发明名称 MANUFACTURE OF STIFFENED COMPOSITE STRUCTURES
摘要 <p>A method of manufacturing a stiffened composite structure comprising the steps of: forming the structure around a mandrel tool; using digital camera data to record the positions of desired pad locations on the structure; bonding pads to the structure at the desired locations; curing the pads and structure; forming stiffeners from composite materials including forming a plurality of tabs at points on the stiffener corresponding to the pads on the structure; using a laser theodolite connected to receive the stored information of the pad locations relative to a datum point on the stiffener to locate the stiffener tabs accurately on the pads; and bonding the stiffeners to the structure via the tabs and pads. Preferably, the location tabs and pads are machined off the final stiffened structure after autoclaving.</p>
申请公布号 EP1077804(A1) 申请公布日期 2001.02.28
申请号 EP19990919432 申请日期 1999.05.04
申请人 BAE SYSTEMS PLC 发明人 DUFFY, ROGER, PHILLIP,
分类号 B29C70/16;B29B11/16;B29C31/08;B29C70/54;(IPC1-7):B29C70/30 主分类号 B29C70/16
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