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 |