发明名称 Integrater hub-mast and gyroplane rotor head comprising it
摘要 The invention provides an integrated hub-mast with a single piece tubular body which supports, by its hub body part (3), a reinforcing girdle (6) on each side of which openings (10, 11) are formed. For each blade of the rotor a retaining and pivoting member (13), formed preferably by a spherical stratified stop, is fixed to the girdle (6) and is retained in the hub body (3), and this member (13) is also fixed between the ends inside the hub body (3), of the lower (20) and upper (21) branches of a forked fastening part (19) connecting the blade to this member (13), these branches passing through the openings (10, 11) of a corresponding pair of openings. A heel (23) fixed under the lower branch (20) bears against a reciprocal ring (24) mounted on a support (29) in the hub-mast (1), which has external fastenings for coupling to resilient return and drag damping members of the blades.
申请公布号 US4749339(A) 申请公布日期 1988.06.07
申请号 US19860885997 申请日期 1986.07.16
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 MOUILLE, RENE L.;LEMAN, JEAN-LUC
分类号 B64C27/35;B64C27/32;(IPC1-7):B64C27/38 主分类号 B64C27/35
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