专利摘要:
fixing device the present invention relates to a fixing device for joining a mounting component (30) to a support component (29), with a cover plate (2), as well as side walls (8,9), profiled on the cover plate (2) that form a u-shape. on the arms of the rods (11,12) marginal wings (21) are provided opposite each other, as well as support faces (17) supported on supporting edges. this results in a very rigid block-shaped construction of the fixing device which has high resistance against very intense extraction forces.
公开号:BR112013018361B1
申请号:R112013018361
申请日:2012-01-30
公开日:2019-12-24
发明作者:Binkert Sven
申请人:A Raymond Et Cie;
IPC主号:
专利说明:

Descriptive Report of the Invention Patent for FIXING DEVICE.
The present invention relates to a fixing device according to the preamble of claim 1.
Such a fixing device has become known from WO 2010/101803 A1. This fixing device already known for fixing a mounting component on a support component has a flattened cover plate, arranged in a top area, and two rod arms that are joined with the cover plate and extend in the direction of the moving away from the cover plate towards a base area. Each stem arm has an external wing and an internal wing, and in each inner wing of a stem arm support profiles are profiled that transfix cutouts of support faces that are shaped in the outer wing of the respective stem arm. In addition, in each external wing of each stem arm, two marginal wings are formed that project in a direction turned in relation to each other. The marginal wings are positioned between the support faces and the cover plate.
The objective of the invention is to propose a fixing device of the species initially mentioned that stands out for its very intense extraction forces and high rigidity.
In a fixation device of the species initially mentioned, this task will be solved with the striking characteristics of claim 1.
Due to the fact that on the cover plate side walls are profiled which form a U-shaped profile with the cover plate and as the outer wings extend on both sides of the free sections of the support faces, it results in a very high rigidity of the fixing device, which through various U-profiles results in intense extraction forces.
Other convenient embodiments of the invention are the subject of the dependent claims.
Other convenient configurations and advantages of the invention result from the subsequent description of examples of execution with respect to
2/9 to the figures in the drawing.
The Figures show:
Fig. 1 perspective view of an example of a fixation device according to the invention,
Fig. 2 perspective view, in partial section, showing an example of execution of Fig. 1,
Fig. 3 detail view, in perspective, of the supporting faces of the execution example of Fig. 1,
Fig. 4 seen in detail, in perspective, of the execution example according to Fig. 1 with free ends reciprocally leaning against internal wings of support faces,
Fig. 5 in perspective view the example of execution according to Fig. 1 in assembled situation,
Fig. 6 in section view of the example of execution of Fig. 1 in the assembled position according to Fig. 5,
Fig. 7 in perspective view another example of making a device according to the invention,
Fig. 8 in perspective view, in partial section, the other example of execution according to Fig. 7,
Fig. 9 detail view in perspective of the other example of execution according to Fig. 7 with adjacent central segments of internal wings of support faces,
Fig. 10 in detail perspective view corresponding to Fig. 3, showing supporting faces of another example of execution, and
Fig. 11 in perspective detail view, corresponding to Fig. 3, supporting faces of yet another example of execution.
Fig. 1 shows in perspective view an example of the execution of a fixing device according to the invention, which consists of a metal plate in a process of stamping and bending. The execution example according to Fig. 1 has, in a top area 1, a flat cover plate 2 of essentially rectangular shape. In the longitudinal direction, in the center of the cover plate 2, in the area of the sides
3/9 marginal, access cuts 3, 4 opposite. At the ends of the cover plate 2, molar arms 5, 6 are profiled on the cover plate 2 which extend from the cover plate 2 towards a base area 7 opposite from the top region 1. In the example shown, the arms molars 5, 6 are aligned transversely to the longitudinal direction of the cover plate 2 and protrude in front of the side of the cover plate 2 which faces towards the base area 7.
The side walls 8, 9 are profiled on the longitudinal edges of the cover plate 2, which are essentially aligned in a rectangular direction towards the cover plate 2 and therefore form, together with the cover plate 2, a U-shaped profile and in the top 1 area result in high rigidity. Each side wall 8, 9 is shaped with a molar arm fitting cutout 10 on one of its molar arms 5, 6, at the opposite end of one of its molar arms 5, 6, and this cutout is so dimensioned that on the occasion of an alignment with parallel molarization of a molar arm 5, 6 in the direction of the cover plate 2, this unit is positioned in positive union in the respective cutouts for molar arm 10, whereas the molar arms 5, 6 , in a relaxation arrangement according to Fig. 1, they stand out beyond the side walls 8, 9 towards the base area 7.
