Instrument Panel Support For A Motor Vehicle
20220281532 · 2022-09-08
Inventors
Cpc classification
B62D25/145
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
An instrument panel support 1 is used for installation between the two A-pillars 2, 2.1 of a motor vehicle. The instrument panel support 1 comprises a cross-member 3 which extends between the A pillars 2, 2.1 and which has at least one connecting element 4, 4.1 on each of its two ends for connecting the instrument panel support 1 to the vehicle by means of screw fasteners 10. The connecting members 4, 4.1 have a U-shaped main body 6 connected to the cross member 3, its longitudinal axis aligned in the z-direction, with at least one support insert extending between the two wings 7, 7.1 and penetrated by a fastener 10, for connecting the instrument panel support 1 on the vehicle side. The opening side of the main body 6 points in the transverse direction to the longitudinal extent of the cross-member 3. The support insert and the wing 8 of the main body 6 have fastening apertures aligned with one another at least in regions for the purpose of passing through the shank of a fastener 10.
Claims
1. An instrument panel support for a motor vehicle to be installed between the two A-pillars (2, 2.1), the instrument panel support (1) comprising a cross-member (3) which extends between the A-pillars (2, 2.1) and which, at each of its two ends, supports at least one connecting member (4, 4.1-4.7) for connecting the instrument panel support (1) on the vehicle side by means of screw fasteners (10), wherein the connecting members (4, 4.1-4.7) have a U-shaped main body (6, 6.1-6.5) connected to the cross member (3), its longitudinal axis aligned in the z-direction, with at least one support insert (9, 9.1-9.3) extending between the two wings (7, 7.1; 7.2-7.5) and penetrated by a fastener (10), for example a screw fastener for connecting the instrument panel support (1) on the vehicle side, the opening side of the main body (6, 6.1-6.5) points in the transverse direction to the longitudinal extent of the cross-member (3), and the support insert (9, 9.1-9.3) and the spine (8, 8.1-8.4) of the main body (6, 6.1-6.5) have fastening apertures (13, 14, 13.1, 14.1) aligned with one another at least in regions for the purpose of passing through the shank of a fastener (10).
2. The instrument panel support of claim 1, characterized in that the opening side of the main bodies (6, 6.1-6.5) of the connecting members (4, 4.1-4.7) points in the direction of the respective B-pillar of the vehicle.
3. The instrument panel support of claim 1 or 2, characterized in that the wings (7, 7.1; 7.2-7.5) of the main bodies (6, 6.1-6.5) formed on the spines (8, 8.1-8.4) have a different outline geometry, in particular in connection to a different wing surface.
4. The instrument panel support of claim 3, characterized in that one wing (7.1) of the main body (6) extends with essentially constant wing height over the entire length of the main body (6), while the other wing (7) has a reduced wing height in the longitudinal extent of the main body (6) adjacent to the support inserts (9, 9.1).
5. The instrument panel support of any one of claims 1 to 4, characterized in that an extension tab (16, 16.1, 16.2) having a connecting point (15.1, 15.3) is molded on the spine (8.4) of the connecting member (4.2, 4.3, 4.7).
6. The instrument panel support of claim 5, characterized in that the extension tab (16, 16.1, 16.2) is folded with respect to the plane of the spine (8.4) of the connecting member (4.2, 4.3, 4.7), in particular in the direction of its two wings.
7. The instrument panel support of claim 6, characterized in that the extension tab (16.2) is additionally connected to at least one of the two wings (7.5).
8. The instrument panel support of any one of claims 1 to 7, characterized in that the support inserts (9, 9.1-9.3) have a U-shaped cross-sectional geometry and face with their opening side towards the spine (8, 8.1-8.3) of the main body (9, 9.1-9.3).
9. The instrument panel support of claim 8, characterized in that flanges (12, 12.1) are molded on the free ends of the wings of the support inserts (9, 9.1), which are folded with respect thereto in directions pointing away from each other.
10. The instrument panel support of any one of claims 1 to 9, characterized in that the support inserts (9, 9.1-9.3) are connected to the respective main body (6, 6.1-6.5) with material fit.
11. The instrument panel support of any one of claims 1 to 10, characterized in that at least two support inserts (9, 9.1-9.3) are arranged in one main body (6, 6.1-6.5).
12. The instrument panel support of claim 11, characterized in that the at least two support inserts (9.2, 9.3) are provided by a single insert part (17) in which the two support inserts (9.2, 9.3) are formed.
