发明名称 Adaptive airplane landing gear
摘要 A duo mode gas hydraulic shock absorbing landing gear strut with a pneumatic spring in combination with a hydraulic fluid controlling orifice for touchdown and automatic means for changing mode after touchdown to impart new pneumatic spring characteristics and to provide duo paths for controlling hydraulic fluid flow.
申请公布号 US4273303(A) 申请公布日期 1981.06.16
申请号 US19790021365 申请日期 1979.03.16
申请人 THE BOEING COMPANY 发明人 SOMM, PAUL T.
分类号 B60G17/015;B64C25/60;(IPC1-7):B64C25/58 主分类号 B60G17/015
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