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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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