发明名称 Helicopter rotor lead-lag damper
摘要 A helicopter rotor lead-lag hydraulic fluid damper has an internal anti-torque shaft preventing rotary motion of the dynamic fluid retaining seal. An independent fluid reservoir under centrifugal force supplies lubrication to the low pressure side of the seal. At rest, the fluid returns to the lower reservoir chamber by gravity.
申请公布号 US4105365(A) 申请公布日期 1978.08.08
申请号 US19760729340 申请日期 1976.10.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FERRIS, DONALD LEROY;SMITH, GEORGE ARTHUR
分类号 B64C27/51;(IPC1-7):B64C27/42 主分类号 B64C27/51
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