COMPONENT FOR AN INJECTION SYSTEM AND INJECTION SYSTEM FOR MIXTURE-COMPRESSING, SPARK-IGNITION INTERNAL COMBUSTION ENGINES AND METHOD FOR PRODUCING SUCH A COMPONENT

Abstract

A component for an injection system for mixture-compressing, spark-ignition internal combustion engines, which is used to apportion a fluid under high pressure, in particular a highpressure line or fluid manifold. The component includes a main body on which at least one hydraulic connection is provided, at least the main body having the connection being formed by single stage or multistage forging, an interior being formed on the main body by chip-removing machining after forging and a connection channel, which intersects with the interior in an intersection region, being formed at the connection by chip-removing machining after forging. The intersection region is deburred by mechanical deburring. An injection system and a method for producing such a component are also described.

Claims

1-11. (canceled)

12. A component for an injection system for a mixture-compressing, spark-ignition internal combustion engine, comprising: a main body on which at least one hydraulic connection is provided, at least the main body having the connection being formed by single stage or multistage forging, an interior of the main body being formed on the main body by chip-removing machining after forging, and a connection channel, which intersects with the interior in an intersection region, being formed at the hydraulic connection by chip-removing machining after forging; wherein the intersection region is deburred by mechanical deburring.

13. The component as recited in claim 12, wherein the component is a high-pressure line or fluid manifold.

14. The component as recited in claim 12, wherein the intersection region is deburred by mechanical retraction deburring.

15. The component as recited in claim 14, wherein a forged material of the main body is provided at an internal wall of the main body, which in operation is exposed to high pressure of fluid, with a material state under compressive residual stress.

16. The component as recited in claim 15, wherein; (i) the internal wall provided with the material state under compressive residual stress of the main body defines the interior, (ii) the internal wall provided with the material state under compressive residual stress of the main body extends over the intersection region, and/or (iii) the internal wall provided with the material state under compressive residual stress of the main body extends at least over the connection channel of the hydraulic connection.

17. The component as recited in claim 16, wherein: (i) the hydraulic connection has a connection chamber which is connected via the connection channel to the interior, and (ii) the internal wall provided with the material state under compressive residual stress extends from the connection channel at least in part over the connection chamber of the connection.

18. The component as recited in claim 12, wherein: (i) the interior of the main body is formed by at least one bore, and/or (ii) the connection channel is formed by at least one bore.

19. The component as recited in claim 12, wherein: (i) the main body and the at least one hydraulic connection are formed from an individual forged part, and/or (ii) the main body is formed from a material which is based on an austenitic special steel.

20. The component as recited in claim 19, wherein the austenitic special steel has a material number of 1.4301 or 1.4307.

21. An injection system for a mixture-compressing, spark-ignition internal combustion engine, which is used for injecting a fluid which is gasoline and/or ethanol and/or a mixture including fuel, the injection system comprising: a main body on which at least one hydraulic connection is provided, at least the main body having the connection being formed by single stage or multistage forging, an interior of the main body being formed on the main body by chip-removing machining after forging, and a connection channel, which intersects with the interior in an intersection region, being formed at the connection by chip-removing machining after forging; wherein the intersection region is deburred by mechanical deburring.

22. A method for producing a component for an injection system for a mixture-compressing, spark-ignition internal combustion engine, which is used to apportion a fluid under high pressure, the fluid being gasoline and/or ethanol and/or a mixture including fuel, the method comprising the following steps: forming a main body and at least one hydraulic connection provided on the main body by single stage or multistage forging' forming an interior on the main body by chip-removing machining after the forging; and forming a connection channel, which intersects with the interior in an intersection region, at the hydraulic connection, by chip-removing machining after the forging; and deburring the intersection region by mechanical deburring.

23. The method as recited in claim 22, wherein the component is a high-pressure line or a fluid manifold.

24. The method as recited in claim 22, wherein: (i) a cutting edge, used for mechanical deburring, of a retraction deburring tool for deburring is applied against the intersection region) by a liquid cutting fluid supplied for cooling during the mechanical deburring, and/or (ii) a cutting edge, used for mechanical deburring, of a retraction deburring tool s applied against the intersection region for deburring by rotating the retraction deburring tool.

25. The method as recited in claim 22, wherein a liquid cutting fluid supplied for cooling during mechanical deburring is at least intermittently placed under such a high pressure that a forged material of the main body is provided at an internal wall of the main body, which in operation is exposed to high pressure of the fluid, with a material state under compressive residual stress.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Preferred exemplary embodiments of the present invention are explained in greater detail in the following description with reference to the figures, in which corresponding elements are provided with matching reference numbers.

[0013] FIG. 1 shows an injection system for a mixture-compressing, spark-ignition internal combustion engine with a component in the form of a fuel manifold in a schematic sectional representation corresponding to one exemplary embodiment of the present invention.

[0014] FIG. 2 shows the portion designated II in FIG. 1 of the component corresponding to the exemplary embodiment in a detailed, schematic representation, according to the present invention.

[0015] FIG. 3 shows the portion designated III in FIG. 1 of the component corresponding to the exemplary embodiment in a detailed, schematic representation in a section perpendicular to a longitudinal axis of the component.

