High-pressure fuel pump

Abstract

A high-pressure fuel pump includes a housing, at least one piston, and a sealing device. The device is positioned on the piston so as to surround the piston, and includes a seal carrier. The carrier is connected, at least in sections, to the housing, and includes at least one radially peripheral portion that is materially bonded to the housing via a capacitor discharge weld connection. Such a pump enables improved cycle times and reduced error rates during production.

Claims

1. A fuel pump, comprising: a housing; at least one piston; a sealing device positioned on the at least one piston so as to radially surround the piston; and a seal carrier having a radially outer edge region, wherein the radially outer edge region includes a connecting portion with an angle of approximately 30 to 60 relative to an axis of the at least one piston, wherein the connecting portion extends radially approximately 2 millimeters to 4 millimeters, and wherein the connecting portion is substance-bonded to the housing of the fuel pump via a capacitor discharge weld connection.

2. The fuel pump as claimed in claim 1, wherein the radially outer edge region is connected to the housing of the fuel pump via a press fit.

3. The fuel pump as claimed in claim 1, wherein: the housing includes a radially peripheral shoulder, and the connecting portion is substance-bonded to the housing via the capacitor discharge weld connection at the radially peripheral shoulder of the housing.

4. The fuel pump as claimed in claim 1, wherein the fuel pump is a high-pressure fuel pump.

5. The fuel pump as claimed in claim 1, wherein the angle between the connecting portion and the axis of the at least one piston is approximately 40 to 50.

6. A method of producing a fuel pump, comprising: positioning a fuel pump housing at a first electrode of a capacitor discharge welding device; positioning a seal carrier on a radially inner portion of the housing; positioning a substantially annular second electrode of the welding device on a radially peripheral connecting portion of the seal carrier, wherein the second electrode is configured to apply a predefinable force to the seal carrier; at least one of adjusting and centering the seal carrier in the housing; and operating the welding device to form a capacitor discharge weld connection between the radially peripheral connecting portion of the seal carrier and the housing.

7. The method as claimed in claim 6, wherein: an edge region of the seal carrier has a press fit at the radially inner portion of the housing; and the capacitor discharge weld connection is formed at the radially peripheral connecting portion of the seal carrier adjacent to the edge region.

8. The method as claimed in claim 6, further comprising: during the operation of the capacitor discharge welding device, determining at least one of a force of the seal carrier relative to the housing, a movement of the seal carrier relative to the housing, and a current development of the capacitor discharge welding device and comparing the at least one of determined force, determined relative movement, and determined current development with at least one corresponding stored value for the force, relative movement, and current development and determining a quality of the weld connection based on the comparison.

9. The method as claimed in claim 6, wherein the fuel pump is a high-pressure fuel pump.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Further features, possible applications and advantages of the disclosure arise from the description below of exemplary embodiments of the disclosure which are explained with reference to the drawings, wherein the features, both alone and in various combinations, may be important for the disclosure without further explicit reference to this being required. The drawing shows:

(2) FIG. 1 a simplified diagrammatic depiction of a fuel system for an internal combustion engine;

(3) FIG. 2 an extract of a longitudinal section through a high-pressure fuel pump;

(4) FIG. 3 an axial sectional view of the radially outer edge region of the seal carrier and of a portion of the housing of the high-pressure fuel pump according to a possible embodiment;

(5) FIG. 4 an axial sectional view of a radially outer edge region of the sealing device and of a portion of the housing of the high-pressure pump according to another possible embodiment;

(6) FIG. 5 an axial sectional view of a radially outer edge region of a seal carrier and of a portion of a housing according to a further possible embodiment;

(7) FIG. 6 an axial sectional view of a seal carrier and of a housing according to a possible embodiment;

(8) FIG. 7 a diagrammatic depiction of a sectional view of a part of the high-pressure fuel pump during performance of the capacitor discharge welding process; and

(9) FIG. 8 a simplified flow diagram with possible method steps in the production of the high-pressure fuel pump.