In the central area of the side walls 8, 9, two rod arms 11,12 are profiled, extending from the top area 1 in the direction of the base area 7, and which are reciprocally opposite, presenting an external wing 13, applied in a side wall 8, 9, externally and an internal wing 14 which through pairs of folding segments 15, arranged in the area of the base 7, segments that involve a free folding section 16, are joined with external wings 13 and between these wings external 13, in opposite position, are mounted on the inside. Due to the width of the folding segments 15, the molar properties of the inner wings 14 can be adjusted relatively easily.
A pair of support faces is profiled on each inner wing 14
4/9 that in the relaxed position shown in Fig. 1, through free sections of support faces 18, formed in the central area on the outer wings 13, extend beyond the outer wings 13 outwards. Between the free sections of the support faces 18 of an external wing 13 there remains a central thread 19 in whose alignment a reinforcement groove 20 is profiled to reinforce the corresponding external wing 13.
In addition, it can be seen from the representation according to Fig. 1 that in this example of execution, on the outer wings 13 of each stem arm 11, 12 are profiled marginal wings 21 that extend in the direction of the marginal wing 21 directly opposite the other external wing 13. The marginal wings 21 extend on both sides of the free sections of the support faces 18, extending essentially over the entire length of the external wings 13 of the stem arms 11, 12 and being located, with their marginal edges pointed one at relative to the other, according to the example of execution of Fig. 1, being positioned immediately adjacent. In this way, the outer wings 13 are blocked and stiffened in the form of a block against inward bending.
Fig. 2 shows in a longitudinal perspective section the example of execution according to Fig. 1, especially with a view to the inner wings 14. From Fig. 2 it can be seen that the inner wings 14, in extension of the free sections of folding 16, are conformed with a reinforcement groove 22 to reinforce the inner wings 14 in their area facing towards the base 7. Furthermore, it can be seen from Fig. 2 that they are joined through a curvature with the inner wings 14 with a central segment 23 approximately aligned parallel to the outer wings 13.
Each inner wing 14 furthermore has an end segment 24, opposite the cover plate 2, which segment, in relation to the central segment 23, has an oblique angular shape in the direction of the outer wing 13 away from the stem arm 11 , 12 respective. In addition, it can be seen in Fig. 2 that the end segment 24 is disposed opposite the access cutouts 3, 4, so that a tool
5/9 disassembly, not shown in Fig. 2, can transfix the access cutouts 3, 4, acting on the terminal segments 24.
Fig. 3 shows in detailed perspective a rod arm 11 of the embodiment according to Fig. 1 in the area of the support faces 17 and the free sections of the support faces 18. In fig. 3 it can be recognized with particular clarity that each support face 17 is formed by a lateral segment 25 that projects laterally in the longitudinal direction of the stem arm 11, connected to the inner wing 14, and a backrest segment 26, essentially disposed towards rectangular to the side segment 25, as well as joined through an angular section with the respective side segment 25, extending in the direction of reciprocal approximation, until close to the central thread 19. The outer edges of the side segments 25, spaced in relation to to the outer wings 13, they are chamfered in the direction of the base segment 7 in order to allow the introduction of the rod arms 11, 12 through cutouts for assembly, suitable for their cross section, using relatively reduced assembly forces.
Each abutment segment 26, on one side of the free section of the support face 18, facing towards the base area 7, is in a position directly opposite the support edge of the abutment segment 27 of the external wing 13, as an edge support, so that a folding of the backrest segments 26 towards the base area 7 is blocked. The marginal faces of the side segments 25, facing towards the base area 7, in turn, meet at the edge of the edges side segment support bracket 28 at the end facing the base region 7 of the free sections of the support faces 18, in the form of supporting edges, so that movement of the side segments 25 towards the base area 7 is also blocked In this way, flexion of the support faces 17 in the exercise of an intense extraction force on a fixing device according to the invention will be effectively avoided, in relation to the example shown and explained do, which can be done in a corresponding assembly explained in detail below.
