发明名称 METHOD FOR MOLDING AIRCRAFT WING STRUCTURE
摘要 PROBLEM TO BE SOLVED: To provide a method for molding an aircraft wing structure capable of improving aircraft performance and appearance. SOLUTION: The prepreg moldings 26 and 28 for a hollow structure are formed by winding a front margin prepreg, a front middle prepreg, a rear middle prepreg and a rear margin prepreg around the respective corresponding forming molds or a front margin mold, a silicone resin-made front middle core mold 35, a rear middle mold, a silicone resin-made rear margin core mold 51, and a metallic rear margin core mold 53 so that both the ends overlap with each other. The overlapping portion is arranged in the area of a middle beam. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011152753(A) 申请公布日期 2011.08.11
申请号 JP20100016848 申请日期 2010.01.28
申请人 HONDA MOTOR CO LTD 发明人 SHIMAMIYA TOMOHIRO;NAMAIZAWA MASAKI;YANAKA SEIWA;SUGIMOTO YOSHIAKI
分类号 B29C43/34;B29C43/10;B29C43/18;B29K105/08;B29L9/00;B29L24/00;B29L31/30;B64C3/20 主分类号 B29C43/34
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