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AssigneeSociete Europeenne de Propulsion
InventorsAndre Delage, Jean-Michel Georges, Jean-Pierre Maumus
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A method of manufacturing a honeycomb structure of thermostructural composite material comprising a fiber reinforcing fabric densified by a matrix, the fibers of the reinforcing fabric being of a material selected from carbon and ceramics, as is the matrix, the method comprising the following steps: making a three-dimensional fiber fabric by means of superposed two-dimensional plies that are bonded together by means of fibers passing through the plies; making slit-shaped cuts in a staggered configuration through the plies, and through the entire thickness of the fabric; stretching the cut fabric in a direction that is not parallel to the cuts but that is parallel to the plies so as to form cells whose walls are constituted by the lips of the cuts; and while the cut texture is held in the stretched state, densifying it using the matrix-constituting material to obtain a rigid honeycomb structure of thermostructural material.
A honeycomb structure of thermostructural composite material comprising a fiber reinforcing fabric densified by a matrix, the fibers of the reinforcing fabric and the matrix being of a material selected from the group consisting of carbon and ceramics, wherein the reinforcing fabric is a three-dimensional fabric formed by superposed two-dimensional plies bonded together by fibers passing through the plies, and wherein the honeycomb structure shows cells having walls formed from cuts extending through the entire thickness of the fabric.
Dependencies are inferred from the claim text.