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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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