发明名称 |
SINGLE PIECE FLOW BASED WING ASSEMBLY SYSTEM |
摘要 |
A method for assembling wings includes supporting a pair of wing spars, which include a plurality of coordination features, upon a pair of stanchions in a generally horizontal position. A plurality of ribs and wing panels are accurately fastened to the pair of wing spars at a first workstation using the coordination features to position accurately the parts. The combination is transferred to downstream workstations via a ground transport vehicle for further processing and assembly to define a pulsed flow wing assembly system. |
申请公布号 |
AU2003268281(A1) |
申请公布日期 |
2004.03.19 |
申请号 |
AU20030268281 |
申请日期 |
2003.08.27 |
申请人 |
THE BOEING COMPANY |
发明人 |
CLAYTON, L. MUNK;LUIS, A. PERIA;HARRY, E. TOWNSEND;DAN, D. DAY |
分类号 |
B64F5/00 |
主分类号 |
B64F5/00 |
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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