DETAILED DESCRIPTION

(10) FIG. 1 shows a fuel system 10 for an internal combustion engine, not shown in further detail, in a simplified diagrammatic depiction. Fuel is delivered from a fuel tank 12 via a suction line 14 by means of a predelivery pump 16, and a low-pressure line 18 via an inlet 20 of a quantity control valve 24 which can be activated by an electromagnetic actuation device 22, to a delivery chamber 26 of a high-pressure fuel pump 28. For example, the quantity control valve 24 may be an inlet valve with forced opening of the high-pressure fuel pump 28.

(11) In the present case, the high-pressure fuel pump 28 is configured as a piston pump, wherein a piston 30 can be moved, vertically in the drawing, by means of a cam disk 32 (drive). An outlet valve 40, drawn as a spring-loaded check valve in FIG. 1, is arranged hydraulically between the delivery chamber 26 and an outlet 36 of the high-pressure fuel pump 28, and can open towards the outlet 36. The outlet 36 is connected to a high-pressure line 44 and via this to a high-pressure accumulator 46 (common rail). Furthermore, a pressure-limiting valve 42, also drawn as a spring-loaded check valve, is arranged hydraulically between the outlet 36 and the delivery chamber 26, and can open towards the delivery chamber 26.

(12) In operation of the fuel system 10, the predelivery pump 16 transports fuel from the fuel tank 12 into the low-pressure line 18. The quantity control valve 24 may be closed and opened depending on the respective demand for fuel. In this way, the fuel quantity delivered to the high-pressure accumulator 46 is influenced. The electromagnetic actuation device 22 is activated by a control and/or regulator device 48.

(13) FIG. 2 shows an extract of a high-pressure pump 28 which comprises a seal carrier 68, formed approximately pot-shaped, and a piston spring 70 which is arranged radially outwardly around a portion of the seal carrier 68 and configured as a coil spring, and rests with an end portion on the seal carrier 68. A spring plate 72 is pressed onto an end portion of the piston 30, at the bottom in the drawing and facing the drive, and receives an end portion of the piston spring 70.

(14) A piston seal, also known as a low-pressure seal and referred to as the sealing device 74, is arranged radially inside the seal carrier 68 and radially surrounds the lower second portion (facing the drive) of the piston 30; it also seals a fluid space (step chamber) present between the housing 50 and the seal carrier 68, outwardly towards the engine block 53. The piston 30 can move along the longitudinal axis 64 relative to the sealing device 74. In a rough approximation, the sealing device 74 as a whole has an annular structure.

(15) In the present case, the sealing device 74 is supported axiallyat the top in FIG. 2by a holding portion 76 arranged inside the seal carrier 68 and also formed approximately hat-like. In the drawing, a spatial region above the sealing device 74 constitutes a fuel side, and a spatial region below the sealing device 74 is an oil side.

(16) Furthermore, the sealing device 74 is supported axiallyat the bottom in FIG. 2by a peripheral edge portion of the seal carrier 68 which is bent radially inward. It is understood that the sealing device 74 may also in some cases have a slight axial play inside a region determined by the holding portion 76 and said edge portion.

(17) The sealing device 74 is arranged on the piston 30 radially outwardly along the longitudinal axis 64, and configured so as to be substantially rotationally symmetrical.

(18) FIG. 3 shows a part of the second portion 92, which extends substantially radially outward and is also shown in FIG. 2, and a radially outer edge region 93 which is adjacent to the second portion 90 and has a connecting portion 94. According to the embodiment shown in FIG. 3, the connecting portion 94 has an angle 96 relative to the piston axis which, in a possible embodiment, amounts to approximately 45. Preferably, the angle 96 lies in ranges between approximately 30 and 60. It is advantageous if the angle 96 lies in a range between 40 and 50, and quite particularly advantageous if the angle 96 amounts to approximately 45, as shown in FIG. 3.

(19) In order to achieve a connecting length 97 of around 1 mm in the performance of the capacitor discharge welding process, it is advantageous if a radius 98 of at least around 0.3 mm of the housing 50 meets a face of the seal carrier 68 or a connecting portion 94 which is angled by the angle 96. Preferably, the more solid component has the radius 98. In this way, the conduction cross-section is reduced so that the solid component (in this case, the housing 50 of the high-pressure fuel pump 28) is melted substantially as early as the thinner-walled component (in this case, the seal carrier 68) and a robust weld seam is created. In order to avoid an undesirable or undefined shunt during the welding process, according to the embodiment shown in FIG. 3, a minimum gap 99 of around 0.1 mm is retained between the housing 50 and the edge region 93 of the seal carrier 68.

