| 发明名称 |
Control surface for an aircraft |
| 摘要 |
A control surface (152) for an aircraft has a reinforced elastomer surface (154) on a surface of the aircraft and has a perimeter (156) attached to the aircraft. An actuation mechanism (160) moves the reinforced elastomer surface (154) from a first position, substantially conforming to a moldline of the aircraft, to a second position, protruding from the moldline of the aircraft.
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| 申请公布号 |
US2001006207(A1) |
申请公布日期 |
2001.07.05 |
| 申请号 |
US20010784771 |
申请日期 |
2001.02.15 |
| 申请人 |
CATON JOHN HAROLD;HOBEY MICHAEL JAMES;GROENEVELD JOHN DAVID;JACOBS JACK HOWARD;WILLE ROBERT HENRY;BRASE LAWRENCE OTTO |
发明人 |
CATON JOHN HAROLD;HOBEY MICHAEL JAMES;GROENEVELD JOHN DAVID;JACOBS JACK HOWARD;WILLE ROBERT HENRY;BRASE LAWRENCE OTTO |
| 分类号 |
B64C9/02;B64C27/615;(IPC1-7):B64C3/58 |
主分类号 |
B64C9/02 |
| 代理机构 |
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代理人 |
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