发明名称 Rotor hub for a rotorcraft
摘要 A rotor hub (103) can include a yoke (211), a mast (201), and one or more radially oriented actuators (207a-207d). The first radial actuator and the second radial actuator each have a piston configured to impart a translation of the yoke (211) relative to the mast (201). The radial actuators (207a-207d) are configured to attenuate in-plane whirling vibrations. The rotor hub (103) can also have actuators (209a-209d) coupled between the mast (201) and the yoke (211) for attenuating flapping and vertical vibrations.
申请公布号 EP2886455(A1) 申请公布日期 2015.06.24
申请号 EP20140176752 申请日期 2014.07.11
申请人 BELL HELICOPTER TEXTRON INC. 发明人 FOSKEY, CHRISTOPHER;SUTTON, DREW;STAMPS, FRANK B.
分类号 B64C27/00 主分类号 B64C27/00
代理机构 代理人
主权项
地址