated as a very important advantage of the valve according to the invention that jet pattern variations are possible in a simple manner.
Besonders vorteilhaft ist es, im Führungsbereich des Lochscheibenelements Strömungsöffnungen vorzusehen, so daß ein ungehindertes Strömen des Mediums in Richtung zum Ventilsitz ermöglicht ist. In vorteilhafter Weise besitzen diese Strömungsöffnungen eine derartige Ausrichtung, daß ein sie durchströmendes Medium drallbehaftet wird.It is particularly advantageous to provide flow openings in the guide region of the perforated disk element, so that an unimpeded flow of the medium in the direction of the valve seat is made possible. Advantageously, these flow openings have an orientation such that a medium flowing through them is subject to swirl.
Die erfindungsgemäßen Verfahren zur Herstellung eines Ventilsitzes für ein Ventil mit den kennzeichnenden Merkmalen der Ansprüche 13 bzw. 14 haben den Vorteil, daß durch ihre Anwendung auf einfache Art und Weise sehr effektiv mehrlagige Lochscheibenelemente aus Metall in sehr großer Stückzahl kostengünstig herstellbar sind (Linienfertigung) . In besonders vorteilhafter Weise wird eine einfache und kostengünstige Lagezuordnung einzelner Blechfolien bzw. der Blechlagen der späterenThe method according to the invention for the production of a valve seat for a valve with the characterizing features of claims 13 and 14 have the advantage that multilayer perforated disk elements made of metal can be produced very effectively and in large numbers at low cost through their use in a simple manner (line production). In a particularly advantageous manner, a simple and inexpensive location assignment of individual sheet foils or the sheet layers of the later one is possible
Lochscheibenelemente durch Hilfsöffnungen realisiert, so daß eine sehr hohe Fertigungssicherheit vorliegt. In bevorzugter Weise kann die Lagezuordnung der Blechfolien automatisch über optische Abtastung und Bildauswertung erfolgen. Auf für die Herstellung mehrlagiger Lochscheibenelemente vorgesehenen Maschinen und Automaten können sehr einfach der Werkstoff, die Blechdicke, die gewünschten Öffnungsgeometrien und weitere Parameter für den jeweiligen Anwendungsfall ideal angepaßt werden. In vorteilhafter Weise erfolgt ein Umformen der vorerst in einem Band vorliegenden und später vereinzelten Ronden derart, daß Lochscheibenelemente gebildet werden, die wenigstens einen Bodenbereich mit der Öffnungsgeometrie und einen Sitzbereich mit einer Ventilsitzfläche aufweisen. Die mehrere Blechlagen umfassenden Lochscheibenelemente vereinen somit Ventilsitz- und Lochscheibenfunktion in jeweils einem Bauteil .Perforated disk elements realized through auxiliary openings, so that there is a very high level of manufacturing reliability. In a preferred manner, the sheet metal foils can be assigned automatically via optical scanning and image evaluation. On machines and machines provided for the production of multi-layer perforated disk elements, the material, the sheet thickness, the desired opening geometries and other parameters can be ideally adapted for the respective application. Advantageously, the blanks, which are initially in a band and later separated, are reshaped in such a way that perforated disk elements are formed which have at least one base region with the opening geometry and one seat region with a valve seat surface. The perforated disk elements comprising several sheet metal layers thus combine valve seat and perforated disk functions in one component each.
Besonders vorteilhaft ist es, die Blechfolien in Form von Folienstreifen oder Folienteppichen für die weitere Bearbeitung bereitzustellen.It is particularly advantageous to provide the sheet metal foils in the form of foil strips or foil carpets for further processing.
Durch die in den Unteransprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen des in den Ansprüchen 13 bzw. 14 angegebenen Verfahrens möglich.Advantageous further developments and improvements of the method specified in claims 13 and 14 are possible through the measures listed in the subclaims.
Als optional einzusetzende Fügeverfahren zum Verbinden mehrerer Blechfolien innerhalb oder außerhalb der Ronden dienen in idealer Weise Schweißen, Löten oder Kleben in all ihren unterschiedlichen Anwendungsformen.Welding, soldering or gluing in all of their different forms of application ideally serve as an optional joining method for connecting several sheet metal foils inside or outside the circular blanks.
In besonders vorteilhafter Weise erfolgt das Vereinzeln der Ronden mit einem Schneidwerkzeug eines Tiefziehwerkzeugs, in dem auch das Umformen der Ronden in topfförmige Lochscheibenelemente vorgenommen wird.The blanks are separated in a particularly advantageous manner with a cutting tool of a deep-drawing tool, in which the blanks are also shaped into cup-shaped perforated disk elements.
In vorteilhafter Weise wird die dem Ventilschließkörper zugewandte Blechlage des Sitzbereichs des Lochscheibenelements gehärtet. ZeichnungThe sheet metal layer of the seat area of the perforated disk element facing the valve closing body is hardened in an advantageous manner. drawing
Ausführungsbeispiele der Erfindung sind in der Zeichnung vereinfacht dargestellt und in der nachfolgenden Beschreibung näher erläutert . Es zeigen Figur 1 ein teilweise dargestelltes Einspritzventil mit einem ersten erfindungsgemäßen Lochscheibenelement, Figur 2 ein Prinzipbild des Verfahrensablaufs bei der Herstellung eines Lochscheibenelements, Figur 3 ein Ausführungsbeispiel eines Folienstreifens für eine spätere Blechlage einesEmbodiments of the invention are shown in simplified form in the drawing and explained in more detail in the following description. FIG. 1 shows a partially illustrated injection valve with a first perforated disk element according to the invention, FIG. 2 shows a schematic diagram of the process sequence for producing a perforated disk element, and FIG. 3 shows an exemplary embodiment of a film strip for a later sheet metal layer
Lochscheibenelements, Figuren 4 und 5 ausschnittsweise zwei Beispiele von Lochscheibenelementen mit unterschiedlich ausgeformten Haltebereichen, Figuren 6 bis 8 ein Tiefziehwerkzeug mit einem zu bearbeitenden Band in verschiedenen Bearbeitungsstufen, Figur 9 schematisch eine zeitliche Abfolge beim Umformen einer Ronde in ein Lochscheibenelement, Figur 10 ein erstes Beispiel eines zweilagigen Lochscheibenelements und Figur 11 ein zweites Beispiel eines zweilagigen Lochscheibenelements.Perforated disk element, FIGS. 4 and 5, in detail, two examples of perforated disk elements with differently shaped holding areas, FIGS. 6 to 8 a deep-drawing tool with a band to be processed in different processing stages, FIG. 9 schematically, a chronological sequence when forming a circular blank into a perforated disk element, a two-layer perforated disk element and FIG. 11 shows a second example of a two-layer perforated disk element.
Beschreibung der AusführungsbeispieleDescription of the embodiments
In der Figur 1 ist als ein Ausfuhrungsbeispiel ein Ventil in der Form eines Einspritzventils für Brennstoffeinspritzanla- gen von gemischverdichtenden fremdgezündeten Brennkraftmaschinen teilweise dargestellt. Das Einspritzventil hat einen rohrförmigen Ventilsitzträger 1, in dem konzentrisch zu einer Ventillängsachse 2 eine Längsöffnung 3 ausgebildet ist. In der Längsöffnung 3 ist eine z. B. rohrförmige Ventilnadel 5 angeordnet, die an ihrem stromabwärtigen Ende 6 mit einem z. B. kugelförmigen Ventilschließkörper 7 verbunden ist. Die Betätigung des Einspritzventils erfolgt in bekannter Weise, beispielsweise elektromagnetisch. Zur axialen Bewegung der Ventilnadel 5 und damit zum Öffnen entgegen der Federkraft einer nicht dargestellten Rückstellfeder bzw. Schließen des Einspritzventils dient ein angedeuteter elektromagnetischer Kreis mit einer Magnetspule 10, einem Anker 11 und einem Kern 12. Der Anker 11 ist mit dem dem Ventilschließkörper 7 abgewandten Ende der Ventilnadel 5 durch z. B. eine mittels eines Lasers hergestellteIn FIG. 1, a valve in the form of an injection valve for fuel injection systems of mixture-compressing spark-ignition internal combustion engines is partially shown as an exemplary embodiment. The injection valve has a tubular valve seat support 1, in which a longitudinal opening 3 is formed concentrically with a valve longitudinal axis 2. In the longitudinal opening 3 is a z. B. tubular valve needle 5 arranged at its downstream end 6 with a z. B. spherical valve closing body 7 is connected. The injection valve is actuated in a known manner, for example electromagnetically. An indicated electromagnetic circuit with a magnet coil 10, an armature 11 and a core 12 serves for the axial movement of the valve needle 5 and thus for opening against the spring force of a return spring (not shown) or closing the injection valve. The armature 11 is facing away from the valve closing body 7 End of the valve needle 5 by z. B. one produced by means of a laser
Schweißnaht verbunden und auf den Kern 12 ausgerichtet .Connected weld and aligned to the core 12.
