发明授权
- 专利标题: Airplane fuselage
- 专利标题(中): 飞机机身
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申请号: US548796申请日: 1995-11-01
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公开(公告)号: US5806797A公开(公告)日: 1998-09-15
- 发明人: Antonio C. Micale
- 申请人: Antonio C. Micale
- 申请人地址: WA Seattle
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 当前专利权人地址: WA Seattle
- 主分类号: B23P21/00
- IPC分类号: B23P21/00 ; B23Q35/02 ; B25J9/16 ; B64C1/00 ; B64C1/06 ; B64C1/12 ; B64F5/00 ; G05B19/418
摘要:
An airplane fuselage including a plurality of individual subassemblies having components that are aligned using coordination holes. The components include an assembly of panels, a plurality of stringer clips, a plurality of frame members, shear ties, and a floor grid made of a plurality of crossmembers. The coordination holes are drilled in selected components and are located at positions on the subassemblies to accurately align the subassemblies relative to each other so the spatial relationship between key features of the subassemblies make them self-locating and intrinsically determinant of the final contour and configuration of the airplane fuselage, independent of hard tooling.
公开/授权文献
- US4994811A Sensitivity time control device 公开/授权日:1991-02-19