ADJUSTMENT ELEMENT AND AN INSTALLATION METHOD FOR AN ADD-ON PART WITH THE HELP OF THE ADJUSTMENT ELEMENT
20230407895 · 2023-12-21
Inventors
Cpc classification
B29C45/14467
PERFORMING OPERATIONS; TRANSPORTING
F16B37/067
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B60Q1/045
PERFORMING OPERATIONS; TRANSPORTING
F16B5/0225
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B60Q1/2642
PERFORMING OPERATIONS; TRANSPORTING
B29C45/0081
PERFORMING OPERATIONS; TRANSPORTING
F16B5/0233
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C45/2618
PERFORMING OPERATIONS; TRANSPORTING
F16B37/041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16B5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An adjustment element with which a component is fastenable and positionable in the space and including a sleeve-like hollow screw with a first and a second axial end and an outer thread to which a component can be retained and can be positioned in axial direction of the hollow screw, adjacent to the first axial end, the hollow screw has a fastening collar which is configured integrally and projects radially to the inside and which encompasses a tubular fastening opening of the hollow screw, and an axial support sleeve arranged within the tubular fastening opening so that the hollow screw is rotatably fastenable with a fastening means to a component in a rotatable manner, which passes through the axial support sleeve.
Claims
1. An adjustment element with which a component is fastenable and positionable in the space, including the following features: a. a sleeve-like hollow screw with a first and a second axial end, a drive feature and an outer thread to which a component is retainable and is positionable in axial direction of the hollow screw, b. adjacent to the first axial end, the hollow screw comprises a fastening collar which is configured integrally and projects radially to the inside and which encompasses a tubular fastening opening of the hollow screw, and c. an axial support sleeve is arranged within the tubular fastening opening so that the hollow screw is rotatably fastenable with a fastening means to a component, which passes through the axial support sleeve.
2. The adjustment element according to claim 1, the axial support sleeve of which is flush with the hollow screw at the first axial end and projects beyond an end, located inside of the hollow screw, of the tubular fastening opening so that the hollow screw is rotatably fastenable with the fastening means.
3. The adjustment element according to claim 2, to which end of the support sleeve located inside of the hollow screw, a support disc with a central opening is arranged, the outer disc diameter of which exceeds an outer diameter of the axial support sleeve and the opening diameter of which is smaller than an inner diameter of the axial support sleeve so that a lateral tolerance compensation is providable by means of a combination of the axial support sleeve, the support disc and the fastening means.
4. The adjustment element according to claim 1, the hollow screw of which comprises the drive feature on an inside and/or an outside.
5. The adjustment element according to claim 4, the hollow screw of which comprises an outer polygon as the drive feature at the first axial end, which encompasses at least partly the tubular fastening opening.
6. The adjustment element according to claim 4, the hollow screw of which includes a form fit inner drive feature adjacent to the second axial end.
7. The adjustment element according to claim 1, in which the hollow screw and/or the support sleeve comprise(s) a remainder of a released and previously connecting predetermined breaking point between the support sleeve and the hollow screw.
8. The adjustment element according to claim 1, in which the hollow screw and the support sleeve are made of the same plastic material or of different plastic materials.
9. A structural component with a fastening opening to which the adjustment element according to claim 1 is fastened with a fastening means.
10. The structural component according to claim 9, wherein a component is fastened on the outer thread of the hollow screw of the adjustment element so that tolerances between the structural component and the component are settable.
11. An installation method with which an add-on part is fastenable and positionable to a structural component with the installation method comprising the following steps: a. screwing-in a hollow screw of the adjustment element according to claim 1 into a retention opening of the add-on part, b. fastening the hollow screw with add-on part to a fastening opening of the structural component with a fastening means that is arranged within the tubular fastening opening of the fastening collar, and c. rotating the hollow screw that is fastened to the structural component so that the add-on part is displaced along a longitudinal axis of the hollow screw.
12. The installation method according to claim 11, with the further step: providing the fastening opening of the structural component with a thread, the thread being configured in a matching manner to a thread bolt serving as a fastening means.
13. The installation method according to claim 11, with the further step: arranging the thread bolt in combination with a support disc in the axial support sleeve so that the hollow screw is rotatably fastened to the structural component.
14. The installation method according to claim 11, with the further step: rotating the fastened hollow screw by means of an outer or an inner drive feature in order to change the axial position of the add-on part on the hollow screw.
15. An injection molding method with which an adjustment element according to claim 1 is producible, comprising the following steps: a. providing an injection mold having the complementary mold features with respect to the adjustment element, b. injection molding the adjustment element with a first plastic material.
