发明名称 Helicopter rotor
摘要 Rotary-wing aircraft rotor comprising a rigid hub coupled to the root of each blade in which a trailing return brace comprises a stack of metal plates alternating with plates of visco-elastic material the ends of which being coupled via a ball joint respectively to the root of one blade and to a place of the hub such that the brace is always slightly inclined.
申请公布号 US4407633(A) 申请公布日期 1983.10.04
申请号 US19810300091 申请日期 1981.09.08
申请人 SOCIETE NATIONALE INDUSTRIELLE AERO. 发明人 MOUILLE, RENE L.
分类号 B64C27/32;B64C27/35;B64C27/51;(IPC1-7):B64C27/38 主分类号 B64C27/32
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