Zur Führung des Ventilschließkörpers 7 während der Axialbewegung dient eine Führungsöffnung 15 eines Lochscheibenelements 16. In das stromabwärts liegende, dem Kern 12 abgewandte Ende des Ventilsitzträgers 1 ist in der konzentrisch zur Ventillängsachse 2 verlaufenden Längsöffnung 3 das Lochscheibenelement 16 durch Schweißen dicht montiert. Das Lochscheibenelement 16 stellt eine Kombination einer Lochscheibe und eines Ventilsitzkörpers üblicher Ventile, insbesondere Brennstoffeinspritzventile, dar und erfüllt somit zugleich die Funktionen beider ansonsten verwendeter Bauteile. Das Lochscheibenelement 16 wird von wenigstens zwei, im Ausführungsbeispiel nach Figur 1 drei eine geringe Dicke aufweisenden, metallenenA guide opening 15 of a perforated disk element 16 is used to guide the valve closing body 7 during the axial movement. The perforated disk element 16 is tightly mounted by welding in the downstream end of the valve seat carrier 1, which is remote from the core 12, in the longitudinal opening 3 which is concentric with the longitudinal axis 2 of the valve. The perforated disk element 16 represents a combination of a perforated disk and a valve seat body of conventional valves, in particular fuel injection valves, and thus simultaneously fulfills the functions of both components that are otherwise used. The perforated disc element 16 is made of at least two, in the exemplary embodiment according to FIG. 1, three metal ones having a small thickness
Blechlagen 20 gebildet, so daß eine sogenannte Blechlaminat- Lochscheibe vorliegt, die auch als Ventilsitz fungiert.Sheet metal layers 20 are formed so that there is a so-called laminated perforated disk which also functions as a valve seat.
Das Lochscheibenelement 16 wird aus mehreren ebenen Blechfolien hergestellt, die beispielsweise durch Tiefziehen oder Näpfen derart verformt werden, daß unterschiedlich ausgerichtete Bereiche des Lochscheibenelements 16 entstehen. So weist das Lochscheibenelement 16 wenigstens einen mittleren Bodenbereich 22 mit einer gewünschten Öffnungsgeometrie 23, einen sich radial nach außen hin anschließenden Sitzbereich 24 mit einer inneren Ventilsitzfläche 25, einen darauffolgenden Führungsbereich 26 mit der inneren Führungsöffnung 15 sowie einen äußeren, den radialen Abschluß bildenden Haltebereich 28 auf. Zwischen dem Führungsbereich 26 und dem Haltebereich 28 kann optional noch ein Verbindungsbereich 30 vorgesehen sein, der z.B. wie in Figur 1 parallel zum Bodenbereich 22 und senkrecht zur Ventillängsachse 2 verläuft. Bis auf den Bodenbereich 22 laufen alle anderen Bereiche 24, 26, 30, 28 ringförmig um den Ventilschließkörper 7 um. Der leicht konisch nach außen hin gebogene Haltebereich 28 übt eine radiale Federwirkung auf die Wandung der Längsöffnung 3 aus. Dadurch wird beim Einschieben des Lochscheibenelements 16 in die Längsöffnung 3 des Ventilsitzträgers 1 eine Spanbildung an der Längsöffnung 3 vermieden. Der Haltebereich 28 des Lochscheibenelements 16 ist an seinem freien Ende mit der Wandung der Längsöffnung 3 beispielsweise durch eine umlaufende und dichte Schweißnaht 32 verbunden. Die dichte Verschweißung verhindert ein Durchströmen von Brennstoff in der Längsöffnung 3 unmittelbar in eine Ansaugleitung der Brennkraftmaschine .The perforated disk element 16 is produced from a plurality of flat sheet metal foils which are deformed, for example by deep drawing or cups, in such a way that differently oriented regions of the perforated disk element 16 arise. For example, the perforated disk element 16 has at least a central base region 22 with a desired opening geometry 23, a seat region 24 which adjoins radially outward with an inner valve seat surface 25, a subsequent guide region 26 with the inner guide opening 15 and an outer holding region 28 which forms the radial closure on. Between the guide area 26 and the holding area 28, a connection area 30 can optionally be provided, which, for example, runs parallel to the bottom area 22 and perpendicular to the longitudinal axis 2 of the valve, as in FIG. Except for the bottom area 22, all other areas 24, 26, 30, 28 run in a ring around the valve closing body 7. The slightly conically bent outward holding area 28 exerts a radial spring effect on the wall of the longitudinal opening 3. As a result, chip formation at the longitudinal opening 3 is avoided when the perforated disk element 16 is inserted into the longitudinal opening 3 of the valve seat carrier 1. The holding area 28 of the perforated disk element 16 is connected at its free end to the wall of the longitudinal opening 3, for example by a circumferential and tight weld seam 32. The tight welding prevents fuel from flowing through the longitudinal opening 3 directly into an intake line of the internal combustion engine.
Die Einschubtiefe des als Ventilsitzteil dienenden Lochscheibenelements 16 in die Längsöffnung 3 bestimmt die Größe des Hubs der Ventilnadel 5, da die eine Endstellung der Ventilnadel 5 bei nicht erregter Magnetspule 10 durch die Anlage des Ventilschließkörpers 7 an derThe insertion depth of the perforated disk element 16 serving as the valve seat part into the longitudinal opening 3 determines the size of the stroke of the valve needle 5, since the one end position of the valve needle 5 when the magnet coil 10 is not energized due to the valve closing body 7 resting against the valve
Ventilsitzfläche 25 des Sitzbereichs 24 festgelegt ist. Die andere Endstellung der Ventilnadel 5 wird bei erregter Magnetspule 10 beispielsweise durch die Anlage des Ankers 11 an dem Kern 12 festgelegt. Der Weg zwischen diesen beiden Endstellungen der Ventilnadel 5 stellt somit den Hub dar.Valve seat 25 of the seat area 24 is fixed. The other end position of the valve needle 5 is when excited Magnetic coil 10 is fixed, for example, by the armature 11 bearing against the core 12. The path between these two end positions of the valve needle 5 thus represents the stroke.
Der kugelförmige Ventilschließkörper 7 wirkt mit der sich in Strömungsrichtung kegelstumpfförmig verjüngenden Ventilsitzfläche 25 des Sitzbereichs 24 des Lochscheibenelements 16 zusammen, die in axialer Richtung zwischen dem Führungsbereich 26 und dem Bodenbereich 22 ausgebildet ist. Der Führungsbereich 26, der Sitzbereich 24 und der Bodenbereich 22 bilden zusammen einen inneren Topf des Lochscheibenelements 16 , der weitgehend den kugelförmigen Ventilschließkörper 7 aufnimmt und umschließt.The spherical valve closing body 7 interacts with the valve seat surface 25 of the seat area 24 of the perforated disk element 16 which tapers in the shape of a truncated cone and is formed in the axial direction between the guide area 26 and the base area 22. The guide area 26, the seat area 24 and the bottom area 22 together form an inner pot of the perforated disk element 16, which largely receives and encloses the spherical valve closing body 7.
