Source: https://patents.google.com/patent/US6434826
Timestamp: 2018-04-25 09:03:44
Document Index: 223438789

Matched Legal Cases: ['Application No. 43', 'application No. 44', 'art 32', 'art 35', 'art 32', 'art 35', 'art 32', 'art 35', 'art 35', 'art 51', 'art 52', 'arts 51']

US6434826B1 - Method for producing a nozzle plate - Google Patents
Method for producing a nozzle plate Download PDF
US6434826B1
US6434826B1 US09145005 US14500598A US6434826B1 US 6434826 B1 US6434826 B1 US 6434826B1 US 09145005 US09145005 US 09145005 US 14500598 A US14500598 A US 14500598A US 6434826 B1 US6434826 B1 US 6434826B1
US09145005
A nozzle plate, particularly for fuel injection valves, with at least one flow path which has at least one supply opening, which path includes a ring gap which opens into a ring-shaped exit opening, as well as a method for the production of such a nozzle plate. For the nozzle plate, it is provided that the flow path has a ring channel assigned to the supply opening, which channel makes a transition into a cylinder-shaped ring gap with a cross-section which narrows in the region of the exit opening. The production of the nozzle plate takes place in that a cavity mold corresponding to the flow path through the nozzle plate is produced, that a layer embedding the cavity mold is galvanically deposited, and that the cavity mold is removed from the galvanically deposited layer.
This application is a divisional application of prior application Ser. No. 08/809,556, filed Mar. 6, 1997, which is the U.S. national phase of International Application No. PCT/DE96/00980, filed Jun. 4, 1996, now U.S. Pat. No. 5,857,628.
A known nozzle plate (German Patent Application No. 43 28 418) has a holder plate with a stepped through-bore, where the segment of this bore which lies towards the supply side, and has a smaller diameter, forms the supply opening. An injection plate is inserted into the bore segment with the larger diameter, which plate has a recess in its edge region assigned to the exit side, forming a ring channel together with a recess in the holder plate assigned to it, which channel is connected with the supply opening via slits provided in the side of the injection plate facing the supply opening. The exit-side edges of the recesses in the holder plate and the injection plate delimit a ring-shaped exit opening of the known nozzle plate.
German patent application No. 44 04 021.0 describes another nozzle plate, composed of two parts, in which a ring channel is provided between the two parts, which channel is connected with a fuel supply region via supply bores provided in the first part, and connected with a fuel exit region via a ring gap. The ring gap, in this connection, is delimited by two mantle surfaces in the shape of truncated cones, with the one being attached to the first part of the nozzle plate and the other to the second part.
The two parts of this nozzle plate are produced by galvanic second-casting of corresponding negative molds, consisting of conductive plastic, where the galvanically cast parts can be mechanically finished and subsequently attached to each other by means of gluing, diffusion soldering, or diffusion welding.
Such nozzle plates with ring gap nozzles are used in fuel injection valves for gasoline engines in order to achieve better atomization of the fuel. In this connection, the fuel is supposed to exit as a cohesive laminar jet in the shape of a conical mantle. Because of the radial expanse along the conical mantle, the fuel film becomes thinner with an increasing diameter towards the exit, until it bursts into very small droplets due to aerodynamic forces. In this manner, it is possible to achieve distribution of the fuel over a relatively large volume.
In order to obtain a uniform laminar jet, uniform pressure distribution and a uniform fuel supply are necessary at the ring gap.
The nozzle plate according to the present invention, has the advantage, in contrast, that it is possible to achieve a uniform, cohesive laminar jet in the shape of a conical mantle at the fuel discharge, by-means of the cylindrical formation of the ring channel, with a cross-section which narrows in the region of the exit opening, without an arrangement of the ring gap itself in the shape of a conical mantle being necessary. In this connection, the formation of the ring gap, according to the present invention, results in an improved flow behavior of the fuel in the nozzle plate itself, and in a more uniform formation of the laminar jet.
It is particularly advantageous if two exit openings arranged concentric to one another are provided, where each of the exit openings has its own flow path assigned to it, since this makes it possible to achieve two fuel jets in the shape of a conical mantle, which have a smaller conical angle and break down into smaller fuel droplets over a shorter path length.
