发明名称 Structural joint and a method for joining in reinforced thermoplastic fabrication
摘要 An aerodynamic structure comprising a skin having inner and outer opposed surfaces and a plurality of spaced, rectangular holes therethrough, each hole having a truncated triangular shape in one transverse cross-section, the truncated apex thereof being at the inner surface, and a support structure including a fiber-reinforced, thermoplastic spar in abutting relation to the inner surface, the spar including a plurality of spaced, integrally-formed, fiber-reinforced, thermoplastic tabs, each tab extending from the spar into a respective one of the holes and being shaped to fill the respective hole.
申请公布号 US5086997(A) 申请公布日期 1992.02.11
申请号 US19900502671 申请日期 1990.04.02
申请人 THE BOEING COMPANY 发明人 GLASS, BILLY M.
分类号 B29C65/60;B64C1/12;F16B17/00 主分类号 B29C65/60
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