Figur 2 zeigt ein Prinzipbild des Verfahrensablaufs bei der Herstellung eines erfindungsgemäßen Lochscheibenelements 16, wobei die einzelnen Fertigungs- und Bearbeitungsstationen nur symbolisch dargestellt sind. Anhand der nachfolgenden Figuren werden einzelne Bearbeitungsschritte noch ausführlicher erläutert. In der ersten, mit A bezeichneten Station liegen entsprechend der gewünschten Anzahl von Blechlagen 20 des späteren Lochscheibenelements 16 Blechfolien als beispielsweise aufgerollte Folienstreifen 35 vor. Bei Verwendung von drei Folienstreifen 35a, 35b und 35c zur Herstellung eines drei Blechlagen 20 umfassendenFIG. 2 shows a basic diagram of the process sequence in the production of a perforated disk element 16 according to the invention, the individual production and processing stations being shown only symbolically. Individual processing steps are explained in more detail with the aid of the following figures. In the first station, denoted by A, there are sheet metal foils corresponding to the desired number of sheet metal layers 20 of the later perforated disk element 16 as, for example, rolled-up foil strips 35. When using three film strips 35a, 35b and 35c for the production of a three sheet layers 20 comprising
Blechlaminat-Lochscheibenelements 16 ist es für die spätere Bearbeitung, speziell beim Fügen, zweckmäßig, den mittleren Folienstreifen 35b zu beschichten. In die Folienstreifen 35 werden nachfolgend jeweils in großer Anzahl gleiche Öffnungsgeometrien 23 pro Folienstreifen 35 sowieSheet metal laminated perforated disk element 16, for later processing, especially when joining, is expedient to coat the middle film strip 35b. In the film strips 35, a large number of identical opening geometries 23 per film strip 35 and
Hilfsöffnungen 54, 55 (Figur 3) zum Zentrieren und Justieren der Folienstreifen 35 bzw. zum späteren Freilegen der Lochscheibenelemente 16 aus den Folienstreifen 35 eingebracht .Auxiliary openings 54, 55 (Figure 3) for centering and adjusting the film strips 35 or for later exposure of the Perforated disk elements 16 introduced from the film strip 35.
Diese Bearbeitung der einzelnen Folienstreifen 35 erfolgt in der Station B. In der Station B sind Werkzeuge 36 vorgesehen, mit denen in den einzelnen Folienstreifen 35 die gewünschten Öffnungsgeometrien 23 sowie die Hilfsöffnungen 54, 55 eingeformt werden. Alle wesentlichen Konturen werden dabei durch Mikrostanzen, Laserschneiden, Erodieren, Ätzen oder vergleichbare Verfahren hergestellt. In den oberen Folienstreifen 35a werden zusätzlich zu den Öffnungsgeometrien 23 und den Hilfsöffnungen 54, 55 noch Strömungsöffnungen 50 (Figur 3) eingebracht. Ein Beispiel eines derart bearbeiteten Folienstreifens 35a veranschaulicht Figur 3. Die Folienstreifen 35 durchlaufen derart bearbeitet die Station C, die eine Erwärmungseinrichtung 37 darstellt, in der die Folienstreifen 35 beispielsweise in Vorbereitung eines Lötvorgangs induktiv erwärmt werden. Die Station C ist nur optional vorgesehen, da jederzeit auch andere, eineThis processing of the individual film strips 35 takes place in station B. In station B, tools 36 are provided, with which the desired opening geometries 23 and the auxiliary openings 54, 55 are formed in the individual film strips 35. All essential contours are produced by micro punching, laser cutting, eroding, etching or comparable processes. In addition to the opening geometries 23 and the auxiliary openings 54, 55, flow openings 50 (FIG. 3) are also introduced into the upper film strip 35a. FIG. 3 illustrates an example of a film strip 35a processed in this way. The film strips 35 pass through the station C, which is a heating device 37 in which the film strips 35 are inductively heated, for example in preparation for a soldering process. Station C is only provided as an option, since at any time others, one
Erwärmung nicht erfordernde Fügeverfahren zur Verbindung der Folienstreifen 35 angewendet werden können.Heating methods not required for connecting the foil strips 35 can be used.
In der Station D erfolgt das Fügen der einzelnen Folienstreifen 35 aufeinander, wobei die Folienstreifen 35 mit Hilfe von Zentriervorrichtungen zueinander genau positioniert werden und beispielsweise durch rotierende Druckwalzen 38 aneinandergedrückt und weitertransportiert werden. In die Hilfsöffnungen 54 greift eine nicht dargestellte Zentriervorrichtung (Indexstifte, Indexbolzen) ein, die dafür sorgt, daß die Ronden 58 der einzelnen Folienstreifen 35 maßgenau und lagesicher übereinander gebracht werden, bevor die Folienstreifen 35 miteinander verbunden werden. Als Fügeverfahren können Laserschweißen, Lichtstrahlschweißen, Elektronenstrahlschweißen, Ultraschallschweißen, Preßschweißen, Induktionslöten, Laserstrahllöten, Elektronenstrahllöten, Kleben oder andere bekannte Verfahren eingesetzt werden. Die festen Verbindungen der Folienstreifen 35 können sowohl innerhalb der Ronden 58 (z.B. im Bereich des späteren Sitzbereichs 24) als auch außerhalb der Ronden 58 nahe der Folienränder 56 oder in zentralen Bereichen des Bandes 39 zwischen jeweils zwei gegenüberliegenden Hilfsöffnungen 54 vorgenommen werden.In station D, the individual film strips 35 are joined to one another, the film strips 35 being positioned exactly with respect to one another by means of centering devices and being pressed together and transported, for example by rotating pressure rollers 38. A centering device (index pins, index bolts), which is not shown, engages in the auxiliary openings 54 and ensures that the round plates 58 of the individual film strips 35 are dimensionally accurate and one above the other brought before the film strips 35 are connected together. Laser welding, light beam welding, electron beam welding, ultrasonic welding, pressure welding, induction soldering, laser beam soldering, electron beam soldering, gluing or other known processes can be used as joining processes. The fixed connections of the film strips 35 can be made both inside the round plates 58 (eg in the area of the later seating area 24) and outside the round plates 58 near the film edges 56 or in central areas of the band 39 between two opposite auxiliary openings 54.
Daran anschließend wird das mehrere Lagen von Folienstreifen 35 umfassende Band 39 in der Station E derart bearbeitet, daß Lochscheibenelemente 16 in der zum Einbau im Einspritzventil gewünschten Größe und Kontur vorliegen. In der Station E erfolgt auch die Vereinzelung der Lochscheibenelemente 16 beispielsweise durch Ausstanzen aus dem Band 39 oder durch Abreißen in einem Werkzeug 40, insbesondere einem Tiefziehwerkzeug. DieSubsequently, the band 39 comprising a plurality of layers of film strips 35 is processed in station E in such a way that perforated disk elements 16 are of the size and contour desired for installation in the injection valve. The station E also separates the perforated disk elements 16, for example by punching them out of the band 39 or by tearing them off in a tool 40, in particular a deep-drawing tool. The
Lochscheibenelemente 16 werden beispielsweise durch Abreißen aus dem Band 39 herausgetrennt und somit vereinzelt, wobei die Lochscheibenelemente 16 zugleich unmittelbar mit einer topfförmigen Gestalt versehen werden. Wird ein Ausstanzen anderweitig als in einem Tiefziehwerkzeug vorgenommen, so ist nach dem Ausstanzen noch ein Tiefziehen oder Näpfen erforderlich.Perforated disk elements 16 are separated from the band 39, for example by tearing, and are thus separated, the perforated disk elements 16 at the same time being provided directly with a pot-shaped shape. If punching out is carried out differently than in a deep-drawing tool, deep-drawing or cuping is still required after punching out.
Nachfolgend erfolgt noch der Einbau der Lochscheibenelemente 16 im Ventilsitzträger 1. Die Lochscheibenelemente 16 werden mit Hilfe einer nicht dargestellten Fügevorrichtung befestigt, wobei in vorteilhafter Weise zur Erzielung einer festen und dichten Verbindung eine Laserschweißeinrichtung verwendet wird.The perforated disk elements 16 are subsequently installed in the valve seat support 1. The perforated disk elements 16 are made with the aid of a joining device (not shown) attached, a laser welding device is advantageously used to achieve a firm and tight connection.