Fig. 4 shows in perspective detail view, the example
6/9 execution point according to Fig. 1 in the area of the central segments 23 and the end segments 24 of the inner wings 14 in an end position of a flexed movement the inner wings 14 inward as, for example, occurs by a disassembly tool introduced by the access cutouts 3, 4 and acting on the terminal segments 24, a tool not shown in Fig. 4.
In this terminal position, the support faces 17 fully penetrated the free sections of the support faces 18, as well as the internal compartment, formed between the inner wings 13, so that the stem arms 11, 12, without obstacles, can be crossed by means of suitable cut-outs for the cross section of the stem arms 11, 12. By forming the end segments 24 in the form of teeth, the end segments 24 are adjacent in the end position and block further reciprocal movement of the inner wings 14 , even if intense forces are applied by the disassembly tool. In this case, the freed sections of the support faces 18, at their end facing towards the top area 1, are dimensioned in such a sufficiently large way that the resistance to an inward movement of the support faces 17, until the terminal position, according to Fig. 4.
Fig. 5 shows an example of making a fixing device according to Fig. 1 and the invention in an ordered mounting position, in which the stem arms 11, 12 are crossed by a support member 29 that can receive intense mechanical load and in an attached module 30, here in the form of an airbag set, being crossed by assembly cutouts. In the mounting arrangement, the backrest segments 26 of the support faces 17 are positioned behind the support section 29 on its side away from the attached component 30, whereas the molar arms 5, 6, as well as possibly the faces side walls 8, 9, separated from the cover plate 2, rest on the attached component 30. In this way, the attached component 30 is securely attached, but separable from the
7/9 support 29.
Fig. 6 shows in a longitudinal section the example of execution of a fixing set according to Fig. 1, according to the invention, shown in the mounting arrangement according to Fig. 5. From Fig. 6 it can be seen clearly that the marginal wings 21, always arranged on the same side as the outer wings 13, except for a relatively narrow slit, are positioned very adjacent, that is, juxtaposed, so that an offset of the outer wings 13 is blocked inwards during application of intense extraction forces. In addition, in the application of intense extraction forces, the inner wings 14 will be displaced in the direction of the outer wing 13 of its stem arm 11, 12, which reinforces the posterior positioning of the back segments 26 of the support faces 17. Also the folding segments 15, in their terminal areas bordering the inner wing 14, touch tightly together which results in a stiffening in the area of the base 7.
Fig. 7 shows in perspective view another example of execution of a fixing device according to the invention, with the example of execution according to Fig. 1 and the other example of execution according to Fig. 1 , reciprocally corresponding elements have the same reference signs and are not explained again in order to avoid repetition in part. In the other example of execution according to Fig. 7 the marginal wings 21 are formed with marginal edges that point in relation to each other and that are formed with a first partial segment 31, straight and elongated, and with a second partial segment 32 shorter and aligned in relation to the first partial segment 31, of angular alignment. The first partial segments 31 project, in this case, in the longitudinal direction of the base area 7, while the second partial segments 39 are aligned in an oblique angular direction in the longitudinal direction of the base area 7. In this way, the second partial segments 32 are pressed against each other in the application of a force directed against the direction of introduction. The applied force, by the positive union thus obtained by the second partial segments 32, will be
8/9 uniformly fitted on the two support faces 17 and, therefore, for the two stem arms 11, 12, with which one of the two stem arms 11,12 reacts to failure due to a force introduced only on one side.
Fig. 8 shows in perspective view, in partial section, the other execution example according to Fig. 7. From Fig. 8 it can be seen that in the other execution example, the back segments 26 are profiled in central segment 23 of the respective inner wing 14 of the respective stem arm 11, 12 by means of a chamfer and touch the marginal edges of the side segments 25 towards the cover plate 2. In the area of the chamfered section of the back segment 26, in the terminal sector of the central segments 23, the inner wings 14 have an access opening 33, applied in the longitudinal direction of the base area 7 in alignment with a respective access cutout 3, 4. In addition, in the other example of execution, the side segments 25, at their ends spaced from the cover plate 2, have a stop segment 34 that extends beyond the respective free section of the face of the segment 18, moving away of the cover plate 2 and with its marginal edge, it projects in a radial direction towards the outside, it is in opposite position to the respective external wing 13. In this way, a movement of the inner wings 14 and the outer wings 13 in a reciprocal direction is blocked.
