Methods and systems for forming a dual layer housing
US-9387612-B2 · Jul 12, 2016 · US
US10427340B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10427340-B2 |
| Application number | US-201515314644-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 19, 2015 |
| Priority date | Jun 3, 2014 |
| Publication date | Oct 1, 2019 |
| Grant date | Oct 1, 2019 |
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A method of manufacturing a wheel has a step (a) during which, by injecting a first polymer material into a first mold, a bearing core is created that extends from a radially internal wall that forms the ball of a steering axis, as far as a radially external peripheral edge, followed by a step (b) of coating during which step a coating layer is overmolded in a second polymer material over the bearing core to form a rim around the peripheral edge, the method being such that during step (a) of creating the bearing core, a preformed reinforcing hoop made of a third material referred to as “reinforcing material” is placed in the first mold then the reinforcing hoop is at least partially embedded in the peripheral edge during injection of the first material.
Opening claim text (preview).
The invention claimed is: 1. A method for manufacturing a wheel, said method comprising: a step (a) of producing a carrier core by injection of a first polymer material in a first mold, wherein the carrier core extends from a radially inner wall forming a bore having a main axis, corresponding to an axis of rotation of the wheel, up to a radially outer peripheral edge, and a coating step (b) during which a coating layer of a second polymer material is formed over the carrier core by an overmolding operation in order to form a rim about the peripheral edge, in the radial over-thickness of the radially outer surface of said peripheral edge, wherein, during the step (a) of producing the carrier core, and before the injection of the first polymer material, a preformed reinforcing ring made of a third material is placed in the first mold, in a position substantially centered on the main axis, then is embedded, at least partially, in the mass of said first material which forms the peripheral edge while injecting the first material, wherein the third material is distinct from the first polymer material and from the second polymer material and has a Young's modulus greater than a Young's modulus of the first material and greater than a Young's modulus of the second material, and wherein the reinforcing ring is formed by a reinforced tape made in a composite reinforcing material which comprises a frame made of continuous reinforcing fibers that extend along the perimeter of the reinforcing ring, according to a direction orthoradial to the main axis, said frame being embedded in a matrix made of thermoplastic polymer material. 2. The method according to claim 1 , wherein the carrier core comprises a hub, which extends axially between a radially inner wall forming the bore and a radially outer surface, a flange which extends substantially radially from said hub up to a flanged edge, which is distinct and radially spaced from the radially outer surface of the hub, and which forms the peripheral edge, and wherein the reinforcing ring is pressed against the radially inner surface of the flanged edge, which faces the radially outer surface of the hub. 3. The method according to claim 2 , wherein, during step (a) of producing the carrier core, a plurality of reinforcing ribs is formed by injection of the first material, the plurality of reinforcing ribs disposed according to a plurality of azimuths about the main axis in order to locally reinforce the axial thickness of the flange, said reinforcing ribs each connecting the radially outer surface of the hub to the radially inner surface of the flanged edge as well as to the lower surface of the flange, which is axially oriented on the side of said flanged edge. 4. The method according to claim 3 , wherein the reinforcing ring is in a form of a serrated crown provided with a plurality of passage slots allowing the reinforcing ribs to pass through the radial thickness of the reinforcing ring without said reinforcing ribs being interrupted by said reinforcing ring. 5. The method according to claim 3 , wherein during step (a) of producing the carrier core, an at least partial re-fusion of the matrix of the reinforcing ring is carried out, so as to connect said matrix with the flanged edge and with the reinforcing ribs, so that the reinforcing ring forms an adhesion interface which radially interrupts the reinforcing ribs while ensuring a connection between the radially inner wall of the flanged edge, to which adheres the radially outer surface of said reinforcing ring and said reinforcing ribs, which adhere to, and start on, the radially inner surface of the same reinforcing ring. 6. The method according to claim 1 , wherein the reinforcing ring has a cross section, whose axial height is strictly greater than the radial thickness. 7. The method according to claim 1 , wherein the reinforcing ring is split along its entire axial height by an opening gap so as to facilitate an elastic clipping of said reinforcing ring within the first mold. 8. The method according to claim 1 , further comprising, after the coating step (b), a step (c) of cutting teeth, during which meshing teeth are cut in the rim.
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