发明名称 ROTOCRAFT ROTOR INCLUDING A FLAPPING ABUTMENT MECHANISM FOR BLADES HINGED ON A HUB OF THE ROTOR
摘要 An abutment mechanism for limiting the flapping of the blades of a rotor (1). High abutment members (6) can be moved into an engagement position by return means (13) exerting an intrinsic return force (R), and into a disengagement position by a flyweight (10) exerting a centrifugal force (C) under the effect of the rotor (1) rotating. At least one magnetic type bistable latch (15) is in selective engagement with the high abutment members (6). When the rotor (1) is stationary and while it is starting to rotate, an engagement latch (15) engages with the high abutment member (6) to prevent it passing from the engagement position towards the disengagement position. At a predetermined centrifugal force threshold, the engagement of the engagement latch (15) with the high abutment member (6) is broken, and the high abutment member (6) quickly passes into the disengagement position.
申请公布号 US2013149149(A1) 申请公布日期 2013.06.13
申请号 US201213693192 申请日期 2012.12.04
申请人 EUROCOPTER;EUROCOPTER 发明人 MONDET JEAN
分类号 B64C27/57 主分类号 B64C27/57
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