Fig. 9 shows in a perspective detail view the other example of execution according to Fig. 7, in the area of the central segments 23 of the internal areas 14 in a terminal position of a flexion movement that folds the internal wings inward 14 radially, as it is produced, for example, using a disassembly tool, not shown in Fig. 9, introduced by the access cutouts 3, 4 and introduced in the access openings 33. In this terminal position, as already explained in In connection with Fig. 4, the support faces 17 have already completely penetrated the free sections of the support faces 18, as well as the internal compartment, formed between the outer wings 13. In the other example of execution, the central segments touch each other in such a way in the region of the folds in relation to the back segments 26 that block
9/9 another movement of reciprocal approach of the inner wings 14, even in the case of intense forces exerted by the assembly tool, with the folds acting in a stabilizing manner.
Fig. 10 shows, in partial partial perspective view, corresponding to Fig. 3, support faces 17 of another example of execution, and in the examples of execution according to Fig. 3 and Fig. 10, elements that are reciprocally corresponding have identical reference signs and then partly are not explained again in detail. In the other example of execution according to Fig. 10, each support face 17 has a connecting wing 35 profiled on the central segment 23, and located internally and adjacent to the central thread 19, as well as having a terminal wing 37 that through a connecting segment 36 is in contact with the connecting wing 35. The connecting thread 36 protrudes beyond the outer wing 13 towards the outside and is chamfered to facilitate assembly in the direction of the base area 7. The end wings 37 are positioned on the side of the respective connecting wing 35, away from the central thread 19, and are aligned in parallel with the respective connecting wing 35, and for contact with the supporting edges of the side segments 28 they penetrate the free sections of the support faces 18.
Fig. 11 shows a detail and perspective view, corresponding to Fig. 3, support faces 17 from yet another example of execution, and in the examples of execution according to Fig. 3, Fig. 10 and Fig. 11 elements that correspond to each other have the same reference signs and in part, additionally do not need to be explained in detail again. In yet another example of execution according to Fig. 11, in modification with the other example of execution according to Fig. 10, in each support face 17 the connecting segments 36 are located on the side of the connecting wing 35 facing in the direction from the top 1, being aligned in a rectangular shape with the outer wings 13, while to facilitate the assembly the sides facing the outside of the connecting wing 35 and the terminal wing 37 are chamfered towards the base area 7.
权利要求:
Claims (17)
[1]
1. Fixing device for fixing a mounting component (30) to a support component (29), with a flat cover plate (2), arranged in a top area (1), and with two rod arms (11 , 12) which are joined with the cover plate (2) and extend from the cover plate (2) in the direction away from a base area (7), with each stem arm (11, 12) comprises an outer wing (13) and an inner wing (14), with each inner wing (14) of a stem arm (11, 12) bearing faces (17) provided by free sections of bearing faces (18) conformed to the external wing (13) of the respective stem arm (11, 12), and in each external wing (13) of each stem arm (11.12) two marginal wings (21) are profiled extend in the direction of reciprocal approximation, characterized by the fact that, on the cover plate (2) side walls (8, 90) are profiled which form a U-profile with the cover plate ra (2) being that each external wing (3) is profiled on a side wall (8, 9) and the marginal wings (21) extend on both sides of the free sections of the support faces (18).
[2]
2. Fixing device according to claim 1, characterized by the fact that the marginal faces facing each other in relation to the marginal wings (21) are rectilinear and adjacent.
[3]
3. Fixing device, according to claim 1, characterized by the fact that the marginal faces of the marginal wings (21), facing each other, have two partial segments (31, 32) straight and aligned in a reciprocal angular direction , being adjacent.
[4]
Fixing device according to any one of claims 1 to 3, characterized in that the supporting faces (17) are shaped in L with a back segment (26), aligned in parallel with the backing plate.
Petition 870190088437, of 06/09/2019, p. 7/9
2/3 cover (2) and with a side segment (25) aligned in a rectangular direction towards the back segment (26).
