发明名称 |
Aircraft with forward opening inlay spoilers for yaw control |
摘要 |
An aircraft comprises first and second wings positioned on opposite sides of a longitudinal axis with each of the first and second wings including an upper surface and a lower surface, wherein no control surfaces are attached to the lower surface of the wings. A first forward opening control surface is attached by a first hinge to an upper surface of the first wing and a second forward opening control surface being attached by a second hinge to an upper surface of the second wing. Each of the first and second hinges is canted with respect to a direction perpendicular to the longitudinal axis. A method of yaw control performed by the aircraft is also included.
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申请公布号 |
US2006102802(A1) |
申请公布日期 |
2006.05.18 |
申请号 |
US20040023949 |
申请日期 |
2004.12.28 |
申请人 |
NORTHROP GRUMMAN CORPORATION |
发明人 |
CLARK WALTER D. |
分类号 |
B64C3/58;B64C1/00;B64C5/08;B64C9/32;B64C39/10;B64D7/00 |
主分类号 |
B64C3/58 |
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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