发明名称 |
Vibration attenuating suspension system for rotary-wing aircraft rotors |
摘要 |
A suspension system is disclosed for reducing vibration between the rotor and the structure of a rotary-wing aircraft having a reduction-gear train coextensive with the shaft of the lift rotor. The housing of said gear train is supported by tie-rods and by a flexible beam having its mid-point attached to said housing and its extremities attached to the aircraft structure through the medium of flexible blocks. The beam may be made of metal or a composite material.
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申请公布号 |
US4014484(A) |
申请公布日期 |
1977.03.29 |
申请号 |
US19750571863 |
申请日期 |
1975.04.25 |
申请人 |
SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE |
发明人 |
MOUILLE, RENE LOUIS |
分类号 |
B64C27/00;(IPC1-7):B64C27/00 |
主分类号 |
B64C27/00 |
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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