发明名称 Method for making a fitting for joining the edges of composite sandwich panels
摘要 A method for fabricating a fitting (580) for a composite sandwich shell edge joint comprising the steps of: providing a bottom die (570) having a cavity therein; placing an inboard ply stack (560) in said cavity; positioning a collar tool (550) having a pocket (552) on top of said inboard ply stack (560); placing a bridge ply stack (540) in said pocket (560) of the collar tool (550); placing an outboard ply stack (530) on top of said bridge ply stack (540); positioning a top die (520) on top of said outboard ply stack (530); and curing said inboard ply stack (560), said bridge ply stack (540) and said outboard ply stack (530) to form said fitting (580).
申请公布号 EP2455214(A3) 申请公布日期 2016.02.17
申请号 EP20110189988 申请日期 2011.11.21
申请人 THE BOEING COMPANY 发明人 HAND, MICHAEL LESLIE;MCCARVILLE, DOUGLAS A.;GUZMAN, JUAN CARLOS
分类号 B29C70/46;B29C65/56;F16B5/01 主分类号 B29C70/46
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