发明名称 Vertically retractable landing gear for transport aircraft
摘要 <p>The undercarriage consists of a number of legs (101) in a line parallel to the aircraft's median lengthwise axis, with a pair of wheels (R) on the lower end of each arm. Each leg comprises a tubular body (102) fixed to the aircraft structure, with a balance arm (103) pivoted to its lower end, and a shock absorber (106) pivoted between a branch (105) on the balance arm and a slider (110) inside the tubular body. The slider is connected to an actuating power cylinder (125) by links (120, 123) at the top of the tubular body so that it is moved axially between two positions corresponding to the raised and lowered undercarriage.</p>
申请公布号 EP1279591(A1) 申请公布日期 2003.01.29
申请号 EP20020291589 申请日期 2002.06.26
申请人 MESSIER-DOWTY S.A. 发明人 DERRIEN, MICHEL;DUCOS, DOMINIQUE;LOCUFIER, JEAN-FRANCOIS
分类号 B64C25/10;B64C25/20;(IPC1-7):B64C25/10;B64C25/58 主分类号 B64C25/10
代理机构 代理人
主权项
地址