发明授权
US09073629B2 Main landing gear of an aircraft, comprising two walking beams joined to the structure of the aircraft in an articulated manner 有权
飞机的主起落架,包括以铰接方式连接到飞行器结构的两个步进梁

  • 专利标题: Main landing gear of an aircraft, comprising two walking beams joined to the structure of the aircraft in an articulated manner
  • 专利标题(中): 飞机的主起落架,包括以铰接方式连接到飞行器结构的两个步进梁
  • 申请号: US13699911
    申请日: 2011-06-16
  • 公开(公告)号: US09073629B2
    公开(公告)日: 2015-07-07
  • 发明人: Dominique Ducos
  • 申请人: Dominique Ducos
  • 申请人地址: FR Velizy Villacoublay
  • 专利权人: MESSIER-BUGATTI-DOWTY
  • 当前专利权人: MESSIER-BUGATTI-DOWTY
  • 当前专利权人地址: FR Velizy Villacoublay
  • 代理机构: Sughrue Mion, PLLC
  • 优先权: FR1054775 20100616
  • 国际申请: PCT/EP2011/060071 WO 20110616
  • 国际公布: WO2011/157807 WO 20111222
  • 主分类号: B64C25/10
  • IPC分类号: B64C25/10 B64C25/34 B64C25/14 B64C25/12
Main landing gear of an aircraft, comprising two walking beams joined to the structure of the aircraft in an articulated manner
摘要:
An aircraft undercarriage comprising two rocker beams (1, 2) carrying wheels and mounted to pivot on a common pivot (Y1), the undercarriage including a shock-absorber device comprising two connecting rods (5, 6), each rod (5, 6) being coupled to a respective rocker beam, at least one connecting rod being telescopic and forming a shock absorber. The two connecting rods also are coupled to a rocker (7) pivotally mounted on a central pivot (8), wherein the common pivot of the rocker beams is secured to a structure of an aircraft to which the undercarriage is fastened and is mounted in a fixed position on the structure. The central pivot of the rocker is movable between a first position (rocker beams in a landing position) and a second position in which a rocker has pulled on the connecting rods to cause the rocker beams to pivot towards a retracted position of the undercarriage.
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