发明名称 Reduced-perimeter aircraft
摘要 Aircraft that have fuselages including a series of frames spaced apart according to a frame pitch. The series of frames are covered by an aircraft skin to define an interior volume of the aircraft. The interior volume contains a series of rows of seats separated according to a seat pitch. The seat pitch may be indexed to the frame pitch such that seats are located between adjacent ones of the series of frames to permit a reduced-perimeter aircraft fuselage with substantially equal passenger comfort metrics. In some embodiments, in addition, a series of windows are located adjacent outboard seats of the series of rows of seats to permit ergonomically appropriate viewing through the series of windows by passengers seated in the outboard seats.
申请公布号 US7717372(B2) 申请公布日期 2010.05.18
申请号 US20070764021 申请日期 2007.06.15
申请人 THE BOEING COMPANY 发明人 SANKRITHI MITHRA M. K. V.;CARNEGIE CAMERON;BOREN KELLY;COLEBROOK PETER
分类号 B64D11/06 主分类号 B64D11/06
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