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Wide-body supersonic airliner

机译:宽体超音速客机

摘要

An airliner in which the wheel bogies of the main landing gear are stored one behind the other in a narrow, hollow keel at the bottom of the fuselage. The narrow keel replaces the usual voluminous hold under the passenger cabin. This decreases the cross-sectional area of the fuselage, to reduce aerodynamic drag.;One main strut of the landing gear angles forward during retraction, while the other strut angles backward. That allows the bogie tandem storage. It also requires swiveling a bogie as it enters the keel. The folding of the drag brace during strut retraction powers the swiveling mechanism. Elsewhere, the side brace folds and twists during retraction.;Dividing the main wing spar at the fuselage and passing only the bottom half under the cabin preserves the reduced hold volume. The decreased cross-sectional area allows the passenger cabin to be enlarged. It creates a “wide-body” supersonic airliner able to carry more passengers.
机译:一架客机,主起落架的车轮转向架在机身底部的狭窄空心龙骨中一个接一个地存放。狭窄的龙骨代替了乘客舱下通常的大容积。这减小了机身的横截面面积,以减小空气阻力。;在收起期间,起落架的一个主支柱向前倾斜,而另一支柱向后倾斜。这样就可以将转向架串联存储。它还需要在转向架进入龙骨时将其旋转。撑杆缩回期间阻力支架的折叠为旋转机构提供了动力。在其他地方,侧面撑杆在收起时会折叠和扭曲。在机身上划分主翼翼梁,并仅使机舱的下半部通过,以减少固定空间。减小的横截面面积允许客舱增大。它创造了一种“宽体”超音速客机,能够搭载更多乘客。

著录项

  • 公开/公告号US2012193470A1

    专利类型

  • 公开/公告日2012-08-02

    原文格式PDF

  • 申请/专利权人 PATRICK A. KOSHELEFF;

    申请/专利号US20110931409

  • 发明设计人 PATRICK A. KOSHELEFF;

    申请日2011-02-01

  • 分类号B64C25/12;B64C30;B64D11;

  • 国家 US

  • 入库时间 2022-08-21 17:33:01

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