Ein konkretes Ausführungsbeispiel eines Folienstreifens 35a für ein Lochscheibenelement 16 zeigt Figur 3. Dabei stellt der Folienstreifen 35a die später dem Ventilschließkörper 7 zugewandte obere Blechlage 20a dar. Üblicherweise werden für die Blechlaminat-Lochscheibenelemente 16 zwei bis fünf Folienstreifen 35 übereinander angeordnet, die jeweils eine Dicke von 0,05 mm bis 0,3 mm, insbesondere ca. 0,1 mm, aufweisen. Jeder Folienstreifen 35 wird in der Station B mit einer Öffnungsgeometrie 23 versehen, die sich über die Länge der Folienstreifen 35 in großer Zahl wiederholt. Im in Figur 3 dargestellten Ausführungsbeispiel weist der obereFIG. 3 shows a specific exemplary embodiment of a film strip 35a for a perforated disk element 16. The film strip 35a represents the upper sheet metal layer 20a which will later face the valve closing body 7. Usually, two to five film strips 35, each with a thickness, are arranged one above the other for the sheet metal laminate perforated disk elements 16 from 0.05 mm to 0.3 mm, in particular approximately 0.1 mm. Each film strip 35 is provided in station B with an opening geometry 23 which is repeated in large numbers over the length of the film strips 35. In the embodiment shown in Figure 3, the upper one
Folienstreifen 35a eine Öffnungsgeometrie 23 in Form einer doppel-H-förmigen Einlaßöffnung 23a auf. Gleichzeitig werden in den anderen Folienstreifen 35 Öffnungen, wie Durchlaßöffnungen 23b oder Abspritzöffnungen 23c mit jeweils anderen Öffnungskonturen ausgeformt. Zusätzlich zu den Öffnungsgeometrien 23 werden in Station B die Strömungsöffnungen 50 sowie Hilfsöffnungen 54 und 55 eingebracht .Film strips 35a have an opening geometry 23 in the form of a double H-shaped inlet opening 23a. At the same time, openings, such as passage openings 23b or spray openings 23c, are formed in the other film strips, each with different opening contours. In addition to the opening geometries 23, the flow openings 50 and auxiliary openings 54 and 55 are introduced in station B.
Zwischen jeweils zwei eingebrachten benachbartenBetween each two introduced neighboring ones
Öffnungsgeometrien 23 werden dabei in gleichen Abständen nahe der Folienränder 56 Hilfsöffnungen 54 als Zentrieröffnungen eingeformt, die entsprechend der Form der dort später eingreifenden Werkzeuge oder Hilfsmittel eckig oder kreisförmig sein können. Die Hilfsöffnungen 54 können auch als nutähnliche Zentrier- und Vorschubausnehmungen unmittelbar an den Folienrändern 56 vorgesehen sein. Andere Hilfsöffnungen 55 werden sichelförmig, die jeweiligen Öffnungsgeometrien 23 und in der oberen Blechlage 20a die Strömungsöffnungen 50 umgebend in den Folienstreifen 35 als Durchbrüche vorgesehen. Die z.B. vier sichelförmigen Hilfsöffnungen 55 schließen mit ihrer inneren Kontur einen Kreis mit einem Durchmesser ein, mit dem die Größe des Lochscheibenelements 16 festgelegt wird. Die von den Hilfsöffnungen 55 eingeschlossenen kreisförmigen Bereiche in den Folienstreifen 35 werden als Ronden 58 bezeichnet. An ihren Enden laufen die Hilfsöffnungen 55 spitz zu, wobei zwischen den einzelnen Hilfsöffnungen 55 schmale Stege 59 gebildet sind, die im Bereich des Rondendurchmessers eine Breite von nur 0,2 bis 0,3 mm besitzen. Beim Tiefziehen in Station E reißen die Stege 59, wodurch die Lochscheibenelemente 16 freigelegt werden. In besonders effektiver Weise können auch mehrere Folienstreifen 35 zu einem größeren Folienteppich zusammengefaßt sein, auf dem Ronden 58 in zwei Dimensionen angeordnet sind.Opening geometries 23 are formed at equal intervals near the film edges 56, auxiliary openings 54 as centering openings, which can be angular or circular, depending on the shape of the tools or aids that will later intervene there. The auxiliary openings 54 can also be provided as groove-like centering and feed recesses directly on the film edges 56. Other Auxiliary openings 55 are crescent-shaped, the respective opening geometries 23 and, in the upper sheet metal layer 20a, the flow openings 50 surrounding the film strips 35 are provided as openings. For example, the four crescent-shaped auxiliary openings 55 enclose with their inner contour a circle with a diameter with which the size of the perforated disk element 16 is determined. The circular areas enclosed by the auxiliary openings 55 in the film strips 35 are referred to as round plates 58. The auxiliary openings 55 taper to a point at their ends, narrow webs 59 being formed between the individual auxiliary openings 55 and having a width of only 0.2 to 0.3 mm in the region of the round diameter. During deep drawing in station E, the webs 59 tear, as a result of which the perforated disk elements 16 are exposed. In a particularly effective manner, a plurality of film strips 35 can also be combined to form a larger film carpet, on which the round plates 58 are arranged in two dimensions.
Während in die Folienstreifen 35b, 35c, die die später vomWhile in the film strips 35b, 35c, which the later from
Ventilschließkörper 7 abgewandten Blechlagen 20b, 20c im inneren Topf umfassen, nur die zentralen Öffnungsgeometrien 23b, 23c sowie die Hilfsöffnungen 54, 55 eingeformt werden, erfolgt in die dem Ventilschließkörper 7 zugewandte obere Blechlage 20a zusätzlich ein Einbringen derSheet metal layers 20b, 20c facing away from valve closing body 7 in the inner pot, only the central opening geometries 23b, 23c and the auxiliary openings 54, 55 are formed, the upper sheet metal layer 20a facing valve closing body 7 is additionally inserted
Strömungsöffnungen 50. Die Strömungsöffnungen 50 sind beispielsweise tropfenförmig ausgeführt und umgeben ringförmig die innere Einlaßöffnung 23a. Dabei verlaufen die einzelnen Strömungsöffnungen 50 nicht exakt radial in Richtung des Rondenmittelpunkts, sondern weisen einen gewissen Verdrehungsgrad auf. So ist einem hindurchströmenden Medium auf sehr einfache Art und Weise eine Drallkomponente aufprägbar. Die Schräglage der Strömungsöffnungen 50 bestimmt den Drall der Strömung. Selbstverständlich können die Strömungsöffnungen 50 auch derart eingebracht werden, daß ein sie durchströmendes Medium radial und nicht drallbehaftet zum Sitzbereich 24 bzw. zum Bodenbereich 22 gelangt. Im fertig ausgeformten Lochscheibenelement 16 befinden sich die Strömungsöffnungen 50 im Führungsbereich 26, wie es sehr anschaulich die Figuren 4 und 5 verdeutlichen. Die zwischen den Strömungsöffnungen 50 verbleibenden Materialbereiche der oberen Blechlage 20a stellen nämlich schmale, stegartige Führungsflächen 60 zur Führung der Ventilnadel 5 bzw. des Ventilschließkörpers 7 dar. Aufgrund der im Lochscheibenelement 16 vorgesehenen Strömungsöffnungen 50 kann in vorteilhafter Weise auf ein Einbringen von eineFlow openings 50. The flow openings 50 are, for example, drop-shaped and surround the inner inlet opening 23a in a ring shape. The individual flow openings 50 do not run exactly radially in the direction of the center of the disk, but instead have a certain degree of rotation. So is a medium flowing through in a very simple way a swirl component can be impressed. The inclined position of the flow openings 50 determines the swirl of the flow. Of course, the flow openings 50 can also be introduced in such a way that a medium flowing through them reaches the seat area 24 or the floor area 22 radially and without swirl. The flow openings 50 are located in the guide region 26 in the perforated disk element 16, as is clearly illustrated in FIGS. 4 and 5. The material areas of the upper sheet-metal layer 20a remaining between the flow openings 50 represent narrow, web-like guide surfaces 60 for guiding the valve needle 5 or the valve closing body 7. Due to the flow openings 50 provided in the perforated disk element 16, one can advantageously be introduced
Mediumströmung erlaubenden Abflachungen, Nuten oder Kanälen am Ventilschließkörper 7 vollständig verzichtet werden.Flattenings, grooves or channels which permit medium flow can be completely dispensed with on the valve closing body 7.
