发明名称 |
IMPROVEMENT OF DOUBLE HUNG VIBRATION ABSORBER FOR HELICOPTER ROTARY WING |
摘要 |
A multibladed helicopter rotor carries at least three bifilar absorbers which are tuned to eliminate in-plane vibrations of the rotor which otherwise would be transmitted to the helicopter fuselage. Improved tuning pin assemblies and cooperating tracking inserts for the absorber reduce the undesirable frictional damping heretofore encountered in bifilar absorbers by centering the pendulous elements of the absorbers relative to their support members and reacting forces normal to centrifugal force by permitting flapping movement of the bifilar mass in the vertical plane. |
申请公布号 |
JPS51126699(A) |
申请公布日期 |
1976.11.04 |
申请号 |
JP19760039769 |
申请日期 |
1976.04.08 |
申请人 |
UNITED TECHNOLOGIES CORP |
发明人 |
RARII BURUUSU IISUTOMAN;AAUIN JIEFUREI KENIGUSUBAAAGU |
分类号 |
B64C27/51;B64C27/00 |
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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