发明名称 Rotary-wing aircraft rotor head having resilient-return interblade ties with built-in damping
摘要 The invention relates to a rotor head having interblade ties with resilient return in lag and with built-in damping, wherein each tie is connected, to each of the two rotor blades joined by it, by articulation means comprising a main ball retained on a member connecting a blade to the hub and centered on or in immediate proximity to the pitch change axis of the corresponding blade. A single main ball may be connected to the adjacent ends of two neighboring ties by a connection member having the shape of a V open towards the hub, or else each tie is connected to a connection member by a respective one of two main balls offset transversely in relation to the pitch change axis of the blade and/or radially along said axis. Application to the main and/or auxiliary rotors of helicopters.
申请公布号 US4915585(A) 申请公布日期 1990.04.10
申请号 US19890343305 申请日期 1989.04.26
申请人 AEROSPATIALE SOCIETE NATIONAL INDUSTRIELLE 发明人 GUIMBAL, BRUNO
分类号 B64C27/35;B64C27/51 主分类号 B64C27/35
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