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
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