(20) FIG. 4 shows the same portion of the housing 50 of the high-pressure fuel pump 28 and seal carrier 68 as in FIG. 3, but according to another possible embodiment in which the weld seam is formed by means of a ring bulge 100. The ring bulge 100 is formed on the housing 50 of the high-pressure pump 28 before the welding process. The connecting portion 94 is here tilted by an angle 101 of around 90 about the longitudinal axis 64 of the piston 30. This allows a particularly stable weld, but other angles of the connecting portion 94 are however possible.

(21) According to another possible embodiment, as shown in FIG. 5, it may be provided to arrange a shoulder 102 on the housing 50 of the high-pressure fuel pump 28 at which the capacitor discharge welding takes place, whereby it is possible to shorten the lever arm and reduce the load.

(22) FIG. 6 shows a further possible exemplary embodiment in which the radially outer edge region 93 is also pressed onto the housing 50 of the high-pressure fuel pump 28, whereby an even more stable connection is possible. Evidently, the enlarged contact area must be taken into account in performance of the capacitor discharge welding process.

(23) FIG. 7 shows an arrangement with which the capacitor discharge welding process according to the disclosure can be performed. For this, the housing 50 of the high-pressure fuel pump 28 is arranged at a first electrode 110. A substantially annular second electrode 112 is arranged at the connecting portion 94 of the seal carrier 68. The connecting portion 94 is formed for example as shown in FIG. 3. Preferably, the second electrode 112 is configured such that it applies a predefinable force to the seal carrier 68 or the connecting portion 94 in a springing and/or floating manner. After adjusting and/or centering the seal carrier 68 in the housing 50, the capacitor discharge welding process is carried out so that a weld seam is formed between the connecting portion 94 and the part of the housing 50 lying thereon.

(24) FIG. 8 shows in a flow diagram method steps which are carried out according to a possible embodiment of the method of the disclosure in the production of the high-pressure fuel pump 28.

(25) The method begins with a step 200 in which the housing 50 of the high-pressure fuel pump 28 is positioned on the first electrode 110. In a step 201, the seal carrier 68 is inserted and pre-positioned. In a step 202, the second electrode 112 is applied and mounted in a floating fashion. Preferably, its own weight is selected such that the force necessary for the later welding process is produced.

(26) In a step 203, the arrangement is centered, and in step 204, the monitoring of the process parameters begins, in particular the sink travel, the force and/or the current development in performance of the welding process.

(27) In a step 205, the capacitor discharge welding takes place so that the seal carrier 68 in the connecting portion 94 is substance-bonded to the housing 50 of the high-pressure fuel pump 28.

(28) In a step 206, the process parameters monitored in step 204 are evaluated. Here, the sink travel of the second electrode 112, also known as the settling travel, and the current development in performance of the capacitor discharge welding process, are particularly relevant. These output parameters from production are compared with predefined values in a step 207. If deviations can be found which exceed a predefinable tolerance threshold, in a step 209 the production process of this high-pressure fuel pump 28 is interrupted and it is declared rejected. Where applicable, some parameters for the welding process are adapted. If the monitored process parameters lie within the predefinable tolerance ranges, the method ends in a step 208.

(29) Because the output parameters can be examined directly for defects, any rejection is declared significantly earlier, which substantially facilitates any corrective intervention and saves defect costs.

(30) By the use of the capacitor discharge welding process, the cycle time is reduced in the production of the high-pressure fuel pump 28, in particular in the substance-bonding of the seal carrier 68 to the housing 50 of the high-pressure fuel pump 28. Furthermore, by the use of the capacitor discharge welding process, there is no need for regular cleaning of the protective glass, which is required for example with the laser welding process in order to verify fault-free welding.

(31) With the method according to the disclosure, a leaking laser weld seam is not established only in the line-end test during the leak test performed there, but it is possible, already during production by the analysis of process parameters, to establish whether the welding process was successful.