发明名称 RIB FOR WING
摘要 PROBLEM TO BE SOLVED: To provide a rib for a wing excellent in lightweight properties, high strength, and low cost (structure simpleness).SOLUTION: A rib R for a wing includes a web 1 and a flange 2 provided at an end of the web 1. The web 1 and the flange 2 are integrally constructed. The web 1 has a core 3 inside. The relation of (a thickness of a cover layer portion 4 covering the core 3 at a position of an end portion of the internal core)>(a thickness of the cover layer portion 4 covering the core 3 at a position of a center portion of the internal core 3) is satisfied.
申请公布号 JP2014015085(A) 申请公布日期 2014.01.30
申请号 JP20120152643 申请日期 2012.07.06
申请人 JAPAN AIRCRAFT MFG CO LTD 发明人 MURASE MASATAKA;FUKUOKA TERUKI;AOI TATSUJI
分类号 B64C3/20;B64C3/18 主分类号 B64C3/20
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