发明名称 HELICOPTER ROTOR LEAD-LAG DAMPER
摘要 <p>IMPROVED HELICOPTER ROTOR LEAD LAG DAMPER 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.</p>
申请公布号 CA1078354(A) 申请公布日期 1980.05.27
申请号 CA19770281544 申请日期 1977.06.28
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FERRIS, DONALD L.;SMITH, GEORGE A.
分类号 B64C27/51;(IPC1-7):64C27/42 主分类号 B64C27/51
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