发明名称 Fuselage housed aircraft undercarriage - has bar connecting main leg and operating jack to rotate wheel axis when extending or retracting
摘要 <p>The retractable aircraft undercarriage has separate units for each side. Each unit consists of a wheel and axle asson an angles shaft (3) free to rotate in a sleeve (4) on the end of the main undercarriage leg (5). This leg is connected to the fuselage by a universal joint (6, 7); backed up by a shock absorber (8) flexibly mounted between the two. The operating unit (12) has its piston rod (13) flexibly supported (17) from the fuselage. Its cylinder (14) is linked to the wheel mounting shaft (3) by a universal coupling (15); to the main leg by a pin jointed bar (16) perpendicular to its axis. Undercarriage retraction /extension thus rotates the wheel assembly in its sleeve.</p>
申请公布号 FR2381663(A1) 申请公布日期 1978.09.22
申请号 FR19770005230 申请日期 1977.02.23
申请人 MESSIER HISPANO 发明人
分类号 B64C25/14;(IPC1-7):64C25/14 主分类号 B64C25/14
代理机构 代理人
主权项
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