Figuren 4 und 5 zeigen ausschnittsweise zwei Beispiele von Lochscheibenelementen 16, wobei alle Bereiche 22, 24, 26, 28 und 30 wenigstens teilweise erkennbar sind. Zumindest die obere Blechlage 20a sollte aus einem härtbaren Werkstoff bestehen, um die Ventilsitzfläche 25 des Sitzbereichs 24 nach dem Tiefziehen zu härten. Dies kann z.B. ringförmig in einem umlaufenden Streifen 62 erfolgen, wie es in Figur 5 angedeutet ist. Es kann jedoch ebenso ein Härten über eine größere Fläche vorgenommen werden. Besonders geeignet sind Induktionshärten, Induktionsimpulshärten, Laserstrahlhärten und Elektronenstrahlhärten. Auf ein Härten kann ganz verzichtet werden, wenn die Kaltverfestigung durch das Umformen bereits ausreicht . Die Feinstbearbeitung der Ventilsitzfläche 25 des Sitzbereichs 24 wird beispielsweise so vorgenommen, daß der Ventilschließkörper 7 der Originalventilnadel 5 mit einer dünnen, leicht abrasiven, idealerweise lösbaren Schicht versehen wird, mit dem der Ventilsitz „eingeschliffen" wird. Danach wird die aufgebrachte Schicht (unter Druck) gelöst und herausgespült. Ideal sind kristalline Schichten aus Salz, Soda oder ähnlichem, die nach der Bearbeitung rückstandsfrei gelöst und herausgespült werden können. Eine Feinbearbeitung der Führungsflächen 60 des Führungsbereichs 26 erfolgt beispielsweise mittels Kalibrierprägen.FIGS. 4 and 5 show sections of two examples of perforated disk elements 16, all areas 22, 24, 26, 28 and 30 being at least partially recognizable. At least the upper sheet metal layer 20a should consist of a hardenable material in order to harden the valve seat surface 25 of the seat area 24 after the deep drawing. This can be done, for example, in a ring in a circumferential strip 62, as indicated in FIG. 5. However, hardening can also be carried out over a larger area. Induction hardening, induction pulse hardening, laser beam hardening and electron beam hardening are particularly suitable. There is no need for hardening if the strain hardening is already sufficient due to the forming. The fine machining of the valve seat surface 25 of the seat area 24 is, for example so that the valve closing body 7 of the original valve needle 5 is provided with a thin, slightly abrasive, ideally detachable layer with which the valve seat is “ground in.” The applied layer is then loosened (under pressure) and rinsed out. Crystalline layers are ideal Salt, soda or the like, which can be loosened and rinsed out after the processing without leaving any residues.
Durch das Tiefziehen oder Näpfen der Ronden 58 in der Station E werden der innere Topf und der äußere Halterand des Lochscheibenelements 16 in gewünschter Form gebildet. Werden die Rondendurchmesser in den einzelnen Folienstreifen 35 gleich groß gewählt, so entsteht durch das Tiefziehen der Blechlagen 20 der Haltebereich 28, der an seinem freien Ende abgestuft ist. Die innere Blechlage 20c des Haltebereichs 28, die aus dem unteren Folienstreifen 35c hervorgeht, endet in stromabwärtiger Richtung gesehen am weitesten entfernt vom Verbindungsbereich 30, während alle weiteren Blechlagen 20 von innen nach außen hin durch den Tiefziehprozeß jeweils kürzer enden (Figur 4) . Die Durchmesser der Ronden 58 können jedoch von vornherein auch unterschiedlich groß festgelegt werden, so daß nach dem Tiefziehen z.B. die äußerenThe inner pot and the outer holding edge of the perforated disk element 16 are formed in the desired shape by deep-drawing or cuping the rounds 58 in the station E. If the blank diameters in the individual film strips 35 are selected to be the same size, the deep-drawing of the sheet-metal layers 20 creates the holding area 28, which is stepped at its free end. The inner sheet metal layer 20c of the holding area 28, which emerges from the lower film strip 35c, ends furthest away from the connecting area 30 when viewed in the downstream direction, while all further sheet metal layers 20 each end shorter from the inside to the outside due to the deep-drawing process (FIG. 4). The diameters of the round blanks 58 can, however, also be set in different sizes from the outset, so that after deep drawing e.g. the outer
Blechlagen 20 des Haltebereichs 28 am freien Ende in einer Ebene enden und die innere Blechlage 20c des Haltebereichs 28 weiter stromabwärts auf ört. Das überstehende Ende 63 der Blechlage 20c kann z.B. durch Biegen oder Bördeln unter die anderen Blechlagenenden umgelegt werden (Figur 5) , wodurch eine einfachere Befestigung z.B. am Ventilsitzträger 1 mittels der Schweißnaht 32 erreichbar ist. In den Figuren 6 bis 8 ist das Tiefziehwerkzeug 40 vereinfacht schematisch dargestellt, das vom Band 39 durchlaufen wird. Das Band 39 liegt mit den Randbereichen außerhalb der Hilfsöffnungen 55 nahe den Folienrändern 56 z.B. auf einer Werkstückauflage 65 auf, gegen die es mittels eines Niederhalters 66 gedrückt wird. Die Werkstückaufläge 65 gehört zu einer Matrize 67 als Teil des Tiefziehwerkzeugs 40. Die Matrize 67 weist eine zumindest teilweise kegelstumpfförmige bzw. geschwungene Öffnung 68 auf, die die eigentliche Matrizenfunktion zur Umformung der Ronden 58 in Lochscheibenelemente 16 übernimmt. Im Niederhalter 66 ist ebenfalls eine Öffnung 69 vorgesehen, die durch die innere Wandung eines hülsenförmigen Schneidwerkzeugs 70 vorgegeben ist. In der weitgehend zylindrisch ausgebildeten Öffnung 69 ist ein Stempel 71 senkrecht zur Ebene des Bandes 39 bewegbar angeordnet, der von dem ebenfalls bewegbaren Schneidwerkzeug 70 umgeben ist. Auf der dem Stempel 71 gegenüberliegenden Seite des Bandes 39 ist in der teilweise geschwungenen, aber auch teilweise zylindrischen Öffnung 68 der Matrize 67 ein Stempelgegenstück 72 vorgesehen, das der Bewegung des Stempels 71 folgt, wobei der zylindrische Abschnitt der Öffnung 68 der Führung des Stempelgegenstücks 72 dient .Sheet metal layers 20 of the holding area 28 end in one plane at the free end and the inner sheet metal layer 20c of the holding area 28 further downstream on local. The protruding end 63 of the sheet metal layer 20c can be folded over, for example by bending or flanging, under the other sheet metal layer ends (FIG. 5), as a result of which a simpler attachment, for example to the valve seat support 1, can be achieved by means of the weld seam 32. The deep-drawing tool 40, which is traversed by the belt 39, is shown schematically in FIGS. 6 to 8. The band 39 rests with the edge areas outside the auxiliary openings 55 near the film edges 56, for example on a workpiece support 65, against which it is pressed by means of a hold-down device 66. The workpiece supports 65 belong to a die 67 as part of the deep-drawing tool 40. The die 67 has an at least partially frustoconical or curved opening 68, which takes over the actual die function for shaping the round plates 58 into perforated disk elements 16. An opening 69 is also provided in the hold-down device 66, which opening is predetermined by the inner wall of a sleeve-shaped cutting tool 70. In the largely cylindrical opening 69, a punch 71 is arranged to be movable perpendicular to the plane of the band 39 and is surrounded by the cutting tool 70, which is also movable. On the side of the band 39 opposite the stamp 71, a stamp counterpart 72 is provided in the partially curved but also partially cylindrical opening 68 of the die 67, which follows the movement of the stamp 71, the cylindrical portion of the opening 68 guiding the stamp counterpart 72 serves.