[0016] FIG. 4 shows a schematic representation of mechanical deburring of an intersection region to explain one possible example configuration of the present invention.

DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS

[0017] FIG. 1 shows an injection system 1 with a fuel manifold (fluid manifold) 2 in a schematic sectional representation corresponding to one exemplary embodiment. In this exemplary embodiment, the fuel manifold 2 of the fuel injection system 1 is a component 3 configured according to the present invention. A high-pressure pump 4 is furthermore provided. The high-pressure pump 4 is connected to the fuel manifold 2 via a fuel line 5 configured as a high-pressure line 5. During operation, a fuel or a mixture including fuel is supplied as the fluid to an inlet 6 of the high-pressure pump 4. The high-pressure line 5 can correspondingly also be configured as component 3' according to the present invention.

[0018] The fuel manifold 2 is used for storing and distributing the fluid to injection valves 7 through 10 configured as fuel injection valves 7 through 10 and reduces pressure fluctuations and pulsations. The fuel manifold 2 can also be used to attenuate pressure pulsations that may arise during switching of the fuel injection valves 7 through 10. During operation, high pressures p may occur at least intermittently in an interior 11 of component 3. The high-pressure line 5 has hydraulic connections 12, 12' configured as high-pressure inlet 12 and high-pressure outlet 12', which can optionally be interchanged, and a main body 13.

[0019] The fuel manifold 2 has a tubular main body 14 which is formed by single stage or multistage forging. A hydraulic connection 15 configured as a high-pressure inlet 15 and a plurality of hydraulic connections 16 through 19 configured as high-pressure outlets 16 through 19 or cups 16 through 19 are provided on the tubular main body 14. A hydraulic connection 20 configured as a pressure sensor connection 20 is furthermore provided on the tubular main body 14. In this exemplary embodiment, the tubular main body 14, the high-pressure inlet 15, the high-pressure outlets 16 through 19 and the pressure sensor connection 20 are formed from a single forged part 14'. The high-pressure inlet 15, the high-pressure outlets 16 through 19 and the pressure sensor connection 20 are thus forged on the main body 14.

[0020] The fuel line 5 is connected at its high-pressure inlet 12 to the high-pressure pump 4 and at its high-pressure outlet 12' to the high-pressure inlet 15 of the fuel manifold 2. The fuel injection valves 7 through 10 are in each case connected to the high-pressure outlets 16 through 19 of the fuel distributor 2. A pressure sensor 21, which is connected to the pressure sensor connection 20, is furthermore provided. The tubular main body 14 is closed at one end 22 by a screw plug 23. In a modified configuration, an axial high-pressure inlet may be provided at one end 24 instead of the lateral and/or radial high-pressure inlet 15.

[0021] After forging, the tubular main body 14 or the individual forged part 14' is machined by at least one chip-removing machining operation. In this exemplary embodiment, after forging, a bore 25 is additionally formed in the tubular main body 14 to form the interior 11. During operation, the fluid supplied to the high-pressure inlet 15 can be distributed via the interior 11 to the fuel injection valves 7 through 10 connected to the high-pressure outlets 16 through 19.

[0022] Bores 26 through 31 are moreover introduced into the individual forged part 14' by chip-removing machining. Bores 27 through 30 are here used for the high-pressure outlets 16 through 19. Bore 26 is used for the high-pressure inlet 15. Bore 31 is used for the pressure sensor connection 20. A thread 22' can furthermore be cut into the bore 25 at the end 22 of the main body 13.

[0023] Bores 32 through 37, which form connection chambers 32 through 37, can moreover be provided at the high-pressure inlet 15, the high-pressure outlets 16 through 19 and the pressure sensor connection 20. In this exemplary embodiment, the bore 25 is oriented axially with regard to a longitudinal axis 38. Bores 26 through 37 are oriented radially or radially eccentrically with regard to the longitudinal axis 38. In the case of a radial or radially eccentric orientation with regard to the longitudinal axis 38, it is then preferably possible, in the case of fastening for example in an engine compartment, to obtain an orientation of bores 26, 31, 32, 37 of connections 15, 20 or bores 27 through 30 and 33 through 36 of connections 16 through 19 above or below the longitudinal axis and/or from the longitudinal axis 38 which points away from or toward an engine.

[0024] Bores 26 through 31 form connection channels 26 through 31 which intersect with the interior 11. These connection channels 26 through 31 connect bores 32 through 37 to the interior 11. Bores 26 through 31 here intersect with the bore 25 which forms the interior 11. This results in intersection regions 40 through 45 on which burrs remain after chip-removing machining. The intersection regions 40 through 45 are deburred by mechanical deburring.

[0025] One possible configuration of connections 15, 20 is described by way of example on the basis of connection 15 and on the basis of FIG. 2. One possible configuration of connections 16 through 19 is described by way of example with reference to connection 16 on the basis of FIG. 3. One possible configuration for mechanical deburring is described on the basis of FIG. 4. This gives rise to one possible configuration of a component 3 which is configured according to an exemplary embodiment of the present invention. Another component 3' of the injection system 1, for example the high-pressure line 5, may also be correspondingly embodied, it being possible for connections 12, 12' to be correspondingly configured and mechanically deburred.