13. The instrument panel support of claim 11 or 12, characterized in that the main body of at least one of the two connecting members (4.6) in the region of the two support inserts has a spine section with a different spine width in each case.
14. The instrument panel support of any one of claims 11 to 13, characterized in that the main body of at least one of the two connecting members (4.6) has a cranked portion (19) located between the two support inserts, by means of which the planes of the spine sections adjacent to the cranked portion (19) are offset from one another.
Description
[0020] In the following, the invention is described by means of embodiments with reference to the accompanying figures. In particular:
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032] The connecting member 4 comprises a U-shaped main body, the two wings 7, 7.1 of which are oriented away from the terminal connector 5. Thus, the opening side of the main body 6 is directed towards the B-pillar of the vehicle. The outer side of the spine 8 of the connecting member 4 rests against the outer side of one wing 7.1 of the terminal connector 5 facing towards the spine 8. Support inserts 9 are inserted in the main body 6. In
[0033] The connecting member 4.1 located on the other side of the cross-member 3 has an identical design. Thus, the above explanations regarding the connecting member 4 also apply to the connecting member 4.1. Identical parts can be used for connecting members 4.4.1.
[0034] The connecting members 4, 4.1 are illustrated schematically in
[0035] In the illustrated exemplary embodiment, the support insert 9 (identical in structure to the support insert 9.1) is a section of a profile with a hat-shaped cross-sectional geometry, the open side of which faces the inside of the spine 8. Flanges 12, 12.1 angled with respect to the wings of the U-structure of the support insert 9 serve as a contact surface on the inside of the spine 8. The flanges 12, 12.1 are welded to the spine 8 of the main body 6, for example by spot welds.
[0036] The cross-member 3 is connected to the outer side 13 (see
[0037] The outline geometry of the wing 7 differs from that of the wing 7.1, in that wing 7 has the same wing height as the wing 7.1 only in the sections in which the support inserts 9, 9.1 are located. In the other sections, the height of the wing 7 is reduced, namely by about 80%. In order to be able to connect the support inserts 9, 9.1 also with respect to their wings on the inside of the wing 7 with a fillet weld, the length of the wing sections with the greater height of the wing 7 is somewhat greater than the extension of the support inserts 9, 9.1 in this respect. Due to the special design of the wing 7 of the main body 2, the connecting member 4 is weight-optimized. An aperture 13, 13.1 is made in the spine of the support inserts 9 forming the upper side 11, as well as at a complementary point in the spine 8 of the main body 2, so that a screw fastener 10 can pass through the connecting member 4 in the x-direction.
[0038] The left-hand end section of the instrument panel support 1 according to
[0039] The terminal connector 5 may be such an angle piece as is shown schematically in
[0040]
[0041] The connecting member 4.3 shown in
[0042]
[0043]
[0044] Yet another design of a connecting member 4.6 is shown in
[0045]
[0046] The description of the exemplary embodiments makes it clear that, due to the clever arrangement of the respective connecting member in the connection arrangement between the cross-member and a vehicle-side contact, which in the exemplary embodiments illustrated is provided by the terminal connector, there is a wide range of possibilities for providing additional connecting points by changing the geometry of the wings. The examples described above represent only a few of a large number of possible embodiments. This also means that the portions of a wing supporting a connecting point may also be embossed, whether by beads for stiffening or by angled portions or embossments or the like. Just as this is shown with reference to the extension tab 16 of the spine 8 in the exemplary embodiment of
[0047] The invention has been described with reference to exemplary embodiments. Without departing from the scope of the applicable claims, there are numerous further ways for a person skilled in the art to realize the invention without this having to be described in more detail within the scope of the present embodiments.
REFERENCE NUMERALS
[0048] 1 instrument panel support [0049] 2, 2.1 A-pillar [0050] 3 cross-member [0051] 4, 4.1-4.7 connecting member [0052] 5, 5.1 terminal connector [0053] 6, 6.1-6.5 main body [0054] 7, 7.1-7.5 wing [0055] 8, 8.1-8.4 spine [0056] 9, 9.1-9.3 support insert [0057] 10 screw fastener [0058] 11 top [0059] 12, 12.1 flange [0060] 13, 13.1 aperture [0061] 14, 14.1 aperture [0062] 15, 15.1, 15.3 connecting point [0063] 16, 16.1, 16.2 extension tab [0064] 17 support insert part [0065] 18 connecting bar [0066] 19 cranked portion [0067] 20 punched-out portion