Zusammen mit dem Stempel 71 bewegt sich das Schneidwerkzeug 70 senkrecht zur Ebene des Bandes 39, so wie es die Pfeile in Figur 7 andeuten. Durch die genau zentrierte und definierte Bewegung von Stempel 71 und Schneidwerkzeug 70 gegen das Stempelgegenstück 72 in der Öffnung 68 der Matrize 67 bei einer hohen Flächenpressung mit einer Kraft, die größer ist als die Gegenkraft des Stempelgegenstücks 72, wird die Ronde 58 sehr exakt aus dem Band 39 durch eine Schneide des Schneidwerkzeugs 70 ausgeschnitten. An einem Absatz 73 der Öffnung 68 in der Matrize 67 kommt das Schneidwerkzeug 70 zum Stillstand, wobei es zugleich für eine Fixierung der Ronde 58 beim nachfolgendenTogether with the punch 71, the cutting tool 70 moves perpendicular to the plane of the band 39, as indicated by the arrows in FIG. 7. Due to the precisely centered and defined movement of the punch 71 and the cutting tool 70 against the punch counterpart 72 in the opening 68 of the die 67 at a high surface pressure with a force which is greater than the counterforce of the punch counterpart 72, the blank 58 is cut out very precisely from the band 39 by a cutting edge of the cutting tool 70. The cutting tool 70 comes to a standstill on a shoulder 73 of the opening 68 in the die 67, and at the same time it fixes the round plate 58 in the subsequent step
Tiefziehvorgang sorgt. Im weiteren Verlauf (Figur 8) wird nur noch der Stempel 71 in die Öffnung 68 hinein bewegt, so daß die Ronde 58 in eine erste topfförmige Gestalt gebracht wird, die bereits das topfförmige Lochscheibenelement 16 sein kann. Zur vollständigen Ausbildung aller Bereiche 22,Thermoforming process. In the further course (FIG. 8), only the stamp 71 is moved into the opening 68, so that the round plate 58 is brought into a first cup-shaped configuration, which can already be the cup-shaped perforated disk element 16. For the complete training of all areas 22,
24, 26, 28 und 30 des Lochscheibenelements 16 wird es jedoch oftmals erforderlich sein, mehrere Umformungsvorgänge in verschiedenen Werkzeugen, die ähnlich dem in den Figuren 6 bis 8 dargestellten Werkzeug 40 gestaltet sind, durchzuführen. Bei diesen in Station E ablaufenden Verfahren handelt es sich neben dem Ausschneiden um translatorisches Zugdruckumformen wie Tiefziehen oder Näpfen. Außerdem können zusätzlich Biegeverfahren zur Anwendung kommen.24, 26, 28 and 30 of the perforated disk element 16, however, it will often be necessary to carry out several forming operations in different tools, which are designed similarly to the tool 40 shown in FIGS. 6 to 8. In addition to cutting, these processes that take place in station E involve translational draft pressure forming such as deep drawing or cups. Bending processes can also be used.
Von der Ronde 58 abgerissen verbleibt ein Blechrand 75 als Abfall im Tiefziehwerkzeug 40, der jedoch recycelt und bei der Herstellung neuer Blechfolien verwendet werden kann. Auf ein festes Verbinden der Folienstreifen 35 in Station D kann vollständig verzichtet werden, wenn durch das Tiefziehen oder Näpfen in Station E der Haltebereich 28 desA sheet edge 75 remains torn from the round blank 58 as waste in the deep-drawing tool 40, which, however, can be recycled and used in the production of new sheet metal foils. A firm connection of the film strips 35 in station D can be completely dispensed with if the holding area 28 of the
Lochscheibenelements 16 in stark umgebogener Form, z.B. fast senkrecht zum Bodenbereich 22 (wie in Figur 1 gezeigt) erzeugt wird, wodurch nämlich in den Biegebereichen ausreichend feste Verbindungen geschaffen werden.Perforated disk element 16 in a strongly bent shape, e.g. is generated almost perpendicular to the bottom region 22 (as shown in FIG. 1), as a result of which sufficiently strong connections are created in the bending regions.
In Figur 9 ist ein Ausführungsbeispiel einer zeitlichen Abfolge bei der Umformung einer Ronde 58 in ein Lochscheibenelement 16 dargestellt. Zu erkennen ist, daß mehrere Tiefzieh- oder Biegevorgänge nötig sind, um eine gewünschte Gestalt des Lochscheibenelements 16 mit den Bereichen 22, 24, 26, 28 und 30 zu erhalten. Die Umformungen der Ronde 58 können auch in einer anderen Reihenfolge als der in Figur 9 gezeigten vorgenommen werden.FIG. 9 shows an exemplary embodiment of a chronological sequence when a round blank 58 is formed into a Perforated disk element 16 shown. It can be seen that several deep-drawing or bending processes are necessary in order to obtain a desired shape of the perforated disk element 16 with the areas 22, 24, 26, 28 and 30. The round blank 58 can also be shaped in a different order than that shown in FIG.
Wie den Figuren 4 und 5 zu entnehmen ist, ist es von Vorteil, die Abspritzöffnungen 23c mit einem Versatz zur Einlaßöffnung 23a auszuformen, so daß die Einlaßöffnung 23a in der Projektion an keiner Stelle die Abspritzöffnungen 23c überdeckt. Der Versatz kann dabei in verschiedene Richtungen unterschiedlich groß sein. Die Durchlaßöffnung 23b ist als die Einlaßöffnung 23a mit den Abspritzöffnungen 23c verbindender Kanal (cavity) ausgebildet. Diese Ausbildung der Öffnungsgeometrie 23 im Bodenbereich 22 des Lochscheibenelements 16 führt zu einem sogenannten S-Schlag in der Strömung des Mediums, speziell des Brennstoffs.As can be seen from FIGS. 4 and 5, it is advantageous to form the spray openings 23c with an offset to the inlet opening 23a, so that the inlet opening 23a does not cover the spray openings 23c at any point in the projection. The offset can be different in different directions. The passage opening 23b is designed as a channel (cavity) connecting the inlet opening 23a with the spray openings 23c. This formation of the opening geometry 23 in the bottom area 22 of the perforated disk element 16 leads to a so-called S-blow in the flow of the medium, especially the fuel.
Durch den S-Schlag innerhalb des Lochscheibenelements 16 mit mehreren starken Stromungsumlenkungen wird der Strömung eine starke, zerstäubungsfordernde Turbulenz aufgeprägt. Der Geschwindigkeitsgradient quer zur Strömung ist dadurch besonders stark ausgeprägt. Er ist ein Ausdruck für die Änderung der Geschwindigkeit quer zur Strömung, wobei die Geschwindigkeit in der Mitte der Strömung deutlich größer ist als in der Nähe der Wandungen. Die aus den Geschwindigkeitsunterschieden resultierenden erhöhten Scherspannungen im Fluid begünstigen den Zerfall in feine Tröpfchen nahe der Abspritzöffnungen 23c. Da die Strömung im Auslaß aufgrund der aufgeprägten Radialkomponente einseitig abgelöst ist, erfährt sie wegen fehlender Konturführung keine Strömungsberuhigung. Eine besonders hohe Geschwindigkeit weist das Fluid an der abgelösten Seite auf. Die zerstäubungsfordernden Turbulenzen und Scherspannungen werden somit im Austritt nicht vernichtet.The S impact within the perforated disk element 16 with several strong flow deflections imparts a strong, atomization-demanding turbulence to the flow. The velocity gradient across the flow is therefore particularly pronounced. It is an expression of the change in speed across the flow, with the speed in the middle of the flow being significantly greater than near the walls. The increased shear stresses in the fluid resulting from the speed differences promote the disintegration into fine droplets near the spray openings 23c. Since the flow in the outlet is detached on one side due to the impressed radial component, it experiences this due to the lack of contour guidance no flow calming. The fluid has a particularly high speed on the detached side. The turbulence and shear stresses required for atomization are therefore not destroyed in the outlet.
Die durch die Turbulenz vorhandenen Querimpulse quer zur Strömung führen unter anderem dazu, daß dieThe transverse impulses across the flow caused by the turbulence lead, among other things, to the
Tröpfchenverteilungsdichte im abgespritzten Spray eine große Gleichmäßigkeit aufweist. Daraus resultiert eine herabgesetzte Wahrscheinlichkeit von Tropfchenkoagulationen, also von Vereinigungen kleiner Tröpfchen zu größeren Tropfen. Die Folge der vorteilhaften Reduzierung des mittleren Tropfchendurchmessers im Spray ist eine relativ homogene Sprayverteilung. Durch den S-Schlag wird in dem Fluid eine feinskalige (hochfrequente) Turbulenz erzeugt, welche den Strahl unmittelbar nach Austritt aus dem Lochscheibenelement 16 in entsprechend feine Tröpfchen zerfallen läßt.Droplet distribution density in the sprayed spray has great uniformity. This results in a reduced likelihood of droplet coagulation, that is, of associations of small droplets into larger drops. The result of the advantageous reduction in the average droplet diameter in the spray is a relatively homogeneous spray distribution. The S blow creates a fine-scale (high-frequency) turbulence in the fluid, which causes the jet to disintegrate into correspondingly fine droplets immediately after emerging from the perforated disk element 16.
