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Front landing gear of reduced height and aircraft, in particular a flying wing, equipped with such a front landing gear

机译:高度降低的前起落架和配备有这种前起落架的飞机,尤其是机翼

摘要

A front landing gear comprising an undercarriage and a landing gear bay, the undercarriage including a single wheel, a landing gear strut and a stay rod, the undercarriage being movable between a retracted position in which it is stowed inside the landing gear bay and a deployed position in which it extends mainly outside the landing gear bay and the aircraft, the wheel then extending in a median longitudinal plane of the aircraft. The landing gear strut is laterally offset, extending in a plane strictly parallel to the plane of the wheel. The landing gear strut is articulated about a longitudinal axis pivot connection such that, when the undercarriage is moved between its retracted and deployed positions, the landing gear strut moves in a transverse plane. The front landing gear is particularly suitable for an aircraft of flying wing type.
机译:一种包括起落架和起落架舱的前起落架,该起落架包括单轮,起落架支柱和撑杆,该起落架可在缩回位置之间移动,在该缩回位置中起落架被收起在起落架舱内并处于展开状态。在其主要延伸到起落架舱和飞机外部的位置,然后轮子在飞机的中间纵向平面中延伸。起落架支柱横向偏移,在严格平行于车轮平面的平面上延伸。起落架支柱围绕纵向轴线枢转连接铰接,使得当起落架在其缩回位置与展开位置之间移动时,起落架支柱在横向平面中移动。前起落架特别适用于飞行翼型飞机。

著录项

  • 公开/公告号US2018281934A1

    专利类型

  • 公开/公告日2018-10-04

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号US201815939869

  • 发明设计人 LAURENT SAINT-MARC;BERNARD GUERING;

    申请日2018-03-29

  • 分类号B64C25/12;B64C25/34;B64C39/10;

  • 国家 US

  • 入库时间 2022-08-21 12:57:33

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