16. The injection molding method according to claim 15 with the further step: c. injection molding a support sleeve in the injection mold so that the hollow screw and the support sleeve are available being connected by means of a predetermined breaking point.
17. The injection molding method according to claim 16 with the further step: d. demolding the hollow screw with the support sleeve, wherein the hollow screw and the support sleeve are separated from each other at the predetermined breaking point and the support sleeve is arranged in the tubular fastening opening.
18. The injection molding method according to claim 15, wherein the injection molding method is a 1K injection molding method and the hollow screw and the support sleeve are made of the same plastic material or wherein the injection molding method is a 2K injection molding method and the hollow screw and the support sleeve are made of different plastic materials.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0046] In the following, the present disclosure will be described in detail based on the drawings. In the drawings, the same reference signs denote the same components, features and/or elements. They show:
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DETAILED DESCRIPTION
[0071]
[0072] The structural component S comprises a fastening opening B with an inner thread. According to a further embodiment, the fastening opening B may be provided by means of a blind rivet nut C with inner thread or by means of a welding nut (not shown) or by means of a thread opening directly in the structural component S.
[0073]
[0074] The structural component may be provided with a threadless opening. The adjustment element 1 can be fastened to this opening with a blind rivet, a plug connection, a bayonet connection, a locking pin or the like.
[0075] In the following, a thread bolt 90 as an exemplary fastening means is described.
[0076] The adjustment element 1 according to
[0077] The outer thread 14 may have a self-inhibiting configuration. The hollow screw 10 can thus be rotated in an opening of the add-on part A without the thread connection between the hollow screw 10 and the add-on part A releasing.
[0078] The thread connection between the hollow screw 10 and the add-on part A has the advantage that a rotating of the hollow screw 10 about its longitudinal axis L displaces the add-on part A relative with respect to the hollow screw 10 in the direction of the longitudinal axis L of the hollow screw 10. In this way, a distance Z between the add-on part A and the structural component S may be changeable and settable, as is shown in
[0079] For this purpose, the hollow screw 10 is fastened to the structural component S, may be rotatable around its longitudinal axis L. The fastening is explained in more detail further below.
[0080] The bolt 90 may be rotatably screwed together with the structural component S by means of a central thread bolt 90. The thread bolt 90 is arranged in a tubular fastening opening 16 of the hollow screw 10. An inner diameter of the fastening opening 16 is larger than an outer diameter of the shaft 92 of the thread bolt 90. Based on this geometric configuration, the hollow screw 10 may be displaceable radially relative to the shaft 92 of the thread bolt 90, before the thread bolt 90 is firmly screwed together with the structural component S (see below). If the structural part S, to which the hollow screw 10 is fastened, is considered as an x-y-fastening plane with the fastening opening B arranged in there, the hollow screw 10 is displaceable in x-y-direction on the plane of the structural component S for the purpose of tolerance compensation before the thread bolt 90 is tightened (see
[0081] Thus, beside the connecting of the add-on part A with the structural component S, the adjustment element 1 realizes a tolerance compensation in all three spatial directions x, y, z between the structural component S and the add-on part A. The adjustment possibility may guarantee in, for example, the vehicle construction the setting of desired gap sizes between a vehicle body and a vehicle lamp.
[0082] A similar embodiment of the hollow screw 10 is shown in
[0083] Furthermore, the hollow screw comprises a fastening collar 20 projecting radially to the inside at a first axial end. The fastening collar 20 may extend inside of the hollow screw 10 in an enclosed manner, thus defining a tubular fastening opening 16.
[0084] The fastening collar 20 may have an inner radially extending rim 22 and an outer radially extending rim 24.
[0085] In the installed state of the adjustment element 1, the outer rim 24 rests against the structural component S directly or adjacent to it, which may be on the retention collar of a blind rivet nut C. An axial support sleeve 40 is arranged within the tubular fastening opening 16.
[0086] The support sleeve 40 may be configured longer than an axial distance between the inner rim 22 and the outer rim 24 of the fastening collar 20. If the hollow screw 10 is fastened to the structural component S, the outer rim 24 and the adjacent axial end 44, i.e. the end 44 of the support sleeve 40 which axially faces to the outside, rest against the structural component S. Accordingly, the outer rim 24 and the end 44 are aligned in a flush manner to one another. Due to the axial length of the support sleeve 40 in comparison with a length of the tubular fastening opening 16, expressed by the axial distance of the rims 22, 24, the end 42 of the support sleeve 40 which faces to the inside projects beyond the inner rim 22.
