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公开(公告)号:US20200070996A1
公开(公告)日:2020-03-05
申请号:US16120676
申请日:2018-09-04
摘要: A pusher rotorcraft is provided in one example embodiment and may include at least one engine in mechanical communication with a drop-down gearbox; a driveshaft in mechanical communication with the drop-down gearbox, a main rotor gearbox, and a tail system gearbox; a main rotor system in mechanical communication with the main rotor gearbox; an anti-torque system in mechanical communication with the tail system gearbox; and a pusher propeller system in mechanical communication with the tail system gearbox.
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公开(公告)号:US20180327086A1
公开(公告)日:2018-11-15
申请号:US15594588
申请日:2017-05-13
IPC分类号: B64C27/32 , B64C27/605 , B64C29/00 , B64C27/06 , F16C19/06
CPC分类号: B64C27/32 , B64C27/06 , B64C27/605 , B64C29/0033 , F16C19/06 , F16C2326/43
摘要: An aircraft rotor assembly has a yoke with at least two arms extending therefrom. The yoke is attached to a mast through a constant-velocity joint, thereby permitting axial tilt of the yoke relative to the mast. Each arm of the yoke includes an axisymmetric elastomeric bearing with a spherical central member and two opposite partially-spherical members attached to the central member. Each axisymmetric bearing cooperates with a cup and a bracket. Each cup is attached to one of the yoke arms and each bracket is attached to a blade cuff.
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