RUN FLAT DEVICE
20230096527 · 2023-03-30
Inventors
- Marie PAGES (CONFLANS STE HONORINE, FR)
- Vincent JOSEPH (MONTARGIS, FR)
- Etienne BRETON (ESCALQUENS, FR)
Cpc classification
B60C17/041
PERFORMING OPERATIONS; TRANSPORTING
B60C15/0209
PERFORMING OPERATIONS; TRANSPORTING
B60C17/04
PERFORMING OPERATIONS; TRANSPORTING
International classification
B60C15/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A run flat device intended to be mounted in a tyre around a wheel rim of a vehicle, the device comprising at least one assembly of two half-shells assembled axially, each half-shell being made of a composite material based on fibres embedded in a thermoplastic or thermosetting resin, each half-shell comprising a radially internal periphery a radially external periphery and a lateral wall connecting the radially internal periphery to the radially external periphery configured so as to form an internal recess within the at least one assembly and each half-shell further comprising a plurality of circumferentially distributed anti-compression ribs extending, within the internal recess, radially from the radially external periphery towards the radially internal periphery.
Claims
1. A run flat device intended to be mounted in a tyre around a wheel rim of a vehicle, the device comprising at least one assembly of two half-shells assembled axially, each half-shell being made of a composite material based on fibres embedded in a thermoplastic or thermosetting resin, each half-shell comprising a radially internal periphery a radially external periphery and a lateral wall connecting the radially internal periphery to the radially external periphery configured so as to form an internal recess within said at least one assembly and each half-shell further comprising a plurality of circumferentially distributed anti-compression ribs extending, within the internal recess, radially from the radially external periphery towards the radially internal periphery.
2. The device according to claim 1, wherein each anti-compression rib comprises a hollow cylinder passing axially through it, suitable for receiving a means of attachment between the two half-shells.
3. The device (10) according to of claim 1 wherein each half-shell comprises centring means complementary to centring means of the other half-shell.
4. The device according to claim 3, wherein said complementary centring means are formed by pins and hollows configured to cooperate with the pins and the hollows of the other half-shell, said pins and said hollows being distributed on and/or between the anti-compression ribs of each half-shell.
5. The device according to claim 3, wherein said complementary centring means are formed by lips and grooves configured to cooperate with the lips and the grooves of the other half-shell, said lips and said grooves being located in circumferential alternation at one end of the radially external periphery of each half-shell.
6. The device according to claim 1, wherein each half-shell comprises fins extending radially from the radially external periphery towards the radially internal periphery, said fins being circumferentially distributed between the anti-compression ribs.
7. The device of claim 6, wherein at least one fin is located between two anti-compression ribs.
8. The device according to claims 6, wherein the fins of a half-shell form closed or open partitions in their centre with the corresponding fins of the other half-shell.
9. The device according to claim 1, wherein each half-shell comprises at the level of its radially internal periphery a plurality of buttresses.
10. The device according to claim 1, comprising a plurality of assemblies of two half-shells, said assemblies being attached to each other.
11. The device according to claim 10, wherein each half-shell comprises at each of its ends an attachment through orifice so that each assembly is attached to the adjacent assembly by an attachment system with cotter pin.
12. The device according to claim 1, wherein each half-shell comprises a frustoconical surface extending circumferentially from the radially internal periphery towards the radially external periphery over at least one portion of the lateral wall, said frustoconical surface being designed to ensure a positioning of a wedge between said half-shell and a bead of a tyre so that said bead of the tyre is locked against the rim of the wheel.
Description
BRIEF DESCRIPTION OF THE FIGURES
[0024] The invention will be better understood with the aid of the following description, given only by way of example and made with reference to the attached drawings in which:
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[0036]
DETAILED DESCRIPTION OF THE INVENTION
[0037] In the following, reference is made to a run flat device 10 intended to be mounted around a wheel rim 1 of a vehicle, and in particular a wheel equipped with a tyre 2.
[0038]
[0039]
[0040] Each of these half-shells 100 is made of a composite material based on fibres embedded in a resin. It should be understood that the term “fibres” can refer to short fibres, i.e. strictly less than 10 millimetres in size. In particular, this allows to limit the propagation of cracks in the half-shells 100. This term can also refer to long fibres, i.e. greater than or equal to 10 millimetres. In particular, this allows to improve the mechanical strength. More generally, it is also possible that the fibres are continuous fibres. It should be noted that it is possible to use a mixture of these two types of fibres in a same part so as to achieve a hybrid technical effect.
[0041] The size of the fibres is therefore chosen in such a way as to find a compromise between the above characteristics.
[0042] The fibres can be, for example, but not limited to, glass or carbon fibres. The resin may be thermoplastic or thermosetting and may for example, but not limited to, be polyepoxide, vinylester, phenolic or polyester.
[0043] Each half-shell 100 further comprises a plurality of anti-compression ribs 108. These anti-compression ribs 108 are circumferentially distributed and extend radially from the radially external periphery 104 towards the radially internal periphery 102.
[0044] The cross-section of each half-shell 100 may, for example, be generally U-shaped, W-shaped, Ω-shaped or the like, so that when axially assembled two half-shells 100 define an internal recess 110 within which the ribs 108 are located. This recess 110 helps to lighten the half-shell 100 and therefore the run flat device 10.