[0087] The axially inner end 42 of the support sleeve 40 may form a ring like abutment for a support disc 50. The support disc 50 is supported on the axially inner end 42 of the support sleeve 40. For this purpose, an outer diameter of the support disc 50 may be larger than an outer diameter of the support sleeve 40, thus guaranteeing that the support disc 50 is completely supported on the support sleeve 40 so as to transfer the mechanical fastening tensions from the underside of the head of the thread bolt 90 via the support sleeve 40 into the structural component S.
[0088] The support sleeve 40 may comprise a central opening 52. The shaft 92 of the thread bolt 90 passes through the central opening 52 in order to fasten the hollow screw 10 in the fastening opening B of the structural component S.
[0089] The difference in length between the tubular fastening opening 16 and the support sleeve 40 may guarantee a distance between the inner rim 22 of the fastening collar 20 and a side of the support disc 50 which faces the inner rim 22 in the fastened state of the hollow screw 10. This distance guarantees that even when in the fastened state, i.e. when screwed together with the structural component S, the hollow screw 10 is rotatable around its longitudinal axis L.
[0090] By that, which may be in the fastened state of the hollow screw 10, the distance Z between the add-on part A and the structural component S can be changed by rotating the hollow screw 10.
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[0092] A 1K injection molding method may be used for the production of the hollow screw 10 and the support sleeve 40. The production routes which are described in the following may be applicable for both a 1K injection molding method as well as a 2K injection molding method.
[0093] According to a first manufacturing alternative, the hollow screw 10 and the support sleeve 40 according to
[0094] According to a further manufacturing alternative, the predetermined breaking point 46 may be automatically separated during demolding the arrangement according to
[0095] The support sleeve 40 within the tubular fastening opening 16 realizes a play between the support sleeve 50 and the fastening collar 20 via its length. A clamping of the hollow screw 10 due to the connection between the thread bolt 90 and the structural component S is thereby avoided.
[0096] The support sleeve 40 is retained in the fastening opening 16 which may be in a friction fit manner. Therefore, a friction between the support sleeve 40 and an inner wall of the fastening opening 16 determines a rotation resistance of the hollow screw 10 against the rotating of the hollow screw 10 around the longitudinal axis L. This rotation resistance may guarantee a set angle position of the hollow screw 10 around the longitudinal axis L. Furthermore, the rotation resistance has a stabilizing effect in terms of possible vibrations of the adjustment element 1 which could lead to a rotating of the hollow screw 10.
[0097] The friction fit between the inside of the fastening opening 16 and the radial outside of the support sleeve 40 may depend on the shape of the support sleeve 40. According to a configuration, the support sleeve 40 may be configured hollow-cylindrically (see
[0098] According to a further configuration of the support sleeve 40, the same may include a circumferential end collar 46 (see
[0099] As a further embodiment,
[0100] On a face side of the support sleeve 40 facing the support disc 50 (not shown),
[0101] According to a further configuration, the hollow screw 10 comprises a drive feature 60 at the first axial end 6 adjacent to the fastening collar 20 on the radial outside. The drive feature 60 may be a polygon, which may be a hexagon. It is arranged directly on the outside of the hollow screw 10.
[0102] According to a further constructive alternative, an axial projection 62 may be provided at the first axial end 6. It may have a smaller diameter than the hollow screw 10 in the portion of the outer thread 14. In this way, the drive feature 62 includes a radial free space which facilitates the engagement of a positive matching tool.
[0103] According to a further embodiment, the hollow screw 10 may have a radially inboard drive feature 64 at the second axial end 8. The inboard drive feature 64 may be adapted to form a form fit rotation connection with a tool 80. For this purpose, the radial inside of the circumferential wall 12 has a plurality of axially extending radially outwardly recessed grooves 66. The grooves 66 may be evenly distributed on the inner circumference of the hollow screw 10. The form-fit adapted tool 80 comprises evenly distributed axial webs 82 which engage into the grooves 66 (see
[0104] The grooves extend in axial direction starting at the second axial end 8. The end of the grooves 66 facing away from the second axial end 8 each form a radial recess in order to hold the engaging axial web 82 of the tool 80. At a certain axial depth of the grooves 66, which may be ramp slopes 68 connect adjacent grooves 66. The ramp slopes 68 reduce the radial height of the radial limiting walls of the radial recess 66. As soon as an engaging axial web 82 reaches the ramp slope 68 and leaves the lower groove 66 because the tool 80 is removed from the second axial end 8, the form fit connection between the tool 80 and the hollow screw 10 is released.
[0105] When the tool 80 is for example rotated clockwise, the hollow screw 10 is screwed into the add-on part A. Meanwhile, the add-on part A moves in the direction of the second axial end 8 and encounters the tool 80 in form of the skirt 84. The skirt 84 encompasses the axial webs 82 at a radial distance. Furthermore, the skirt 84 extends in axial direction so that it partly covers the axial webs 82.
