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
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