Method for producing a semi-finished product or component comprising a metal carrier and a hardenable coating with fibre-reinforced plastic
US-2015298399-A1 · Oct 22, 2015 · US
US10974469B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10974469-B2 |
| Application number | US-201616060985-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 12, 2016 |
| Priority date | Dec 11, 2015 |
| Publication date | Apr 13, 2021 |
| Grant date | Apr 13, 2021 |
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A method for manufacturing a semifinished product or part is disclosed in which a metal support embodied as a metal sheet or blank is covered with at least one prepreg containing a thermally cross-linkable thermosetting matrix with endless fibers, the thermosetting matrix of the prepreg is pre-cross-linked by means of heating, and the metal support covered with the pre-cross-linked prepreg is formed into a semifinished product or part by means of deep drawing or stretch deep drawing. In order to enable plastic deformation in fiber-reinforced regions of the metal support, it is proposed that during the pre-cross-linking of the thermosetting matrix of the prepreg, its matrix is transferred into a viscosity state that is higher than its minimum viscosity and prior to reaching its gel point, the prepreg is formed together with the metal support.
Opening claim text (preview).
The invention claimed is: 1. A method for manufacturing a semifinished product or part, comprising: covering a metal support embodied as a metal sheet or blank with at least one prepreg containing a thermally cross-linkable thermosetting matrix with endless fibers, pre-cross-linking the thermosetting matrix of the prepreg by heating, and forming the metal support covered with the pre-cross-linked prepreg into a semifinished product or part by deep drawing or stretch deep drawing with a forming tool holding the metal sheet or blank with a hold-down device, wherein during the pre-cross-linking of the thermosetting matrix of the prepreg, the matrix of the prepreg is transferred into a viscosity state that is higher than a minimum viscosity of the matrix and prior to reaching a gel point of the matrix, the prepreg is formed together with the metal support. 2. The method according to claim 1 , wherein before the forming, the degree of cross-linking of the thermosetting matrix is set to 4 to 15%. 3. The method according to claim 1 , wherein during the forming, the degree of cross-linking of the thermosetting matrix is set to 20 to 45%. 4. The method according to claim 3 , wherein during the forming, the degree of cross-linking (a) of the thermosetting matrix is set to 25 to 40%. 5. The method according to claim 1 , wherein during the forming, the thermosetting matrix is heated to 120 to 220° C. 6. The method according to claim 5 , wherein during the forming, the thermosetting matrix is heated to 150 to 180° C. 7. The method according to claim 1 , comprising heating the forming tool and forming the metal support by the heated forming tool. 8. The method according to claim 1 , wherein after the combined forming of the semifinished product or part, the prepreg undergoes unpressurized curing together with the metal support. 9. The method according to claim 1 , comprising, before or during the covering of the metal support with the prepreg, applying an intermediate layer to the metal support, which bonds the prepreg to the metal support. 10. The method according to claim 1 , wherein during the forming, the prepreg is held down on the metal support in some regions and is thus affixed to the metal support in those regions. 11. The method according to claim 10 , wherein during the forming, the prepreg is engaged in a forming way by segments or groups of segments of a female die and/or a male die of the forming tool. 12. The method according to claim 11 , wherein in the course of the forming procedure, an engagement region widens out in the segments or the groups of segments toward an edge of the metal support. 13. The method according to claim 1 , comprising covering the metal support in some regions with the at least one prepreg. 14. The method according to claim 13 , wherein 20 to 40% of a flat side of the metal support is covered with the at least one prepreg. 15. The method according to claim 1 comprising manufacturing a structural component of a vehicle.
Shaping or impregnating by compression (B29C70/34 takes precedence){not applied} · CPC title
{the layer of fibres or particles being impregnated or} embedded in a plastic substance · CPC title
of metal · CPC title
Multiple coating on one surface · CPC title
Knitted fabric · CPC title
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