[0026] FIG. 2 shows the portion designated II in FIG. 1 of component 3 corresponding to the exemplary embodiment in a detailed, schematic representation. A conical and/or stepped transition 46 is provided between bores 26, 32 in this exemplary embodiment. Bores 26, 32 may here in particular be arranged coaxially. Depending on the application, a suitable thread can also be provided at the connection 15, for example for connecting the high-pressure line 5.

[0027] Deburring of the intersection region 40 may be carried out from the bore 32, as is also explained on the basis of FIG. 4. A chamfer 40' can be formed at the intersection region 40 as a result.

[0028] FIG. 3 shows the portion designated III in FIG. 1 of the component 3 corresponding to the exemplary embodiment in a detailed, schematic representation in a section perpendicular to the longitudinal axis 38. In this exemplary embodiment, the bore 33 has a flat bore bottom 47, the bore 33 being arranged eccentrically relative to the bore 27. The bore 27 may here be oriented radially relative to the longitudinal axis 38. The bore 33 is then oriented radially eccentrically with regard to the longitudinal axis 38. Deburring of the intersection region 41 may be carried out from the bore 33, as is illustrated on the basis of FIG. 4. A chamfer 41' can be formed at the intersection region 41 as a result.

[0029] In this exemplary embodiment, the connection 15 can thus take the form of a valve cup 15.

[0030] FIGS. 2 and 3 illustrate options for implementing non-eccentric and eccentric connection geometries in which mechanical deburring can be carried out.

[0031] FIG. 4 shows a schematic representation of mechanical deburring of an intersection region 40 by means of retraction deburring tool 50 to explain a possible configuration of the present invention. The bores 25, 26 intersect with one another in the intersection region 40. The retraction deburring tool 50 can be inserted via the bore 32 (FIG. 2) along an axis 51. The retraction deburring tool 50 has at least one cutting edge 52. On insertion, the cutting edge 52 can be entirely or partially folded into a circumferential surface 53 of the retraction deburring tool 50. The cutting edge 52 can be folded out by rotation 54 and/or by application of a cutting fluid which can be supplied via the retraction deburring tool 50.

[0032] Retracting the retraction deburring tool 50 in a retraction direction 55 results in mechanical deburring of the intersection region 40 by way of the cutting edge 52 as a result of the rotation 54. Rotation 54 and/or the supplied liquid cutting fluid here applies the cutting edge 52 against the intersection region 40. The chamfer 40' can be formed in the process. The retraction deburring tool 50 can then be removed, the cutting edge 52 entirely or partially folding back into the circumferential surface 53.

[0033] Mechanical removal of a burr and chip-removing de-edging can thus be achieved in the intersection region 40. Depending on the configuration of the retraction deburring tool 50, the cutting edge 52 may for example also be held in place by a spring in order to facilitate insertion and removal of the retraction deburring tool 50.

[0034] The time sequence of the chip-removing machining for configuring bores 25 through 37 can be implemented in a suitable manner. Mechanical deburring of intersection regions 40 through 45 can here be suitably integrated into or follow on from this machining.

[0035] In one possible implementation of the method, the bore 25 can firstly be drilled to provide the interior 11. Bores 32 through 37 for the connection geometries of connections 15 through 20 and bores 26 through 31 serving as connection channels 26 through 31 to the interior 11 can then be drilled. Mechanical deburring of the intersection regions 40 through 45 can then proceed. Mechanical deburring can thus follow on from the chip-removing machining.

[0036] In one possible embodiment of the method, once bore 25 for the interior 11 has been drilled, all the connection geometries are machined, in particular all bores 32 through 37 are drilled, then all bores 26 through 31 serving as connection channels 26 through 31 or connection bores 26 through 31 are drilled and finally all intersection regions 40 through 45 are mechanically deburred.

[0037] One possible modification of this method involves carrying out drilling and deburring in a different sequence which integrates deburring into the chip-removing machining. If a plurality of intersection regions 40 through 45 are mechanically deburred, a machining sequence may in each case relate to one of connections 15 through 20. This means, for example at connection 15, that bore 32 is drilled, then bore 26 is drilled and then the intersection region 40 is mechanically deburred. These steps can be carried out correspondingly in succession for each of connections 15 through 20.

[0038] Mechanical deburring thus does not necessarily proceed after completion of chip-removing machining. In particular, mechanical deburring can thus also be integrated into the chip-removing machining. By suitable process parameters and the selection of a suitable cutting fluid, it is also possible for an internal wall 60 extending, inter alia, from the bore 25 over the intersection region 40 and through the bore 26 to be provided with a material state under compressive residual stress. This internal wall 60 can also extend into the transition 46 (FIG. 2) or the bore bottom 47 (FIG. 3) and at least in part over bores 32 through 37. Provision of the internal wall 60 with the material state under compressive residual stress results in improved cyclic strength.

[0039] The present invention is not limited to the described exemplary embodiments.