[0045] The anti-compression ribs 108 allow the assembly 20 and the run flat device 10 to be reinforced once the half-shells 100 are assembled. These ribs 108 also allow the load applied to the radially external periphery 104 to be transmitted towards the rim 1. These ribs 108 may each comprise a hollow cylinder 112 passing axially through, suitable for receiving a means of attachment between the two half-shells 100.
[0046] Each half-shell 100 may comprise circumferential ends 114 at the level of which may be located an additional hollow cylinder 112a axially passing through, suitable for receiving a means of attachment between the two half-shells 100. At the level of its circumferential ends 114 there may also be an axially through orifice 116 through which a cotter pin 31 of the attachment system 30 is intended to pass.
[0047] Each half-shell 100 may comprise centring means 118 complementary to centring means 118 of another half-shell 100.
[0048] In the example of
[0049] In one embodiment, not shown, the centring means 118 are formed by alternately distributed pins and hollows in the ribs 108. The pins 120 and the hollows 121 of one half-shell 100 are configured to cooperate with the hollows 121 and the pins 120 of the other half-shell 100. In such a configuration, each half-shell 100 comprises a single rib 108 or an even number of ribs 108.
[0050] Each half-shell 100 may also comprise fins 122 extending radially from the radially external periphery 104 towards the radially internal periphery 102. The fins 122 are distributed circumferentially between the ribs 108. In the example of
[0051] The fins 122 may have, but are not limited to, a generally triangular or rectangular shape. In use, the fins 122 of one half-shell 100 form partitions with the corresponding fins 122 of the other half-shell 100. These partitions provide radial rigidity to the assembly 20. These partitions can be open or closed in the centre, depending on the rigidity required.
[0052] The fins 122 are oriented in the same way as the ribs 108 and improve the mechanical strength of the device 10 once it is assembled, in particular by reinforcing its compressive strength.
[0053] It is understood that the alternating ribs 108 and fins 122 form a repeating pattern. In the example shown in
[0054] Each half-shell 100 may comprise, at the level of its radially internal periphery 102, a plurality of anti-bending buttresses 124. These anti-bending buttresses 124 are circumferentially distributed and extend radially from the radially internal periphery 102 towards the radially external periphery 104. The buttresses 124 may be located in the extension of the ribs 108.
[0055] Advantageously, each half-shell 100 also comprises a frustoconical surface 126, The frustoconical surface 126 extends circumferentially from the radially internal periphery 102 towards the radially external periphery 104 over at least on portion of the lateral wall 106. This frustoconical surface 126 is designed to allow the positioning of a wedge 3, shown in
[0056]
[0057]
[0058] Each rib 108 of a half-shell 200 may comprise an axially through hollow cylinder 112, similar to that described above, suitable for receiving an attachment means between two half-shells 200.
[0059] Each half-shell 200 may comprise centring means 118 complementary to centring means 118 of another half-shell 200.
[0060] In the example of
[0061] In other words, only the hollow cylinders 112 are located on the ribs 108.
[0062] Each half-shell 200 may comprise fins 122 extending radially from the radially external periphery 104 towards the radially internal periphery 104. The fins 122 are distributed circumferentially between the ribs 108. In the example of
[0063] Each half-shell 200 may comprise, at the level of its radially internal periphery 102, a plurality of anti-bending buttresses 124. These anti-bending buttresses 124 are circumferentially distributed and extend radially from the radially internal periphery 102 towards the radially external periphery 104. A buttress 124 may be interposed between a fin 122 and a rib 108 or between two fins 122.
[0064] In the example of
[0065] In addition, each of the half-shells 100, 200 described above may be monobloc. Ribs 108, centring means 118, fins 122 and buttresses 124 are came from matter with the half-shell 100, 200.
[0066] The half-shells 100, 200 of the run flat device 10 can be removed and replaced.
[0067] It is clear that the run flat device according to the invention allows for a combination of lightness and strength. In particular, these characteristics allow to reduce the total mass of the run flat device, and therefore of the vehicle intended to be equipped with it, while maintaining the mechanical performance related to compression and the bending.
[0068] Another advantage is the improved maintenance of the device when it comprises removable and interchangeable half-shells, it is possible to replace only the damaged half-shell with a new one, without having to replace the whole device. In this way, savings can be made.
[0069] Furthermore, the manufacture of the half-shells 100, 200 is simplified when each half-shell 100, 200 is a single part monobloc. The half-shell 100, 200 can be manufactured by thermocompression. In such a manufacturing method, the material making up the half-shell 100, 200, i.e. the fibres embedded in the resin, is heated and shaped using a mould and a counter-mould. The shaping of the half-shell 100, 200 during the thermocompression method follows a temperature cycle, an example of which is shown in
[0070] In a step 310, during a preheating phase, the material is preheated from t0 to t1, in the mould or out of the mould; t1 corresponding to the time required to reach a setpoint temperature, noted Tc. This setpoint temperature Tc is also referred to as baking temperature.
[0071] In a step 320, during a baking phase, the material is baked in its mould at the baking temperature Tc. This temperature Tc is specific to each type of resin. For a given resin, the temperature Tc may be, for example, 150° C. The baking of the material at temperature Tc takes place from t1 to t2 and this baking time also varies depending on the resin, for example 60 minutes for a given resin.
[0072] In a step 330, during a cooling phase, the mould containing the shaped material of a half-shell 100, 200 cools from t2 to reach a demoulding temperature, at which the half-shell 100, 200 can be demoulded.