作者: Yasuhiro Toi , Masahiro Noda , Atsushi Harada , Shigeki Tanaka
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摘要: PROBLEM TO BE SOLVED: To provide a wing made of composite material capable reducing cost, by splitting the into two interbeam structure front and rear in cord-directional central part, forming integratingly respectives thereof to be coupled using mechanical coupling means. SOLUTION: This is constituted 2 skeleton 4 formed integrally with beam 12, half rib 13 stringers 14, 15,16 material, outer plates 5, 6 bonded on upper under faces 4, 3 7 17, 18 19, 20, 21 8, 9 7, metal 10 for means 11. COPYRIGHT: (C)2002,JPO