[5]
5. Fixing device according to claim 4, characterized by the fact that each backrest segment (26) is chamfered to a side segment (25).
[6]
6. Fixing device according to claim 4, characterized by the fact that each backrest segment (26) is chamfered in a central segment (23) of an internal wing (14).
[7]
Fixing device according to any one of claims 4 to
6, characterized by the fact that the side segments (25), on the side opposite the backrest segment (26), have a stop segment (34) opposite the external wing (13).
[8]
Fixing device according to any one of claims 4 to
7, characterized by the fact that each external wing (13) has support edges (27, 28) that are opposite the back segments (26) and the side segments (25) on its opposite side in relation to the cover plate (2).
[9]
Fixing device according to any one of claims 1 to
3, characterized by the fact that each support section (17) has a joining wing (35), profiled on a central segment (23), as well as a terminal wing (3), joined, through a joining segment ( 36), with the connecting wing (35), the connecting wing (35) and the terminal wing (37) of each support face (17) being reciprocally aligned in parallel.
[10]
10. Fixing device, according to claim 9, characterized by the fact that the joining segment (36) projects outwards from the respective external wing (13), being aligned obliquely in the direction of the base area (7 ).
[11]
Fixing device according to claim 9, characterized by
Petition 870190088437, of 06/09/2019, p. 8/9
3/3
I the fact that the joining segment (36) projects towards the top area (1) being aligned in a rectangular direction towards the outer wings (13).
[12]
Fixing device according to any one of claims 1 to 11, characterized in that the cover plate (2), extending obliquely from the cover plate (2), molar arms (5, 6) are profiled that extend towards the base area (7).
[13]
13. Fixing device according to any one of claims 1 to 12, characterized by the fact that each internal wing (14), at its end facing the cover plate (2), has an end segment (24) which is disposed in the opposite position of an access cutout (3, 4) conformed to the cover plate (2).
[14]
14. Fixing device according to claim 13, characterized in that the end segments (24) of the inner wings (14) reciprocally touch in a terminal position, blocking another movement of the inner wings (14) in the direction of reciprocal approximation.
[15]
Fixing device according to any one of claims 1 to 12, characterized in that at least one inlet opening (33) is formed in each internal wing (14), and in opposition to this opening, an opening is provided access cutout (3, 4) formed into a cover plate (2).
[16]
16. Fixing device according to any one of claims 1 to 15, characterized in that the outer wings (13) and / or the inner wings (14) have reinforcing grooves (20, 22).
[17]
17. Fixing device according to any one of claims 1 to 16, characterized by the fact that, between the outer wing (13) and the inner wing (14) of a rod arm (11,12), two segments are formed folding section (15) between which a fold-free section (16) is formed.
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同族专利:
公开号 | 公开日
WO2012104250A1|2012-08-09|
CN103348145A|2013-10-09|
CN103348145B|2016-01-06|
ES2557566T3|2016-01-27|
JP2014505845A|2014-03-06|
US9009928B2|2015-04-21|
BR112013018361A2|2016-10-04|
JP5662589B2|2015-02-04|
DE202011101112U1|2012-08-28|
EP2670988B1|2015-10-07|
PL2670988T3|2016-03-31|
HK1186230A1|2014-03-07|
EP2670988A1|2013-12-11|
US20130302087A1|2013-11-14|
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法律状态:
2018-12-18| B06F| Objections, documents and/or translations needed after an examination request according art. 34 industrial property law|
2019-07-09| B06T| Formal requirements before examination|
2019-11-05| B09A| Decision: intention to grant|
2019-12-24| B16A| Patent or certificate of addition of invention granted|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/01/2012, OBSERVADAS AS CONDICOES LEGAIS. |
优先权:
申请号 | 申请日 | 专利标题
DE102011010141A|DE102011010141A1|2011-02-02|2011-02-02|Fastening device for connecting attachment unit to support unit in airbag assembly, has inner wing and outer wing that are provided in two shaft arms that are connected to the cover plate|
DE201120101112|DE202011101112U1|2011-02-02|2011-05-26|fastening device|
PCT/EP2012/051445|WO2012104250A1|2011-02-02|2012-01-30|Fastening device|
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