发明名称 STRUCTURAL INTEGRATED REPAIR METHOD AND SYSTEM TOOL DEVICE FOR REPAIRING DELAMINATED COMPOSITE STRUCTURES
摘要 A system for repair of damaged holes in composite structures (10) incorporates a repair system tool device (33) having a sleeve (34) sized to be closely received in a hole (16) in a composite structure. The sleeve has a central bore (50) for receiving parent resin and an array of orifices (36) for radial expulsion of the parent resin into the hole. A caul plate (62) seals the central bore and a vacuum bag (68) covering the caul plate is sealed to the surface of the composite structure. Introduction of vacuum in the vacuum bag provides a differential pressure for infusion of resin from the orifices in the sleeve into delaminations extending from the hole.
申请公布号 EP2939822(A1) 申请公布日期 2015.11.04
申请号 EP20150165084 申请日期 2015.04.24
申请人 THE BOEING COMPANY 发明人 DAN-JUMBO, EUGENE
分类号 B29C73/02;B29C65/00;B29C65/48;B29C65/54;B29C70/44;B29C70/54;B29C73/14;B29C73/30;B32B37/00 主分类号 B29C73/02
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