With the exit opening, which is lens-shaped in a top view, it is possible to form the fuel jet which is sprayed out in such a way, in advantageous manner, that the fuel flow is divided into two partial flows. This makes it possible, for example, to supply both intake valves of a four-valve engine at the same time.
Another advantage of the present invention consists of the fact that because of the holder ridges arranged between the supply openings, the inner segment which delimits the flow path on the inside can be connected with the ring-shaped segment of the nozzle plate which delimits the flow path on the outside, in a stable manner, without the fuel flow being hampered by the nozzle plate.
In this connection, the supply openings and the holder ridges located between them can also be provided outside the diameter of the ring-shaped exit opening and therefore radially outside the ring gap, which makes it possible to enlarge the flow cross-section of the flow path through the nozzle plate on the supply side, in order to make the flow through the nozzle plate even more uniform.
The method for the production of a nozzle plate has the advantage, in this connection, that the nozzle plate can be made in one piece using this method, so that none of the joining processes which influence the formation of the ring gap, such as gluing, soldering or welding, have to be carried out on the nozzle plate.
In advantageous manner, it is possible to produce the width of the ring gap precisely, by second-casting of a single cavity mold, and it does not depend on the precision with which the connection between two parts is produced. In particular, tolerances in joining and welding together two parts are eliminated. Another advantage consists of the fact that the nozzle plate can be produced with two ring gaps which serve as exit openings, each with its own flow path, without significant additional effort.
A particular advantage of the method according to the present invention consists of the fact that the die for the production of the cavity mold can easily be produced by mechanical lathing work, e.g. with a diamond-tipped tool, with great precision. The slant of the inside wall of the ring gap, which is necessary for formation of the laminar jet to discharge the fuel, can be produced with great precision, by finishing a die part from the outside.
FIG. 1 shows a top view of an exit side of a first exemplary embodiment of a nozzle plate according to the present invention.
FIG. 2 shows a cross-section, essentially along the line II—II of FIG. 3, through the nozzle plate as illustrated in FIG. 1.
FIG. 3 shows a top view of a supply side of the nozzle plate illustrated in FIG. 1.
FIG. 4 shows a cross-section through an injection mold for a production of a cavity mold, which serves to produce the nozzle plate illustrated in FIGS. 1-3.
FIG. 5 shows a cross-section corresponding the cross-section of FIG. 4, where a top die of the injection mold has been removed and the cavity mold has been affixed on an auxiliary carrier.
FIG. 6 shows a cross-section through the cavity mold embedded in a galvanically deposited layer.
FIG. 7 shows a cross-section corresponding to the cross-section of FIG. 6, through the galvanically deposited layer, where the cavity mold has been removed.
FIG. 8 shows a cross-section through the nozzle plate corresponding to the cross-section of FIG. 2, with a connector element of a fluid supply and a flow measurement device set thereon.
FIG. 9 shows a cross-section through a cavity mold for the nozzle plate with two ring gaps attached to an auxiliary carrier.
FIG. 10 shows a cross-section similar to the cross-section of FIG. 8, through the nozzle plate produced with the cavity mold illustrated in FIG. 9.
FIG. 11 shows a schematic top view of a lens-shaped ring gap.
The nozzle plate 10 in FIGS. 1 to 3, produced according to the present invention, consists of a material which can be galvanically deposited, particularly of a metal or a metal alloy, preferably of nickel-phosphorus, and has a flat surface 11 on the supply side, shown at the top in FIG. 2, in which a plurality of supply openings 12 is provided, as shown in FIG. 3, which are separated from one another by means of holder ridges 13 located between them. The ring-shaped supply openings 12, which are arranged at a uniform distribution over the circumference, open into a ring channel 14, which makes a transition into a cylindrical ring gap 15 in the flow direction.
The ring gap 15 is delimited, on its outside circumference, by a cylindrical mantle surface 16, and, on its inside circumference, by a cylindrical mantle surface 17, which makes a transition into a conical mantle surface 18 in the region of a ring-shaped exit opening 19, so that the ring gap 15 narrows uniformly towards the exit opening 19.
