发明名称 CRASH ATTENUATION LANDING GEAR
摘要 <p>In a landing gear for an airframe mounted on a cushioned strut, an airframe mounted portion is guided along a landing gear portion after the landing gear touches down. Crash attenuation is absorbed by a work absorbing tube secured at one end thereof to the airframe portion in an encircling relation with respect to the airframe portion. A work applying structural fitting is secured to the airframe at the other end of the work absorbing tube and is adapted to engage and work the tube as the airframe moves downward relative to the airframe portion to dissipate energy involved in arresting downward movement of the airframe. Coupling structure between the airframe and the airframe mounted portion is provided to fail at a predetermined load to permit movement of the airframe relative to the airframe portion.</p>
申请公布号 CA1032143(A) 申请公布日期 1978.05.30
申请号 CA19760257096 申请日期 1976.07.15
申请人 TEXTRON INC. 发明人 FAGAN, CASTLE H.
分类号 B64C25/58;B64C25/60;(IPC1-7):64C25/58 主分类号 B64C25/58
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