RETRACTABLE AERODYNAMIC UNDERBODY FLAP WITH FORCE ABSORPTION BY THE LOWER SUPPORT

Abstract

A motor vehicle comprising an aerodynamic underbody flap (1) rotating about a transverse axis (10) and a lower transverse structure (4) arranged at the rear of the lower part of a front bumper (6). The rear part of the lower transverse structure (4) comprises guide means (41, 42) which, in the event of a frontal impact, guide the backward movement of the lower transverse structure (4) such that the rear face of the lower transverse structure (4) comes into contact with the axis (10) of the aerodynamic underbody flap (1).

Claims

1. Motor vehicle comprising an aerodynamic underbody flap (1) rotating about a transverse axis (10) and a lower transverse structure (4) arranged at the rear of the lower part of a front bumper (6) characterized in that the rear part of the lower transverse structure (4) comprises guide means (41, 42) which, in the event of a frontal impact, guide the backward movement of the lower transverse structure (4) such that the rear face of the lower transverse structure (4) comes into contact with the axis (10) of the aerodynamic underbody flap (1).

2. Motor vehicle according to claim 1, wherein the axis of rotation (10) of the aerodynamic underbody flap (1) is mounted on bearings fixed onto the lower part of a frame (5) of a technical front face.

3. Motor vehicle according to claim 2, wherein the frame (5) of the technical front face is fixed onto the rear part of an upper transverse structure (3).

4. Motor vehicle according to claim 3, wherein the upper transverse structure (3) is fixed onto the front end of longitudinal side members (2) by means of crash boxes (30).

5. Motor vehicle according to claim 3 or claim 4, wherein the frame (5) of the technical front face is arranged at a distance of more than 100 mm from the front end of said longitudinal side members (2).

6. Motor vehicle according to claim 2, wherein the frame (5) of the technical front face is fixed directly onto the longitudinal side members (2).

7. Motor vehicle according to any of the preceding claims, wherein the guide means (41, 42) are formed by one or more upper clamps (41) and by one or more lower clamps (42) extending the lower structure respectively above and below the axis (10) of the aerodynamic underbody flap (1).

8. Motor vehicle according to claim 7, wherein the aerodynamic underbody flap (1) has windows (12) arranged near the axis (10) to allow the passage of the lower clamps through the flap (1) when said aerodynamic underbody structure (1) is in the open position.

9. Motor vehicle according to claim 7 or claim 8, wherein the lower clamps (42) and the upper clamps (41) are arranged transversely and alternately.

10. Motor vehicle according to any of claims 7 to 9, wherein the lower clamps (42) and the upper clamps (41) extend around the rear part of the axis (10) of the aerodynamic underbody flap (1).

11. Motor vehicle according to any of the preceding claims, wherein the aerodynamic underbody flap (1) is made using a thermoplastic material.

12. Motor vehicle according to claim 11, wherein the axis (10) of the aerodynamic underbody flap comprises an inserted reinforcement piece (13) in the form of a rod made of metal or a composite material around which is molded the thermoplastic part forming the aerodynamic underbody flap (1).

Description

[0027] A clearer understanding of the invention will emerge from the accompanying Figures, which are provided by way of example and are in no way limiting, wherein:

[0028] FIG. 1 is a schematic perspective representation of the front part of a vehicle.

[0029] FIG. 2 is a schematic cross-sectional view in a plane perpendicular to the transverse direction of the device covered by the present invention.

[0030] FIG. 3 is a schematic cross-sectional view in a plane perpendicular to the transverse direction of an alternative embodiment of the invention.

[0031] FIG. 4 is a schematic perspective view of the aerodynamic underbody structure.

[0032] FIG. 5 is a schematic perspective view of a first embodiment of the guide means of the lower transverse structure.

[0033] FIG. 6 is a schematic perspective view of a second embodiment of the guide means of the lower transverse structure.

[0034] In what follows, in the orthonormal coordinates OXYZ, direction OX, oriented in the forward direction of the vehicle, is called the longitudinal direction, direction OY, oriented in the transverse direction of the vehicle, is called the transverse direction, and direction OZ, oriented from bottom to top, is called the vertical direction.

[0035] FIG. 1 shows the main structural elements of the front part of a vehicle.

[0036] An upper curved transverse beam 3, commonly called the upper transverse structure, is mounted by means of two crash boxes 30 to the front end of two side members 2 oriented in the longitudinal direction of the vehicle.

[0037] The bumper 6, shown by a dotted line, is fixed to the front of the upper transverse structure 3.

[0038] The lower part of the bumper 6 conceals a transverse beam 4, commonly called the lower transverse structure. As previously mentioned, this lower transverse structure 4 serves to reinforce the lower part of the bumper 6 and to limit its deformation in the event of an impact at low speed.

[0039] FIG. 2 shows the case in which the vehicle comprises an aerodynamic underbody flap 1 rotating about a transverse axis 10 between a closed position and an open position (shown by dotted lines). The axis 10 of the aerodynamic underbody flap 1 is supported by bearings 11 mounted on the frame 5 (shown by dotted lines) of the technical front face, the elements of which, such as a condenser, guide means, a radiator or a horn, have not been shown in the interests of clarity.

