| 发明名称 |
CANARD-LOCKED OBLIQUE WING AIRCRAFT |
| 摘要 |
An aircraft includes a fuselage, a main wing pivotally coupled to an aft portion of the fuselage, and a canard coupled to a forward portion of fuselage, wherein the main wing and the canard are configured to be connected together for supersonic flight and disconnected from each other for subsonic flight. |
| 申请公布号 |
EP2961652(B1) |
申请公布日期 |
2017.01.04 |
| 申请号 |
EP20140709508 |
申请日期 |
2014.02.25 |
| 申请人 |
Northrop Grumman Systems Corporation |
发明人 |
SOMMER, Geoffrey S.;COTE, Kenneth A. |
| 分类号 |
B64C3/40;B64C5/04;B64C30/00;B64C39/12 |
主分类号 |
B64C3/40 |
| 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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