In den Figuren 10 und 11 sind zwei Beispiele von einfachen, zweilagigen erfindungsgemäßen Lochscheibenelementen 16 dargestellt, bei denen die gegenüber dem in Figur 1 dargestellten Ausführungsbeispiel gleichbleibenden bzw. gleichwirkenden Teile durch die gleichen Bezugszeichen gekennzeichnet sind. Das Lochscheibenelement 16 in Figur 10 weist zwei Blechlagen 20a und 20c auf, die ausgehend von der Ronde 58 derart umgeformt wurden, daß der mittlere Bodenbereich 22 mit der Öffnungsgeometrie 23, der Sitzbereich 24 mit der Ventilsitzflache 25 sowie der Führungsbereich 26 mit den Strömungsöffnungen 50 vorgesehen sind. Diese drei Bereiche 22, 24 und 26 bilden wiederum zusammen einen Topf. Der Führungsbereich 26 dient jedoch zugleich auch als Haltebereich 28; ein Verbindungsbereich 30 ist gar nicht vorgesehen. Der Führungsbereich 26 liegt somit bereits mit seiner dem Ventilschließkörper 7 abgewandten Blechlage 20c an der Wandung des Ventilsitzträgers 1 in der Längsöffnung 3 an. Eine feste Verbindung vonFIGS. 10 and 11 show two examples of simple, two-layer perforated disk elements 16 according to the invention, in which the parts which are the same or have the same effect as the embodiment shown in FIG. 1 are identified by the same reference numerals. The perforated disc element 16 in FIG. 10 has two sheet-metal layers 20a and 20c, which, starting from the circular blank 58, were shaped in such a way that the central base region 22 with the opening geometry 23, the seat region 24 with the valve seat surface 25 and the guide region 26 with the flow openings 50 are provided are. These three areas 22, 24 and 26 in turn form a pot. However, the guide area 26 serves at the same time as a holding area 28; a connection area 30 is not provided at all. The guide region 26 is therefore already in contact with the wall of the valve seat carrier 1 in the longitudinal opening 3 with its sheet metal layer 20c facing away from the valve closing body 7. A firm connection of
Lochscheibenelement 16 und Ventilsitzträger 1 wird durch die Schweißnaht 32 erreicht, die beispielsweise im abgewinkelten Übergang von Führungsbereich 26 und Sitzbereich 24 am Ventilsitzträger 1 angebracht wird. Die Einlaßöffnungen 23a der Blechlage 20a weisen einen teilweisen Versatz zu den Abspritzöffnungen 23c der Blechlage 20c auf.Perforated disk element 16 and valve seat carrier 1 is achieved by the weld seam 32, which is attached to the valve seat carrier 1, for example, in the angled transition from the guide region 26 and the seat region 24. The inlet openings 23a of the sheet metal layer 20a have a partial offset to the spray openings 23c of the sheet metal layer 20c.
Im Unterschied zum Lochscheibenelement 16 in Figur 10 besitzt das Ausführungsbeispiel gemäß Figur 11 einen anders ausgebildeten Sitzbereich 24. Der Sitzbereich 24 ist aus seiner kegelstumpfförmigen Kontur heraus mit einer Wulst 77 versehen, die zum Ventilschließkörper 7 hin gerichtet ist und die an der dem Ventilschließkörper 7 zugewandten Blechlage 20a die ringförmig umlaufende Ventilsitzfläche 25 aufweist. In vorteilhafter Weise dient die Wulst 77 auch der Versteifung des Lochscheibenelements 16. Durch das Einbringen der Wulst 77 wird zudem das Anbringen der Schweißnaht 32 vereinfacht, da im Verbindungsbereich der Werkzeugzugang erleichtert ist . In contrast to the perforated disk element 16 in FIG. 10, the exemplary embodiment according to FIG. 11 has a differently designed seating area 24. The seating area 24 is provided with a bulge 77 from its frustoconical contour, which is directed towards the valve closing body 7 and which faces the valve closing body 7 Sheet metal layer 20a has the annular valve seat surface 25. In an advantageous manner, the bead 77 also serves to stiffen the perforated disk element 16. The introduction of the bead 77 also simplifies the attachment of the weld seam 32, since tool access is facilitated in the connection area.

Claims

Patentansprüche claims
1. Ventil, insbesondere Brennstoffeinspritzventil für Brennstoffeinspritzanlagen von Brennkraftmaschinen, mit einer Ventillängsachse, mit einem festen Ventilsitz, mit einem mit dem Ventilsitz zusammenwirkenden1. Valve, in particular fuel injection valve for fuel injection systems of internal combustion engines, with a valve longitudinal axis, with a fixed valve seat, with one interacting with the valve seat
Ventilschließkörper, der entlang der Ventillängsachse axial bewegbar ist, mit einer Lochscheibe, die wenigstens eine Abspritzöffnung aufweist, dadurch gekennzeichnet, daß die Lochscheibe als Lochscheibenelement (16) mit wenigstens zwei metallenen, sandwichartig aneinander liegenden Blechlagen (20) ausgeführt ist und das Lochscheibenelement (16) in einem Sitzbereich (24) derart ausgeformt ist, daß es den Ventilsitz (25) aufweist.Valve closing body, which is axially movable along the longitudinal axis of the valve, with a perforated disk which has at least one spray opening, characterized in that the perforated disk is designed as a perforated disk element (16) with at least two metal, sheet-metal layers (20) sandwiching one another and the perforated disk element (16 ) is shaped in a seating area (24) in such a way that it has the valve seat (25).
2. Ventil nach Anspruch 1, dadurch gekennzeichnet, daß das Lochscheibenelement (16) einen mittleren Bodenbereich (22) mit einer Öffnungsgeometrie (23) für den vollständigen Durchgang eines abzuspritzenden Mediums aufweist, an den sich radial nach außen hin der Sitzbereich (24) als umlaufender Ringbereich anschließt. 2. Valve according to claim 1, characterized in that the perforated disc element (16) has a central bottom region (22) with an opening geometry (23) for the complete passage of a medium to be sprayed, to which the seat region (24) extends radially outwards circumferential ring area connects.
3. Ventil nach Anspruch 2, dadurch gekennzeichnet, daß der Sitzbereich (24) in stromabwärtiger Richtung kegelstumpfförmig verjüngend bis hin zum Bodenbereich (22) verläuft.3. Valve according to claim 2, characterized in that the seat area (24) tapers in a truncated cone in the downstream direction to the bottom area (22).
4. Ventil nach Anspruch 2 oder 3, dadurch gekennzeichnet, daß zusätzlich zum Bodenbereich (22) und zum Sitzbereich4. Valve according to claim 2 or 3, characterized in that in addition to the floor area (22) and the seating area
(24) ein Führungsbereich (26) zur Führung des axial bewegbaren Ventilschließkörpers (7) am Lochscheibenelement (16) vorgesehen ist.(24) a guide area (26) for guiding the axially movable valve closing body (7) on the perforated disk element (16) is provided.
5. Ventil nach Anspruch 4, dadurch gekennzeichnet, daß der Bodenbereich (22) , der Sitzbereich (24) und der Führungsbereich (26) derart ausgeformt sind, daß sie zusammen einen inneren Topf des Lochscheibenelements (16) bilden.5. Valve according to claim 4, characterized in that the bottom region (22), the seat region (24) and the guide region (26) are shaped such that together they form an inner pot of the perforated disc element (16).
6. Ventil nach Anspruch 4, dadurch gekennzeichnet, daß der Führungsbereich (26) ringförmig umlaufend und achsparallel verläuft.6. Valve according to claim 4, characterized in that the guide region (26) extends annularly and axially parallel.
7. Ventil nach einem der Ansprüche 4 bis 6, dadurch gekennzeichnet, daß der Führungsbereich (26) zugleich als Haltebereich (28) ausgeführt ist, der der Befestigung des Lochscheibenelements (16) im Ventil dient.7. Valve according to one of claims 4 to 6, characterized in that the guide area (26) is also designed as a holding area (28) which serves to fasten the perforated disc element (16) in the valve.
8. Ventil nach Anspruch 5, dadurch gekennzeichnet, daß zusätzlich zum inneren Topf (22, 24, 26) ein Haltebereich (28) vorgesehen ist, der den äußeren radialen Abschluß des Lochscheibenelements (16) bildet und über einen8. Valve according to claim 5, characterized in that in addition to the inner pot (22, 24, 26) a holding area (28) is provided which forms the outer radial closure of the perforated disc element (16) and via a
Verbindungsbereich (30) mit dem Führungsbereich (26) verbunden ist. Connection area (30) is connected to the guide area (26).
