首页>
外国专利>
METHOD FOR MANUFACTURING A PANEL OF AN AIRCRAFT LEADING EDGE FOR PROVIDING AN EXTENDED LAMINAR FLOW, LEADING EDGE COMPRISING AT LEAST ONE PANEL OBTAINED BY THE METHOD
METHOD FOR MANUFACTURING A PANEL OF AN AIRCRAFT LEADING EDGE FOR PROVIDING AN EXTENDED LAMINAR FLOW, LEADING EDGE COMPRISING AT LEAST ONE PANEL OBTAINED BY THE METHOD
展开▼
机译:制造用于提供延伸的层流的飞机前缘板的方法,该方法包括至少一个前缘板
展开▼
页面导航
摘要
著录项
相似文献
摘要
A method for manufacturing an aircraft leading edge panel, includes a step of overmoulding a coating onto a sheet positioned in a cavity of a mould, which cavity is delimited by a shaping surface which exhibits an optimized surface finish. The coating includes, after the overmoulding step, an exterior face which corresponds to the exterior face of the panel that is to be obtained and which exhibits an optimized surface finish conferred by the shaping surface of the mould. A panel may be obtained using this method and a leading edge includes at least one such panel. Because of the optimized surface finish of the exterior surface thereof, the panel contributes to extending the regions of laminar flow.
展开▼