发明名称 |
AEROSPACE VEHICLE YAW GENERATING SYSTEMS AND ASSOCIATED METHODS |
摘要 |
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system can further include a movable control surface coupled to the fuselage and extending generally in a horizontal plane. The control surface can be movable to a deflected position in which the control surface can be positioned to create a flow pattern proximate to the fuselage when the aerospace vehicle is located in a flow field. The flow pattern can be positioned to create a pressure differential between the first portion of the fuselage and the second portion of the fuselage. The first and second portions can be located so that the pressure differential produces a yawing moment on the aerospace vehicle.
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申请公布号 |
US2006284022(A1) |
申请公布日期 |
2006.12.21 |
申请号 |
US20050158198 |
申请日期 |
2005.06.21 |
申请人 |
HARRIGAN JEFFERY S;BEAUFRERE HENRY L |
发明人 |
HARRIGAN JEFFERY S.;BEAUFRERE HENRY L. |
分类号 |
B64C13/16;B64C3/58 |
主分类号 |
B64C13/16 |
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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