The nozzle plate 10 therefore has a ring-shaped segment 20 which is located outside the ring gap 15, which is connected, in one piece, with an inner segment 21 located within the ring gap 15, via the holder ridges 13. On the exit side, the nozzle plate 10 has a ring surface 22 which lies parallel to the surface 11, and makes a transition into a truncated conical mantle surface 23, which extends at least to the exit opening 19. It is also possible, however, that the truncated conical mantle surface 23 on the ring-shaped segment 20 extends beyond the ring-shaped exit opening 19 of the ring gap 15, to the inner segment 21. Towards the center of the nozzle plate 10, the truncated conical mantle surface 23 is followed by another flat surface 24, which lies parallel to the supply-side surface 11, either directly or separated by the ring gap. The surface 24 can be a ring-shaped surface, as in the exemplary embodiment shown. It is also possible, however, to structure the flat surface 24 as a circular surface.
For the production of the nozzle plate 10 described, as shown in FIG. 4, first a cavity mold 30 is produced from plastic, for example a thermoplastically formable and releasable plastic, particularly PMMA (polymethyl methacrylate), preferably using the injection-molding process. In this connection, the cavity mold 30 corresponds to the flow path through the nozzle plate 10 to be produced, formed by the supply openings 12, the ring channel 14, and the ring gap 15.
The injection-molding process is carried out, in this connection, using an appropriate molding die 31, which comprises a top die part 32 with a top inner core 33, and a top outside ring 34, as well as a bottom die part 35 with a bottom inner core 36, a bottom outside ring 37, and a die plate 38. For the simultaneous formation of several cavity molds 30, the top die part 32 can have several inner cores 33, in a manner not shown in greater detail, with a corresponding outside ring arrangement. The bottom die part 35 is then structured in a corresponding manner.
The flow path planned for the nozzle plate 10 is formed between the bottom inner core 36 and the bottom outside ring 37, which are carried by the die plate 38. An injection-molding supply 39 is formed between the top inner core 33 and the top outside ring 34, which supply makes a transition, via a narrow area 40 which produces a predetermined breaking point, into a casting space for a support ring 41, which serves as the carrier element for the cavity mold 30 during further production of the nozzle plate 10. The carrier element may be made from an electrically non-conducting material.
Furthermore, continuations 42 corresponding to the holder ridges 13 of the nozzle plate 10 are provided on the top inner core 33, which continuations engage in a region between the bottom outside ring 37 and the bottom inner core, thereby establishing the regions for the supply openings 12. On the bottom inner core 36 of the mold die 31, the cylindrical mantle surface and the conical mantle surface which delimit the ring gap 15 towards the inside are formed as outside surfaces, which can therefore be formed with great precision.
After injection of the plastic into the cavity of the mold die 31 which reproduces the flow path of the nozzle plate 10, for production of the cavity mold 30 with the attached support ring 41, the top die part 32 is removed, together with the excess plastic material located in the injection supply 39.
Then, as shown in FIG. 5, a conductive plastic plate of PMMA, preferably reinforced with a metal grid, is attached, particularly welded on, as an auxiliary carrier, while the cavity mold 30 is still in the bottom die part 35. This makes it possible to avoid deformations of the cavity mold 30 during attachment of the plastic plate 43. Then the bottom die part 35 is also removed, so that the cavity mold 30 is exposed.
Subsequently, a layer 44, preferably consisting of nickel-phosphorus, is deposited on the conductive plastic plate 43, completely embedding the cavity mold 30. Defects which can occur as the layer grows in the region 45 of the ridges 13, when filling the edges in the transition region 46 between the ring channel 14 and the ring gap 15, as well as when the layer 44 grows together in the outside region 47 of the ridges 13, are insignificant in this connection, since the formation of the ring gap 15 on the exit side is not influenced by such defects.
After galvanic deposition of the layer 44, from which the nozzle plate 10 is later formed, the plastic plate 43 which serves as an auxiliary carrier during galvanization is removed, and the supply-side surface 11 of the nozzle plate 10 is produced by grinding.
