发明名称 |
AIRCRAFT WING EXTENSION AND NOZZLE SYSTEM |
摘要 |
A system and method to control flight of an aircraft. The aircraft having an engine with a rotatably nozzle assembly configured to create forward propulsion and yaw control of the aircraft. The engine exhaust passing through the nozzle is redirected with a valve disposed within the nozzle. Lift is created with a lift system carried by the wing of the aircraft. Additional lift is created during flight with a retractable wing extension disposed within the fixed wing of the aircraft. |
申请公布号 |
CA2757553(C) |
申请公布日期 |
2015.03.31 |
申请号 |
CA20112757553 |
申请日期 |
2011.11.08 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
ROBERTSON, DANIEL B.;GRONINGA, KIRK L. |
分类号 |
B64C3/54;B64D33/04 |
主分类号 |
B64C3/54 |
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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