[0040] The bearings 11 are usually arranged at the two lateral ends of the aerodynamic underbody flap 1. The aerodynamic underbody flap as well as the axis 10 are made, for example, of a thermoplastic material. In order to prevent the deformation of the flap 1 under the effects of dynamic forces, it may be necessary to reinforce the axis 10 with the aid of a transverse insert 13 in the form of a rod made of metal or a composite material around which is molded the thermoplastic part forming the flap itself.

[0041] The lower transverse structure 4 is fixed onto the lower part of the bumper 6. It will be observed here that the fixing elements of the lower transverse structure are independent of those of the fixing of axis 10, so that the lower transverse structure must travel a certain distance, in the order of several millimeters, before coming into contact with the axis 10 of the aerodynamic underbody flap 1. This arrangement avoids interfering with the rotational movement of the aerodynamic flap and provides the operators working on the assembly lines with easy access to the fixing elements.

[0042] The guide means are formed by upper 41 and lower 42 clamps projecting towards the rear of the lower transverse structure 4 and designed to surround the upper part and the lower part of the axis 10 of the aerodynamic underbody flap 1 so that in its backward movement, the rear part of the lower transverse structure 4 comes into contact with the front part of the axis 10.

[0043] FIG. 2 also shows the case in which the frame 5 of the technical front face is arranged at a distance d, in front of the side members 2.

[0044] This arrangement has the advantage of bringing the aerodynamic underbody flap 1 forwards closer to the bumper and the front of the vehicle, and of improving the aerodynamic efficiency of the vehicle. It also enables a shorter lower transverse structure that occupies less space to be fitted.

[0045] Ideally, this distance d is greater than about one hundred millimeters, measured between two vertical planes perpendicular to the OX axis and passing through the front end part of the technical front face and through the front end of the longitudinal side members 2 respectively.

[0046] The frame 5 of the technical front face can then be fixed onto the rear part of the upper ansverse structure 3 or onto the crash box 30, as desired.

[0047] In the event of a frontal impact that may cause the deformation of the box 30, the frame 5 of the technical front face also moves backwards thus preventing damage to the elements that it supports.

[0048] FIG. 3 illustrates the case, less favorable from an aerodynamic point of view, in which the frame 5 of the technical front face is fixed directly onto the front of the side members 2. The lower transverse structure must then be longer or, as illustrated, must have extended clamps and a greater backward travel in order to delay the deformation of the box 30.

[0049] FIG. 4 shows in greater detail the aerodynamic underbody flap 1, wherein the windows 12 are made in the part of the aerodynamic underbody flap located near the axis 10. These windows 12 serve to allow the passage of the lower clamps 42 when the aerodynamic underbody flap 1 rotates from the dosed position to the open position.

[0050] FIG. 5 shows in greater detail the rear part of the lower transverse structure 4 on which the upper clamps 41 and the lower clamps 42 are installed. It will be observed that the upper and lower clamps are not placed opposite one another and are arranged transversely in alternating order.

[0051] In this first embodiment, the clamps 41 and 42 are designed to position themselves around only the front part of the axis 10. This first embodiment enables easier demolding of the lower transverse structure 4 when the latter is made of injected thermoplastic.

[0052] In a second embodiment, shown in FIG. 6, the clamps 41 and 42 extend around the rear part of the axis 10. Although more complicated to achieve by molding, this second embodiment enables absorption by the lower transverse structure of the longitudinal forces to which the axis 10 is subjected when the flap 1 is in the open position and must oppose the deformations of the axis or flap generated by aerodynamic forces when the vehicle is travelling at high speed. This arrangement also enables a reduction in the rigidity of the axis of the aerodynamic underbody flap 1 so that, when the aerodynamic underbody flap 1 is in the open position, said axis 10 can deform slightly in order to come into contact with the front internal part of the lower and upper clamps.

[0053] As can be seen, the forms of cooperation between the axis 10 of the aerodynamic underbody flap 1 and the lower transverse structure 4, the mechanical resistance of which is added in the case of deformation of one or other of these elements, optimize the resistance of the vehicle under the action of a frontal impact, or under the action of aerodynamic pressure when the vehicle is travelling at high speed.

[0054] This is made possible by the presence of guide means that guide the backward movement of the lower transverse structure 4,

[0055] Also, the different embodiments of the invention described above can be subject to numerous variations without departing from the scope of the invention.

NOMENCLATURE

[0056] 1 Aerodynamic underbody flap

[0057] 10 Axis of the aerodynamic underbody flap

[0058] 11 Bearing of the axis of the aerodynamic underbody flap

[0059] 12 Window

[0060] 13 Insert to reinforce the axis of the underbody aerodynamic flap

[0061] 2 Longitudinal side member.

[0062] 3 Upper transverse structure

[0063] 30 Crash box

[0064] 31 Fixing bolts

[0065] 4 Lower transverse structure

[0066] 41 Upper clamp

[0067] 42 Lower clamp

[0068] 5 Frame of the technical ront face

[0069] 6 Bumper

[0070] P Cross-section

[0071] d Distance between the front end part of the frame of the technical front face and the front of the longitudinal side member