首页> 外国专利> Main landing gears fixing device for aircraft, has deployment unit permitting to move gears between storage and deployment positions, and fixation unit connecting end of gears on fuselage structure, where housing receives gears of aircraft

Main landing gears fixing device for aircraft, has deployment unit permitting to move gears between storage and deployment positions, and fixation unit connecting end of gears on fuselage structure, where housing receives gears of aircraft

机译:飞机的主要起落架固定装置,具有允许在存储位置和展开位置之间移动齿轮的展开单元,以及在机身结构上连接齿轮末端的固定单元,壳体容纳飞机的齿轮

摘要

The device has a fixation unit connecting an end of two main landing gears (2) on a peripheral fuselage structure (7) of an aircraft (1), where the structure permits direct retrieval of forces from the gears. A gear housing is formed in the fuselage structure of the aircraft, and receives the gears. A deployment unit permits to move the gears between a storage position where the gears enter the housing, and a deployment position where the gears are released from the housing such that wheels (10) of the gears are placed under a low wing (4) of the aircraft.
机译:该装置具有固定单元,该固定单元将两个主起落架(2)的端部连接在飞机(1)的外围机身结构(7)上,其中该结构允许直接从起落架上取回力。齿轮箱形成在飞机的机身结构中,并容纳齿轮。展开单元允许在齿轮进入壳体的存放位置与齿轮从壳体释放的展开位置之间移动齿轮,从而使齿轮的轮(10)置于齿轮的低翼(4)下方。飞机。

著录项

  • 公开/公告号FR2897591A1

    专利类型

  • 公开/公告日2007-08-24

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20060050596

  • 发明设计人 DANILO CIPRIAN;

    申请日2006-02-22

  • 分类号B64C25/04;B64C25/12;

  • 国家 FR

  • 入库时间 2022-08-21 20:26:49

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