发明名称 Method for manufacturing composite components
摘要 Methods and systems for manufacturing composite components, including asymmetric composite components, are disclosed. In one embodiment, a method of forming a composite component includes providing a forming tool having a base portion and at least one retaining portion; forming an uncured composite component on the forming tool; curing the composite component; performing a manufacturing operation on the cured composite component engaged with the forming tool; and after performing the manufacturing operation on the cured composite component, removing the cured composite component from the forming tool. In further embodiments, the forming tool may have a plurality of reference apertures disposed therethrough for performing drilling operations on the cured composite component.
申请公布号 US7748119(B2) 申请公布日期 2010.07.06
申请号 US20050144146 申请日期 2005.06.03
申请人 THE BOEING COMPANY 发明人 KISMARTON MAX U.
分类号 B21D53/88;B32B9/02 主分类号 B21D53/88
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