发明名称 |
Manufacture of stiffened composite structures |
摘要 |
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. |
申请公布号 |
AU3722199(A) |
申请公布日期 |
1999.12.06 |
申请号 |
AU19990037221 |
申请日期 |
1999.05.04 |
申请人 |
BRITISH AEROSPACE PUBLIC LIMITED COMPANY. |
发明人 |
ROGER PHILLIP DUFFY |
分类号 |
B29C70/16;B29B11/16;B29C31/08;B29C70/54 |
主分类号 |
B29C70/16 |
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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