发明名称 |
Stop-rotor rotary wing aircraft |
摘要 |
Systems and methods for transitioning an aircraft between helicopter and fixed wing flight modes are provided. In one embodiment, an aircraft comprises a plurality of wings each having a spar and a flap; a flap actuator configured to move the flap with respect to the spar; and a center section rotatably coupled to each spar. The center section includes at least one spar actuator configured to rotate at least one of the wings about a rotational axis of the spar when the aircraft transitions between helicopter and fixed wing flight modes.
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申请公布号 |
US2010230547(A1) |
申请公布日期 |
2010.09.16 |
申请号 |
US20090486023 |
申请日期 |
2009.06.17 |
申请人 |
THE GOVERNMENT OF THE US, AS REPRESENTED BY THE SECRETARY OF THE NAVY |
发明人 |
TAYMAN STEVEN K. |
分类号 |
B64C27/24 |
主分类号 |
B64C27/24 |
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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