发明名称 |
Commercial aircraft low cost, lightweight floor design |
摘要 |
An aircraft deck support system includes horizontal deck support beams connected to the aircraft's frames. Each deck support beam has a plurality of machined, generally T-shaped supports. Each T-shaped support includes either a horizontal recess or a raised surface formed in a deck support beam upper chord and a U-shaped aperture formed in a beam web. The T-shaped support matably receives a cross-support beam attachment flange perpendicularly aligned with the deck support beams. Each cross-support beam includes a web perpendicularly connected at an upper end to the attachment flange, and a stiffening flange at a web lower end. Both the web and the stiffening flange are freely suspended within the U-shaped aperture of the T-shaped support. When joined, the cross-support beam seats on the T-shaped support allowing both the cross-support beam and the deck support beam to develop maximum bending moments at a reduced structural weight.
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申请公布号 |
US6554225(B1) |
申请公布日期 |
2003.04.29 |
申请号 |
US20020171608 |
申请日期 |
2002.06.14 |
申请人 |
THE BOEING COMPANY |
发明人 |
ANAST PETER Z.;HANSKEN RICKIE |
分类号 |
B64C1/18;(IPC1-7):B64C1/00 |
主分类号 |
B64C1/18 |
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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