发明名称 SYSTEM AND METHOD FOR MANUFACTURING A STIFFENED COMPOSITE STRUCTURE
摘要 A system for manufacturing a stiffened composite panel may include a stiffener tooling assembly, a caul plate, and a rotatable strongback. The stiffener tooling assembly may include stiffener tooling configured to support a plurality of composite stiffeners. The caul plate may have a layup surface for laying up a composite skin. The strongback may be releasably coupled to the caul plate. The system may include a plurality of hinges each having a fixed hinge portion and a movable hinge portion. The movable hinge portion may be coupled to the strongback for rotation thereof between an open position and a closed position for engagement of the caul plate with the stiffener tooling assembly.
申请公布号 EP3112145(A1) 申请公布日期 2017.01.04
申请号 EP20160175420 申请日期 2016.06.21
申请人 The Boeing Company 发明人 ENCINOSA, Joe;BARWICK, Andrew;BICK, Robert
分类号 B29D99/00;B29C33/26 主分类号 B29D99/00
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