Finally, as shown in FIG. 7, the cavity mold 30 is removed by removing the plastic, so that the flow path formed in the galvanically deposited layer 44, by the supply openings 12, the ring channel 14, and the ring gap 15, is exposed.
As shown in FIG. 8, finally the surface of the galvanically deposited layer 44 which corresponds to the exit side of the nozzle plate 10 to be formed, is finished by means of a material-removing process, in order to form the ring surface 22, the truncated conical mantle surface 23 which extends over the exit opening, and the flat surface 24 which is located on the inside segment 21 of the nozzle plate.
During finishing of the truncated conical mantle surface 23 which preferably extends over the exit opening 19, in order to adjust the exit opening 19 in such a way that the flow path through the nozzle plate 10 demonstrates the necessary flow resistance, a connector element 48 of a fluid supply and flow-through measurement device, not shown in greater detail, is set onto the supply-side surface 11 of the nozzle plate 10 to be formed, so that a fluid can be supplied to the supply side of the nozzle plate 10 at constant pressure. During finishing of the truncated conical mantle surface 23, the exit opening 19 is exposed and constantly enlarged, so that the flow through the nozzle plate 10, which is being finished, increases until it has reached the desired value. Now the exit opening 19 has the necessary size.
The finishing process, which involves material removal or cutting, preferably takes place with a tool tipped with natural diamond, which makes it possible to cleanly form the edges of the ring gap 15 which delimit the exit opening 19.
In order to obtain edges of the ring gap which are as free of burrs as possible, finishing of the exit side of the nozzle plate 10 can be carried out while the flow path is still filled with the cavity mold 30. In this case, the necessary size of the exit opening 19 is measured optically, for example.
The method described can be used for the production of an individual nozzle plate 10, but it is practical if several nozzle plates 10 are produced at the same time with this method, in such a way that several cavity molds 30 are simultaneously formed using the injection-molding method, and are affixed to a common auxiliary carrier. The layer from which the individual nozzle plates 10 are then produced is then deposited in a single galvanization step. It is practical if parting molds are provided between the cavity molds 30 for the flow path of the nozzle plates, so that when the surface of the galvanically deposited layer 44 which is assigned to the exit side of the nozzle plates 10 is being finished, the nozzle plates 10 to be formed from it can be separated in simple manner.
FIG. 9 shows a cavity mold 50 for a nozzle plate 10′ according to a different exemplary embodiment of the present invention, with an inner mold part 51, corresponding to a first flow path through the nozzle plate 10′, and an outer mold part 52, corresponding to a second flow path through the nozzle plate 10′. It is practical if the mold parts 51, 52 are arranged concentric to one another, i.e. if the corresponding flow paths are formed in accordance with the first exemplary embodiment of the invention described on the basis of FIGS. 1 to 8.
FIG. 10 illustrates finishing of the exit side of a nozzle plate 10′ produced with the cavity mold 50 according to FIG. 9, in which a connector element 48′ of a fluid supply and flow-through measurement device is set on, in order to determine the size of the exit opening 19 during finishing of the exit side of the nozzle plate 10′. It is practical if the connector element 48′ is designed in such a way, in this connection, that the flow through each of the two exit openings can be determined separately, as indicated by the arrows Q1 and Q2.
In order to create the largest possible supply region for each of the two flow paths through the nozzle plate 10′, and, on the other hand, to be able to arrange the ring gaps 15 with a relatively small diameter, close to one another, connector channels 49 in conical mantle shape are formed between the ring gaps 15 and the ring channels 14.
Here, the supply openings 12 in each instance, with the related holder ridges 13, lie radially outside the corresponding exit opening 19 and therefore also radially outside the corresponding ring channel 15. This arrangement of the supply openings 12 and ring channel 15, which is necessarily required for the nozzle plate 10′ according to FIG. 10, can also be provided for the nozzle plate 10 described on the basis of FIG. 1 to 3, in order to achieve the greatest possible supply-side flow cross-section, which makes a uniform distribution of the flow energy, without variations, possible.
