- 专利标题: Linkage mechanism for driving aircraft landing gear bay door
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申请号: US14892698申请日: 2014-08-20
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公开(公告)号: US09868519B2公开(公告)日: 2018-01-16
- 发明人: Jun Lv , Qinggong Meng , Pu Zhang , Hao Jiang , Shangxin Yang , Hengkang Zhang , Jian Ma
- 申请人: COMMERCIAL AIRCRAFT CORPORATION OF CHINA., LTD , COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE
- 申请人地址: CN Shanghai
- 专利权人: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE
- 当前专利权人: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE
- 当前专利权人地址: CN Shanghai
- 代理机构: Dority & Manning, P.A.
- 优先权: CN201310513351 20131025
- 国际申请: PCT/CN2014/084769 WO 20140820
- 国际公布: WO2015/058580 WO 20150430
- 主分类号: B64C25/20
- IPC分类号: B64C25/20 ; B64C25/16 ; B64C25/10
摘要:
A linkage mechanism for controlling an aircraft landing gear hatch door includes a primary torsion tube having a first portion located inside a landing gear hatch and a second portion outside the landing gear hatch. A first drive apparatus transfer the driving force of a landing gear support column to the primary torsion tube. A secondary torsion tube has an inner end portion located inside the hatch and an outer end portion located outside the hatch. A second drive apparatus is located outside the landing gear hatch and connects the primary torsion tube and the secondary torsion tube outside the hatch. Two third drive apparatuses are connected between the inner end portion of the secondary torsion tube and one of the hatch doors.
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