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 |
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代理人 |
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主权项 |
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地址 |
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