发明名称 |
HELICOPTER DEICER SYSTEM POWER TRANSFER ASSEMBLY |
摘要 |
<p>A device (10) for isolating from vibrational and impulse loads a power transfer unit (14) that transfers power from a helicopter electrical system to a plurality of deicing segments on the rotor blades includes a distributor (13) rotating with the rotor blades for distributing power from the power transfer unit (14) to the deicing segments, a housing (11) having an upper cylinder (24) and lower cylinder (23) the latter of which is flexibly secured to the helicopter as by a joint including ball (40),housing 11 substantially isolating the power transfer unit (14) from such loads, and a shaft (12) rotatably engaging the upper cylinder (24) for carrying the distributor (13) in rotation with the rotor blades.</p> |
申请公布号 |
CA1195308(A) |
申请公布日期 |
1985.10.15 |
申请号 |
CA19820406312 |
申请日期 |
1982.06.29 |
申请人 |
GOODRICH(B.F.) COMPANY (THE) |
发明人 |
ADAMS, LOWELL J.;SWEET, DAVID B. |
分类号 |
B64D15/12;(IPC1-7):B64D15/12 |
主分类号 |
B64D15/12 |
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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