Using the production method described, not only nozzle plates with circular exit openings, but also those that have lens-shaped exit openings 19′ can be produced, as shown in FIG. 11. In this connection, the lens-shaped exit opening 19′ is composed of two circular arc segments 61 with a large radius of curvature, and two circular arc segments 62 with a small radius of curvature, where the two segments 61 with a large radius of curvature lie opposite one other with their concave sides, and are connected with one another at their ends via the segments 62 with a small radius of curvature. The, circular arc segments 61 with a large radius of curvature lie symmetrical to an axis X, while the circular arc segments 62 with a small radius of curvature are arranged symmetrical to an axis Y.
The fuel flow which flows through the nozzle can be divided into two mass flows, separated from each other in the direction of the Y axis, by means of a ring gap nozzle with a lens-shaped exit opening arranged in accordance with FIG. 11, since the fuel jet given off in the direction of the X axis, via the corresponding segments of the exit opening, breaks up sooner than the one given off in the Y direction. Such a ring gap nozzle is practical, for example, if two inlet valves of a cylinder of a four-valve engine, in each instance, are to be supplied with fuel at the same time.
1. A method for producing a nozzle plate with at least one flow path which has at least one supply opening, the flow path having a ring gap which opens into a ring-shaped exit opening, the nozzle plate being for use with a fuel injection valve, the method comprising the steps of:
producing a cavity mold from a thermoplastically formable material using an injection-molding process, the cavity mold corresponding to the flow path through the nozzle plate;
galvanically depositing a layer which embeds the cavity mold, the nozzle plate being entirely formed as a single piece from the layer; and
removing the cavity mold from the galvanically deposited layer.
2. The method according to claim 1, wherein the cavity mold is produced from a releasable plastic material.
3. The method according to claim 2, wherein the releasable plastic material is a polymethyl methacrylate material.
4. The method according to claim 1, wherein the galvanically deposited layer includes nickel-phosphorus.
producing, together with the cavity mold, a carrier element the cavity mold and the carrier element both being made from an electrically non-conductive material, the carrier element being connected with the cavity mold;
producing an electrically conductive auxiliary carrier from an electrically conductive material; and
attaching the electrically conductive auxiliary carrier to the cavity mold via the carrier element.
6. The method according to claim 5, wherein the electrically conductive auxiliary carrier includes a plastic plate.
7. The method according to claim 6, wherein the plastic plate is reinforced with a metal grid.
8. The method according to claim 5, wherein the electrically conductive auxiliary carrier is attached on a side of the cavity mold which contains the at least one supply opening.
9. The method according to claim 8, wherein the step of attaching the electrically conductive auxiliary carrier occurs before the step of removing a side of the cavity mold which contains the ring-shaped exit opening for the flow path from a corresponding injection-molding die.
removing the electrically conductive auxiliary carrier from the galvanically deposited layer after the electrically conductive auxiliary carrier has been formed.
11. The method according to claim 10, wherein the electrically conductive auxiliary carrier is removed from the galvanically deposited layer by grinding.
grinding the galvanically deposited layer adjacent to the supply opening until the at least one-supply opening is exposed.
after a removal of the cavity mold from the galvanically deposited layer and using a material-removing process, finishing a remaining galvanically deposited layer which is adjacent to the ring-shaped exit opening on the cavity mold.
during the finishing step, providing a fluid, which is under a constant pressure, to the flow path from a supply side, the fluid flowing through the ring-shaped exit opening at a predetermined rate.
15. The method according to claim 13, wherein the finishing step is performed with a tool having a natural diamond tip and before the removal of the cavity mold from the galvanically deposited layer.
16. The method according to claim 1, wherein the nozzle plate has at least two exit openings parallel to one another with respect to the flow path, each of the at least two exit openings having a respective flow path, and wherein the cavity mold is produced with at least two mold parts.
17. The method according to claim 16, wherein the at least two mold parts are formed concentric to one another.
18. The method according to claim 1, wherein a plurality of nozzle plates are produced simultaneously, and wherein a plurality of cavity molds corresponding to the plurality of nozzle plates are produced simultaneously and arranged on a common auxiliary carrier.
