发明名称 Pitch control swash plates of helicopter rotor blades
摘要 The rotating (14) and non-rotating (16) stars are guided axially (Z-Z) and to tilt on this axis by non-rotating axial guides columns (28) and slides (33). One of two runners (38) carrying two diametrically opposite trunnions (41) slide on the slides. The runners allow pivoting of the non-rotating star around a diametral axis (X-X) whereas the sliding of the runners on the slides guides the pivoting of the non-rotating star around a second diametral axis (Y-Y) perpendicular to the other axes. This second axis is the axis of the cylindrical face (37) of the slides.
申请公布号 FR2771708(A1) 申请公布日期 1999.06.04
申请号 FR19970015218 申请日期 1997.12.03
申请人 EUROCOPTER FRANCE 发明人 RAMPAL ETIENNE JEAN;GARCIN SYLVIE JACQUELINE
分类号 B64C27/605;(IPC1-7):B64C27/605 主分类号 B64C27/605
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