Fuel Delivery Assembly for an Internal Combustion Engine
20170342952 · 2017-11-30
Assignee
Inventors
Cpc classification
F02M55/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M2200/8023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M2200/856
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/145
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M2200/853
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M61/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A fuel delivery assembly for an internal combustion engine, including an injector cup, a fuel injector received therein, and a spring clip is disclosed. The injector cup has a circumferential wall with an external shoulder. The fuel injector has a shoulder which is axially spaced apart from the injector cup. The spring clip has a base portion with two radially compliant webs bearing against the shoulder of the circumferential wall and being in force-fit engagement with the circumferential wall. The spring clip has an axially compliant portion bearing against the shoulder of the fuel injector and being elastically deformable to bias the fuel injector in axial direction from the upper end towards the lower end.
Claims
1. A fuel delivery assembly for an internal combustion engine, comprising a fuel injector having a fuel inlet portion, an injector cup, and a spring clip, wherein the injector cup extends along a longitudinal axis from an upper end to a lower end, has a circumferential wall with an external shoulder, and an opening adjacent to the lower end, the fuel inlet portion of the fuel injector is received in the injector cup such that the fuel injector projects from the injector cup through the opening, the fuel injector has a shoulder which is axially spaced apart from the injector cup, the spring clip has a base portion with two radially compliant webs bearing against the shoulder of the circumferential wall to prevent displacement of the base portion in an axial direction of the injector cup towards the upper end and being in force-fit engagement with the circumferential wall to prevent displacement of the base portion in the axial direction towards the lower end, and the spring clip has an axially compliant portion bearing against the shoulder of the fuel injector and being elastically deformable to bias the fuel injector in the axial direction and the fuel injector from the upper end towards the lower end.
2. The fuel delivery assembly according to claim 1, further comprising a clamp, wherein the injector cup has two slots which perforate the circumferential wall and are arranged axially between the opening and the shoulder of the circumferential wall, the clamp has two legs, each leg being positioned in one of the slots so that axial displacement of the clamp with respect to the injector cup in a direction towards the lower end is blocked, and the fuel inlet portion has a radial protrusion which bears on the legs of the clamp so that the clamp blocks axial displacement of the fuel injector with respect to the clamp in the axial direction of the fuel injector from the upper end towards the lower end.
3. The fuel delivery assembly according to the claim 2, wherein the base portion is arranged axially between the slots and the shoulder of the circumferential wall and the axially compliant portion is arranged axially between the slots and the shoulder of the fuel injector.
4. The fuel delivery assembly according to claim 2, wherein the base portion has a partial annular shape formed by the webs and opens in a first radial direction, and the clamp is generally U-shaped and opens in a second radial direction, opposite to the first radial direction.
5. The fuel delivery assembly according to claim 1, wherein the base portion has a flattened section which engages with a flat surface region of the circumferential wall.
6. The fuel delivery assembly according to claim 1, wherein each of the webs is in full-area contact with the circumferential wall over an angular range of at least 45°.
7. The fuel delivery assembly according to claim 1, wherein the spring clip is a one-piece, sheet-metal part.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] In the figures:
[0025]
[0026]
[0027]
[0028]
[0029]
DETAILED DESCRIPTION
[0030] In the exemplary embodiments and figures, similar, identical or similarly acting elements are provided with the same reference symbols. In some figures, individual reference symbols may be omitted to improve the clarity of the figures.
[0031]
[0032] The injector cup 20 is shown in an unassembled state in the perspective view of
[0033] The injector cup 20 is hollow. It has a circumferential wall 230 which extends from the upper end 210 to the lower end 220 and forms a recess of the injector cup 20. Adjacent to the lower end 220, the recess ends in an opening 250. Adjacent to the upper end 210, the injector cup 20 has a fuel inlet opening (not visible in the figures) which perforates the circumferential wall 30 for hydraulically coupling the recess to the fuel rail 50 via the outlet port 510 of the fuel rail 50.
[0034] Through the opening 250, a fuel injector 10 is shifted into the recess of the injector cup 20 so that a fuel inlet portion 110 of the fuel injector 10 is arranged in the recess. The fuel inlet portion 110 of the fuel injector 10 is also shown in
[0035] The fuel injector 10 projects from the injector cup 20 in a first axial direction which is directed from the upper end 210 towards the lower end 220 of the injector cup 20. The fuel injector 10 is, for example, configured for injecting fuel directly into a combustion chamber of an internal combustion engine.
[0036] In the present embodiment, the circumferential wall 230 of the injector cup 20 is perforated adjacent to the lower end 220 by two slots 260. The slots 260 are arranged in mirror symmetrical fashion with respect to a plane comprising the longitudinal axis L. The slots 260 are each delimited by two surfaces which extend parallel to the longitudinal axis L and by two circumferentially extending surfaces which face in the first axial direction and in a second axial direction, opposite to the first axial direction.
[0037] The fuel inlet portion 110 of the fuel injector 10 has a radial protrusion 130. In the present embodiment, the radial protrusion 130 is a circumferential flange which protrudes from a generally cylindrical outer surface of the fuel inlet portion 110 in the present embodiment. In the assembled state of the fuel delivery assembly 1, the protrusion 130 of the fuel inlet portion 110 is axially offset in the second axial direction at least with respect to a portion of the slots 260, specifically with respect to the circumferentially extending surface which faces in the second axial direction.
