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公开(公告)号：US20170174311A1
公开(公告)日：2017-06-22
申请号：US14975115
申请日：2015-12-18
申请人： The Boeing Company
摘要： An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage without changing the structural layout or configuration of the fuselage structural interfaces.
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公开(公告)号：US11279472B2
公开(公告)日：2022-03-22
申请号：US16405794
申请日：2019-05-07
申请人： The Boeing Company
摘要： Systems and methods for wide set retracting landing gear of a cargo aircraft. One embodiment is an aircraft that includes a fuselage including a nose, and a pair of main landing gears comprising a pair of main posts disposed across the fuselage, each main post having a main wheel and configured to pivot forward toward the nose to retract the main wheel. The aircraft also includes a pair of nose landing gears comprising a pair of nose posts disposed across the fuselage, each nose post having a nose wheel and configured to pivot inboard to retract the nose wheel.
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公开(公告)号：US09849966B2
公开(公告)日：2017-12-26
申请号：US14975115
申请日：2015-12-18
申请人： The Boeing Company
摘要： An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage without changing the structural layout or configuration of the fuselage structural interfaces.
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