[0106] When the hollow screw 10 is screwed into the add-on part A, the tool 80 is moved through the add-on part A by means of the skirt 84 in the direction of the second axial end 8. Due to this movement in axial direction of the hollow screw 10, the axial webs 82 are displaced from the engagement in the grooves 66 into the portion of the ramp slopes 68, causing the form fit between tool 80 and hollow screw 10 to be released. In this way, it is avoided that the hollow screw 10 can be screwed out of the engagement with the add-on part A.
[0107] A further embodiment of an inboard form fit drive feature is shown in
[0108]
[0109]
[0110] In order to facilitate the fastening of the add-on part A to the structural component S for the worker, a fastening opening B in the shape of a thread opening is provided in the structural component S. According to a first embodiment, the fastening opening B may have an inner thread at its radial inner wall. The add-on part A with adjustment element 1 and a thread bolt 90 arranged in there in a loss-proof manner having a support disc 50 may be provided for the worker. The worker then screws the thread bolt 90 into the fastening opening B and fastens the add-on part A. After that, the distance between the add-on part A and the structural component S is changed with the help of the tool 80 according to a desired clearance.
[0111] According to a further embodiment, a blind rivet nut C may be fastened in the fastening opening B. Same provides a fastening thread for the thread bolt 90. The installation method proceeds accordingly as described above, with the exception that the thread bolt 90 is screwed into the inner thread of the set blind rivet nut C (see
[0112] At the add-on part A, the preinstalled adjustment element 1 already comprises a blind rivet nut C arranged on the thread bolt 90. Therefore, the worker may arrange the add-on part A in a fitting manner in the structural component S, with the shaft 92 of the thread bolt 90 with preinstalled blind rivet nut C being inserted into the fastening opening B of the structural component S. As soon as the blind rivet nut C has been arranged in a fitting manner, the worker starts rotating the thread bolt 90 with the help of a suitable tool. The blind rivet nut C is set into the fastening opening B of the structural component by means of the rotation of the thread bolt 90 and the adjustment element 1 is fastened. After that, the worker adjusts the distance between the structural component S and the add-on part A (see
[0113] In
[0114] Firstly, the structural component S with a fastening opening B and a blind rivet nut C fastened in there is provided (step S1,
[0115] As a further preparation of the installation of the add-on part A, the hollow screw 10 or the complete adjustment element 1 may be screwed into an opening of the add-on part A (step S2a,
[0116] According to a further configuration, the add-on part A with adjustment element 1 already fastened to it may be delivered or provided (step S2b). Therefore, the worker does not have to screw the adjustment element 1, which may be the hollow screw 10, in an opening of the add-on part A.
[0117] The thread bolt 90 is or will be arranged jointly with the support disc 50 within the axial support sleeve 40 (step S3). Due to the arrangement of the support sleeve 40 between the support disc 50 and the structural component S, the hollow screw 10 is rotatably held at the structural component S even after the thread bolt 90 has been tightened (
[0118] After having arranged the thread bolt 90 in the adjustment element 1 and in the fastening opening B of the structural component S, the thread bolt 90 is screwed together with the thread of the fastening opening B and fastened with it (step S4a).
[0119] Before or during screwing tight the thread bolt 90 in the fastening opening B, the adjustment element 1 is moved in the plane of the structural component in order to compensate tolerances (see above and
[0120] The lateral tolerance compensation may be enabled as a result of the inner diameter of the support sleeve 40 being larger than the outer diameter of the shaft 92 of the thread bolt 90 which passes through the support sleeve 40 (step S4b).
[0121] Once the add-on part A has been fastened to the structural component S by means of the adjustment element 1, the hollow screw 10 is rotated with the form-fit/positively acting tool 80. With the help of the rotation of the hollow screw 10, the distance between the structural component S and the add-on part A changes (step S5).
[0122] The positively acting tool 80 may engage into the second axial end 8 of the hollow screw 10. A structure is provided there, which may be at the radial inner side of the wall 12, which guarantees a form-fit and releasable rotation connection with the tool 80 (see
[0123] The hollow screw 10 may be rotated with a tool by means of the radially outer drive feature 60 so as to set the distance suitably (step S6).
[0124] As can be seen from the sectional view in
[0125] For the sake of completeness and with reference to
[0126]
[0127] These different fastening means may all fulfil the same function as the thread bolt 90 as fastening means. The adjustment element 1 may be fastened to the structural component S by means of these fastening means, wherein a rotation of the hollow screw 10 can be realized even after fastening the hollow screw 10 to the structural component S.