[0038] The fuel delivery assembly 1 further comprises a clamp 40 which is shown separately in
[0039] The fuel delivery assembly 1 of the present embodiment further comprises a spring clip 30, shown separately in a perspective view in
[0040] The base portion 310 has two radially compliant webs 315 which engage around the circumferential wall 230. The thickness of the webs 315—i.e., the material thickness in radial direction—corresponds to the thickness of the sheet metal from which the spring clip 30 is manufactured. The longitudinal extension of the webs 315 is about 4 to 5 times as large as the material thickness in radial direction so that the webs 315 are elastically deformable in radial direction and rigid in axial direction.
[0041] The base portion 310 is shaped such that, in the assembled state, the radially compliant webs 315 are elastically deformed in radially outward direction. Further, the shape of an inner circumferential surface portion of the webs 315 matches the shape of the circumferential wall 230 so that the inner circumferential surface portions are in full area contact with the circumferential wall 230, in particular over an angular range of at least 45° for each web 315. In this way, a press-fit connection is established between the base portion 310 and the circumferential wall 230 of the injector cup 20 for preventing displacement of the base portion 310 in the first axial direction.
[0042] Between the webs 315, the base portion 310 has an interconnection portion extending circumferentially from one of the webs 315 two the other one of the webs 315 for connecting the webs 315 to one another. The interconnecting portion has a flattening or flattened section 340 which is in full area contact with flat surface region 270 of the circumferential wall 234. In this way, the angular position of the spring clip 30 relative to the injector cup 20 is set, i.e., indexing of the spring clip 30 relative to the injector cup 20 is achieved.
[0043] Remote from the interconnection portion, the webs 315 have free ends so that the base portion 310 has a partial annular general shape, formed by the webs 315 and in the present embodiment also by the interconnection portion. The partial annular shape is open in a first radial direction R1.
[0044] The U-shaped clamp 40 is open in a second radial direction R2, opposite to the first to the direction R1. In this way, the free ends of the legs 410 of the clamp 40 face towards the interconnection portion of the base portion 310 of the spring clip 30 and the free ends of the webs 315 face towards the closed end of the U-shape of the clamp 40.
[0045] The base portion 310 of the spring clip 30 is arranged axially subsequent to the slots 260 in a direction towards the upper end 210 of the injector cup 20, i.e., in the second axial direction. Subsequent to the base portion 310 in the second axial direction, the circumferential wall 230 has an external shoulder 240. In the present embodiment, the circumferential wall 230 has a first portion adjacent to the upper end 210 having a first diameter and a second portion adjacent to the lower end 220 having a second diameter, the second diameter being smaller than the first diameter. An interface between the first and second portions is represented by the shoulder 240, being embodied as a step of the external surface of the circumferential wall 230 in the present embodiment.
[0046] The webs 315 of the base portion 310 of the spring clip 30 bear against the shoulder 240. In this way, axial displacement of the base portion 310 in the second axial direction is blocked by form fit engagement between the webs 315 and the shoulder 240.
[0047] The fuel injector 10 also has a shoulder 120, being axially spaced apart from the injector cup 20 in the first axial direction. In particular, the shoulder 120 is positioned subsequent to the fuel inlet portion 110 in the first axial direction on the fuel injector 10. For example, the shoulder 120 of the fuel injector 10 is a step of a housing of the fuel injector 10. The axially compliant portion 320 of the spring clip 30 bears against the shoulder 120 of the fuel injector 10.
[0048] Specifically, in the present embodiment, the axially compliant portion 320 has two axially compliant webs 325 which are curved and/or kinked such that they each have a contact region which is in contact with the shoulder 120 and laterally arranged between a free first end and a second end which merges with the connection portion 330. The first and second ends are spaced apart from the shoulder 120 of the fuel injector 10, i.e., they are axially displaced in the second axial direction with respect to the contact region. The material thickness of the axially compliant webs 325 corresponds in particular to the thickness of the sheet-metal from which the spring clip 30 is manufactured.
[0049] The axial positions of the shoulder 120 of the fuel injector 10, shoulder 240 of the injector cup 20, as well as the axial positions and dimensions of the clamp 40, the slots 260 of the injector cup 20, and the radial protrusion 130 of the fuel inlet portion 110 of the fuel injector 10 are selected such that the axially compliant webs 325 of the axially compliant portion 320 of the spring clip 30 are elastically deformed when the fuel delivery assembly 1 is assembled. This way, the spring clip 30 presses the radial protrusion 130 of the fuel injector 10 against the clamp 40 and the clamp 40 against the circumferential wall 230 of the injector cup 20 in axial direction.
[0050] One or more embodiments have been described herein in an illustrative manner, and it is to be understood that the terminology which has been used is intended to be in the nature of words of description rather than of limitation. Obviously, many modifications and variations of the invention are possible in light of the above teachings. The description above is merely exemplary in nature and, thus, variations may be made thereto without departing from the spirit and scope of the invention as defined in the appended claims.