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.
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
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