Process for the production of a panel of composite material with stiffening strips
AssigneeAirbus France
InventorsMichel Buge, Eric Rambaud, Alain Porte, Bruno Legeay
Life of this patent
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AssigneeAirbus France
InventorsMichel Buge, Eric Rambaud, Alain Porte, Bruno Legeay
Estimating the term…
A process for the production of a panel (7) of composite material with stiffening strips (3), in which a mold (1) is draped with at least one first ply (2) of fibers pre-impregnated with resin, there is emplaced at desired positions on said ply (2) at least one stiffening strip (3), the stiffening strip (3) as well as at least a portion of the remaining surface of the first ply (2) is covered with at least one second ply (4) of fibers pre-impregnated with resin, then a bladder (6) is placed to cover the above elements, the assembly is then placed under vacuum and then in an autoclave to polymerize the resin. Before emplacement of the stiffening strip (3) and/or of the second ply (4), there is interposed at least one layer (5) of a non-adherent material between at least one portion of the surface of the stiffening strip (3) and one and/or the other of the plies (2, 4).
Process for the production of a panel (7) of composite material with stiffening strips (3), in which a mold (1) having the shape and size of the panel to be produced, is draped with at least one first ply (2) of fibers pre-impregnated with resin, there is emplaced at desired positions on said ply (2) at least one stiffening strip (3), the stiffening strip (3) as well as at least a portion of the remaining surface of said first ply (2) is covered with at least one second ply (4) of fibers pre-impregnated with resin, then a bladder (6) is positioned to cover the above elements to form an assembly, a suitable vacuum is drawn in the space between the mold (1) and the bladder (6), the assembly is then disposed in an autoclave to subject it to a pre-established polymerization cycle for the resin, at temperatures and pressures suitable to said resin, and finally, the panel is demolded;
Dependencies are inferred from the claim text.