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US 2022/0009183 A1Published application
Method of manufacture of a composite material
AssigneeHexcel Composites Limited
InventorMarco ARCIDIACONO
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Abstract
A method of manufacture of a composite component is provided, the method comprising the steps of providing two layers of pre-preg composite material, one of which has an edge adjacent a surface of the other. Pressure and, optionally, vibrational energy is applied to the edge to thereby smooth the ply drop.
Claims20
A method of joining together multiple layers of pre-preg, comprising the steps of:
- providing a first layer of pre-preg, said layer having a surface and a plurality of edges;
- providing a second layer of pre-preg, the second layer having a surface and a plurality of edges;
- laying-up the first and second layers of pre-preg such that an edge of the second layer is adjacent a surface of the first layer of pre-preg, but such that the edges of the first and second layers of pre-preg do not terminate in the same place, the difference in positioning of said edges forming an edge drop;
- and
- applying pressure and vibrational energy to the edge of the second layer of pre-preg to thereby smooth the ply drop at the edge of the second layer of prepreg;
- wherein the step of applying pressure and vibrational energy to the edge of the second layer is carried out at a first position and wherein the method comprises a further step of applying pressure and vibrational energy to the second layer at a second position, the second position being offset in a direction normal to the edge of the second layer with respect to the first position;
- wherein the pressure applied is between 20 kPa and 500 kPa;
- and wherein
- the second layer defines an undulating formation having a plurality of protrusions having triangular or curved edges.
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Dependencies are inferred from the claim text.