发明名称 Stiff panel having composite stiffeners with reduced shock sensitivity
摘要 A stiff panel (1) comprises a skin (2) and at least one stiffener (3) of composite material on said skin. Free surface (311) of web (31) of stiffener (3) on the stiff panel according to the invention comprises a deformable core (33) and a covering (34) which covers core (33) and joins said core with structural part (35) of web (31). The width of core (33) is equal to or greater than the width of structural part (35) of web (31) of stiffener (3), depending on the shock energy against which panel (1) must be protected.
申请公布号 US7814729(B2) 申请公布日期 2010.10.19
申请号 US20070766177 申请日期 2007.06.21
申请人 AIRBUS FRANCE 发明人 NORMAND MATHIEU;LACOMBE JEAN-CLAUDE
分类号 B29D99/00;E04C2/38 主分类号 B29D99/00
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