19. The method according to claim 1, wherein in the flow path of the nozzle plate, the ring gap is delimited by a first cylindrical mantle surface on an outside circumference of the ring gap and is delimited by a second cylindrical mantle surface on an inside circumference of the ring gap, the second cylindrical mantle surface transitioning into a conical mantle surface in a region of the ring-shaped exit opening so that the ring gap narrows towards the ring-shaped exit opening.
20. The method according to claim 19, wherein the flow path includes a ring channel.
21. The method according to claim 19, wherein the flow path includes a plurality of supply openings.
22. The method according to claim 21, wherein each of the plurality of supply openings are separated by one holder ridge of a plurality of holder ridges.
23. The method according to claim 21, wherein the plurality of supply openings are arranged in a uniform distribution over a circumference of the plurality of supply openings.
24. The method according to claim 19, wherein the flow path includes a plurality of supply openings, each of the plurality of supply openings being separated by one holder ridge of a plurality of holder ridges, and the plurality of supply openings being arranged in a uniform distribution over a circumference of the plurality of supply openings.
in the flow path of the nozzle plate, the ring gap is delimited by a first cylindrical mantle surface on an outside circumference of the ring gap and is delimited by a second cylindrical mantle surface on an inside circumference of the ring gap, the second cylindrical mantle surface transitioning into a conical mantle surface in a region of the ring-shaped exit opening so that the ring gap narrows towards the ring-shaped exit opening; and
the flow path includes a ring channel.
26. The method according to claim 25, wherein the flow path includes a plurality of supply openings.
27. The method according to claim 26, wherein each of the plurality of supply openings are separated by one holder ridge of a plurality of holder ridges.
28. The method according to claim 26, wherein the plurality of supply openings are arranged in a uniform distribution over a circumference of the plurality of supply openings.
29. The method according to claim 25, wherein the flow path includes a plurality of supply openings, each of the plurality of supply openings being separated by one holder ridge of a plurality of holder ridges, and the plurality of supply openings being arranged in a uniform distribution over a circumference of the plurality of supply openings.
30. The method according to claim 1, wherein the ring gap narrows towards the ring-shaped exit opening.
31. The method according to claim 30, wherein the flow path includes a ring channel.
32. The method according to claim 30, wherein the flow path includes a plurality of supply openings.
33. The method according to claim 32, wherein each of the plurality of supply openings are separated by one holder ridge of a plurality of holder ridges.
34. The method according to claim 32, wherein the plurality of supply openings are arranged in a uniform distribution over a circumference of the plurality of supply openings.
35. The method according to claim 30, wherein the flow path includes a plurality of supply openings, each of the plurality of supply openings being separated by one holder ridge of a plurality of holder ridges, and the plurality of supply openings being arranged in a uniform distribution over a circumference of the plurality of supply openings.
36. The method according to claim 1, wherein the ring gap narrows towards the ring-shaped exit opening, and the flow path includes a ring channel.
37. The method according to claim 36, wherein the flow path includes a plurality of supply openings.
38. The method according to claim 37, wherein each of the plurality of supply openings are separated by one holder ridge of a plurality of holder ridges.
39. The method according to claim 37, wherein the plurality of supply openings are arranged in a uniform distribution over a circumference of the plurality of supply openings.
40. The method according to claim 36, wherein the flow path includes a plurality of supply openings, each of the plurality of supply openings being separated by one holder ridge of a plurality of holder ridges, and the plurality of supply openings being arranged in a uniform distribution over a circumference of the plurality of supply openings.
41. The method according to claim 36, wherein a conical mantle surface in a region of the ring-shaped exit opening in the flow path of the nozzle plate narrows the ring gap towards the ring-shaped exit opening.
42. The method according to claim 30, wherein a conical mantle surface in a region of the ring-shaped exit opening in the flow path of the nozzle plate narrows the ring gap towards the ring-shaped exit opening.
43. The method according to claim 1, wherein the cavity mold is an annular cavity mold to directly form a ring channel and an adjacent ring gap of the nozzle plate, the nozzle plate being a one-piece nozzle plate.
