发明名称 Helicopter rotor
摘要 Helicopter rotor on which a number of blades are each connected to a perimetrical bridge element on a hub by means of a fork element extending round the said bridge element and connected to it by means of two elastomer supports, arranged in series, of which one is designed to dampen at least operation of the blade in the hub plane.
申请公布号 US4588356(A) 申请公布日期 1986.05.13
申请号 US19830558182 申请日期 1983.12.05
申请人 COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. 发明人 PARIANI, EMILIO
分类号 B64C27/32;B64C27/35;B64C27/48;B64C27/51;(IPC1-7):B64C27/35 主分类号 B64C27/32
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