| 发明名称 |
CONTROL SYSTEM AND STRATEGY FOR TAIL SITTER |
| 摘要 |
A tail sitter aircraft is capable of forward flight and hover operations. The tail sitter aircraft includes a wing and first and second prop-nacelles supportively disposed on the wing. Each of the first and second prop-nacelles includes an articulable rotor, which is rotatable about variable rotational axes and which includes blades that are collectively and cyclically controllable in both forward flight and hover regimes. |
| 申请公布号 |
US2017021924(A1) |
申请公布日期 |
2017.01.26 |
| 申请号 |
US201615158152 |
申请日期 |
2016.05.18 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Kubik Stephen;Driscoll Joseph T.;D'Anna Frank P.;Alber Mark R.;Lauder Timothy Fred;Fegely Cody |
| 分类号 |
B64C29/02;B64D29/02;B64D31/06;B64C15/12 |
主分类号 |
B64C29/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A tail sitter aircraft capable of forward flight and hover operations, comprising:
a wing; and first and second prop-nacelles supportively disposed on the wing, each of the first and second prop-nacelles including an articulable rotor, which is rotatable about variable rotational axes and which comprises blades that are collectively and cyclically controllable in both forward flight and hover regimes. |
| 地址 |
Straftford CT US |