9. Ventil nach einem der Ansprüche 4 bis 8, dadurch gekennzeichnet, daß in der dem Ventilschließkörper (7) zugewandten Blechlage (20a) im Führungsbereich (26) wenigstens zwei Strömungsöffnungen (50) ausgebildet sind.9. Valve according to one of claims 4 to 8, characterized in that in the valve closing body (7) facing sheet metal layer (20a) in the guide region (26) at least two flow openings (50) are formed.
10. Ventil nach Anspruch 9, dadurch gekennzeichnet, daß die Strömungsöffnungen (50) geneigt zur Ventillängsachse (2) ausgeformt sind, so daß einem durch sie hindurchströmenden Medium eine Drallkomponente aufprägbar ist.10. Valve according to claim 9, characterized in that the flow openings (50) inclined to the valve longitudinal axis (2) are formed so that a swirl component can be impressed on a medium flowing through them.
11. Ventil nach Anspruch 9 oder 10, dadurch gekennzeichnet, daß die zwischen den Strömungsöffnungen (50) verbleibenden Materialbereiche der inneren Blechlage (20a) stegartige Führungsflächen (60) zur Führung des axial bewegbaren Ventilschließkörpers (7) am Lochscheibenelement (16) darstellen.11. Valve according to claim 9 or 10, characterized in that between the flow openings (50) remaining material areas of the inner sheet metal layer (20a) web-like guide surfaces (60) for guiding the axially movable valve closing body (7) on the perforated disc element (16).
12. Ventil nach Anspruch 2, dadurch gekennzeichnet, daß die Öffnungsgeometrie (23) im Bodenbereich (22) des12. Valve according to claim 2, characterized in that the opening geometry (23) in the bottom region (22) of the
Lochscheibenelements (16) derart vorgesehen ist, daß die Abspritzöffnungen (23c) in der dem Ventilschließkörper (7) abgewandtesten Blechlage (20c) wenigstens einen teilweisen Versatz zu einer Einlaßöffnung (23a) in der dem Ventilschließkörper (7) zugewandtesten Blechlage (20a) besitzen.Perforated disk element (16) is provided such that the spray openings (23c) in the sheet metal layer (20c) facing away from the valve closing body (7) have at least a partial offset to an inlet opening (23a) in the sheet metal layer (20a) facing the valve closing body (7).
13. Verfahren zur Herstellung eines Ventilsitzes für ein Ventil, insbesondere für ein Ventil nach einem der Ansprüche 1 bis 12, mit den Verfahrensschritten a) Bereitstellen von wenigstens zwei dünnen metallenen Blechfolien (35) in Form von Folienstreifen oder Folienteppichen, b) Einbringen von gleichen Öffnungsgeometrien (23) und Hilfsöffnungen (54, 55) pro Blechfolie (35) in großer13. A method for producing a valve seat for a valve, in particular for a valve according to one of claims 1 to 12, with the method steps a) providing at least two thin metal sheet foils (35) in the form of foil strips or foil carpets, b) introducing the same opening geometries (23) and auxiliary openings (54, 55) per sheet foil (35) in large
Anzahl, c) Aufeinanderbringen der einzelnen Blechfolien (35) zum Herstellen eines Bandes (39) mit einer Vielzahl von RondenNumber, c) bringing together the individual sheet foils (35) to produce a strip (39) with a large number of round blanks
(58) , d) Vereinzeln der Ronden (58) und Umformen der Ronden (58) in Lochscheibenelemente (16) , die wenigstens einen Bodenbereich (22) mit der Öffnungsgeometrie (23) und einen Sitzbereich (24) mit dem Ventilsitz (25) aufweisen.(58), d) separating the round plates (58) and shaping the round plates (58) into perforated disk elements (16), which have at least one base region (22) with the opening geometry (23) and one seat region (24) with the valve seat (25) exhibit.
14. Verfahren zur Herstellung eines Ventilsitzes für ein14. A method of manufacturing a valve seat for a
Ventil, insbesondere für ein Ventil nach einem der Ansprüche 1 bis 12, mit den Verfahrensschritten a) Bereitstellen von wenigstens zwei dünnen metallenen Blechfolien (35) in Form von Folienstreifen oder Folienteppichen, b) Einbringen von gleichen Öffnungsgeometrien (23) und Hilfsöffnungen (54, 55) pro Blechfolie (35) in großer Anzahl, c) Aufeinanderbringen der einzelnen Blechfolien (35) , d) Verbinden der Blechfolien (35) durch Anwendung einesValve, in particular for a valve according to one of claims 1 to 12, with the method steps a) providing at least two thin metal sheet foils (35) in the form of foil strips or foil carpets, b) introducing the same opening geometries (23) and auxiliary openings (54, 55) per sheet metal foil (35) in large numbers, c) bringing the individual sheet metal foils (35) together, d) connecting the sheet metal foils (35) by using a
Fügeverfahrens , wobei ein Band (39) mit einer Vielzahl von Ronden (58) vorliegt, e) Vereinzeln der Ronden (58) und Umformen der Ronden (58) in Lochscheibenelemente (16) , die wenigstens einen Bodenbereich (22) mit der Öffnungsgeometrie (23) und einen Sitzbereich (24) mit dem Ventilsitz (25) aufweisen. Joining method, a band (39) having a plurality of round plates (58) is present, e) separating the round plates (58) and shaping the round plates (58) into perforated disc elements (16) which have at least one base region (22) with the opening geometry ( 23) and a seating area (24) with the valve seat (25).
15. Verfahren nach Anspruch 13 oder 14, dadurch gekennzeichnet, daß zusätzlich zu den Öffnungsgeometrien15. The method according to claim 13 or 14, characterized in that in addition to the opening geometries
(23) und den Hilfsöffnungen (54, 55) in einer Blechfolie (35) Strömungsöffnungen (50) eingebracht werden.(23) and the auxiliary openings (54, 55) in a sheet metal foil (35) flow openings (50) are introduced.
16. Verfahren nach Anspruch 15, dadurch gekennzeichnet, daß das Einbringen der Öffnungsgeometrien (23) , der Hilfsöffnungen (54, 55) sowie der Strömungsöffnungen (50) mittels Stanzen, Laserschneiden, Erodieren oder Ätzen erfolgt.16. The method according to claim 15, characterized in that the introduction of the opening geometries (23), the auxiliary openings (54, 55) and the flow openings (50) by means of punching, laser cutting, eroding or etching.
17. Verfahren nach Anspruch 14, dadurch gekennzeichnet, daß das Verbinden der Blechfolien (35) mittels Schweißen, Löten oder Kleben vorgenommen wird.17. The method according to claim 14, characterized in that the connection of the sheet metal foils (35) is carried out by means of welding, soldering or gluing.
18. Verfahren nach Anspruch 13 oder 14, dadurch gekennzeichnet, daß das Umformen der Ronden (58) mittels Tiefziehen oder Näpfen mit Hilfe eines Tiefziehwerkzeugs18. The method according to claim 13 or 14, characterized in that the shaping of the blanks (58) by means of deep drawing or cups with the aid of a deep drawing tool
(40) erfolgt.(40) takes place.
19. Verfahren nach Anspruch 18, dadurch gekennzeichnet, daß das Vereinzeln der Ronden (58) durch ein Schneidwerkzeug19. The method according to claim 18, characterized in that the separation of the blanks (58) by a cutting tool
(70) im Tiefziehwerkzeug (40) vor dem Umformen erfolgt.(70) in the deep-drawing tool (40) before forming.
20. Verfahren nach einem der Ansprüche 13 bis 19, dadurch gekennzeichnet, daß nach dem Umformen ein Härten des Ventilsitzes (25) im Sitzbereich (24) erfolgt. 20. The method according to any one of claims 13 to 19, characterized in that after the shaping, the valve seat (25) is hardened in the seat region (24).
EP98931957A 1997-06-25 1998-04-21 Valve and method for producing a valve seat for a valve Expired - Lifetime EP0920359B1 (en)

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DE19726991A DE19726991A1 (en) 1997-06-25 1997-06-25 Valve and method for manufacturing a valve seat for a valve
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PCT/DE1998/001103 WO1999000201A1 (en) 1997-06-25 1998-04-21 Valve and method for producing a valve seat for a valve

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AU8206398A (en) 1999-01-19
DE59803184D1 (en) 2002-04-04
EP0920359B1 (en) 2002-02-27

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