US09145005 1995-08-17 1998-09-01 Method for producing a nozzle plate Expired - Fee Related US6434826B1 (en)
DE19530193 1995-08-17
DE1995130193 DE19530193A1 (en) 1995-08-17 1995-08-17 Nozzle plate, in particular for fuel injection valves, and method of manufacturing a nozzle plate
US08809556 Division
PCT/DE1996/000980 Division WO1997007332A1 (en) 1995-08-17 1996-06-04 Injector plate, especially for fuel injection valves, and process for its production
US6434826B1 true US6434826B1 (en) 2002-08-20
ID=7769668
US08809556 Expired - Fee Related US5857628A (en) 1995-08-17 1996-06-04 Nozzle plate, particularly for fuel injection valves, and method for the production of a nozzle plate
US09145005 Expired - Fee Related US6434826B1 (en) 1995-08-17 1998-09-01 Method for producing a nozzle plate
US (2) US5857628A (en)
EP (1) EP0787257B1 (en)
JP (1) JPH10507510A (en)
DE (1) DE19530193A1 (en)
ES (1) ES2168474T3 (en)
WO (1) WO1997007332A1 (en)
JP3814815B2 (en) * 1998-03-25 2006-08-30 株式会社デンソー The injection hole plate and a method of manufacturing the same
KR20150038305A (en) * 2012-08-01 2015-04-08 쓰리엠 이노베이티브 프로퍼티즈 컴파니 Fuel injectors with non-coined three-dimensional nozzle outlet face
US1748402A (en) * 1925-06-26 1930-02-25 Taylor James Hall Process of making nozzles
GB665131A (en) 1949-02-17 1952-01-16 Rolls Royce Improvements relating to liquid fuel injectors
FR1169812A (en) 1956-04-16 1959-01-06 Mowag Motorwagenfabrik Ag multiple nozzle
DE1099487B (en) 1954-11-29 1961-02-16 Commercial Shearing ring nozzle
DE2433691A1 (en) 1974-07-12 1976-01-29 Int Harvester Co Needle valve for fuel injection in combustion engine - with opening of very large section and rapidly adjustable fuel throughput for optimum jet preparation
US4584065A (en) * 1983-08-27 1986-04-22 Kernforschungsanlage Julich Gmbh Activated electrodes
EP0212195A1 (en) 1985-07-16 1987-03-04 Starrfräsmaschinen AG Dust decrease and chip transferring and apparatus on a machine tool work station
US4745670A (en) * 1980-10-28 1988-05-24 Rockwell International Corporation Method for making chemical laser nozzle arrays
US4997528A (en) * 1986-11-13 1991-03-05 Maschinenfabrik Rieter Ag Mold for, and method of, fabricating a perforated body and perforated body for use as a friction spinning element
US5215260A (en) 1992-02-25 1993-06-01 Kallista, Inc. Plumbing spout
DE4404021A1 (en) 1994-02-09 1995-08-10 Bosch Gmbh Robert Nozzle plate, in particular for injection valves and methods of manufacturing a nozzle plate
US5697154A (en) * 1994-02-16 1997-12-16 Nippondenso Co., Ltd. Method of producing a fluid injection valve
US5718384A (en) * 1994-10-22 1998-02-17 Robert Bosch Gmbh Injection nozzle
US4798505A (en) 1985-07-16 1989-01-17 Starrfrasmaschinen Ag Process and apparatus for removal of dust and chip material at the machining station of a machine tool
US5857628A (en) 1999-01-12 grant
WO1997007332A1 (en) 1997-02-27 application
JPH10507510A (en) 1998-07-21 application
DE19530193A1 (en) 1997-02-20 application
EP0787257A1 (en) 1997-08-06 application
EP0787257B1 (en) 2001-11-14 grant
ES2168474T3 (en) 2002-06-16 grant
US6884370B2 (en) 2005-04-26 Matrix and method of producing said matrix
US4421153A (en) 1983-12-20 Method of making an aerofoil member for a gas turbine engine
US5820774A (en) 1998-10-13 Ceramic core for casting a turbine blade