发明名称 Fabrication method of composite components and thus obtained components
摘要 During the cooking of a composite component including layers of fibers embedded into a matrix, a superficial pressure is exerted. This superficial pressure generates a deformation that causes local contacts of fibers of at least two layers without damaging these fibers. As a result, when an electrical current is applied on a side of the composite component, such as during a lightning strike or a short circuit, the added local contacts enable the electric current to flow along multiple fibers in the composite component, thereby avoiding significant spikes in temperature.
申请公布号 US8790564(B2) 申请公布日期 2014.07.29
申请号 US201113182123 申请日期 2011.07.13
申请人 Airbus Operations (SAS) 发明人 Provost Benjamin
分类号 B29C70/00;B29C70/44;B29C70/88;B29K707/04 主分类号 B29C70/00
代理机构 Wood, Herron & Evans, LLP 代理人 Wood, Herron & Evans, LLP
主权项 1. A method for manufacturing a composite component comprising superimposed layers of electrically conductive fibers embedded into an electrically insulating matrix the method comprising: (A) forming an assembly comprising superimposed layers of electrically conductive fibers and separated by a resin intended for making up the matrix; (B) achieving a vacuum around the assembly; (C) submitting the assembly in vacuum to a compression and a cooking, wherein at least during the cooking, a superficial pressure is exerted on the assembly generating a deformation that causes local contacts of fibers of at least two superimposed layers, without damaging the fibers; and (D) removing the pressure plate following step (C), wherein before steps (B) and (C), the method includes applying a pressure plate, the pressure plate provided with an uneven surface on a side of the assembly so as to create the superficial pressure, and wherein during the steps (B) and (C), the method includes maintaining the pressure plate in position.
地址 Toulouse Cedex FR