发明授权
- 专利标题: Forebody nozzle for aircraft directional control
- 专利标题(中): 前身喷嘴用于飞机方向控制
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申请号: US970747申请日: 1992-11-02
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公开(公告)号: US5273237A公开(公告)日: 1993-12-28
- 发明人: Robert W. Guyton , Jon A. Tinapple , Kenneth C. Cornelius
- 申请人: Robert W. Guyton , Jon A. Tinapple , Kenneth C. Cornelius
- 申请人地址: DC Washington
- 专利权人: The United States of America as represented by the Secretary of the Air Force
- 当前专利权人: The United States of America as represented by the Secretary of the Air Force
- 当前专利权人地址: DC Washington
- 主分类号: B64C15/14
- IPC分类号: B64C15/14 ; F41G7/00 ; F42B10/60
摘要:
A system for augmenting yaw control in an aircraft is described which comprises first and second thrust nozzles disposed on the upper surface of the aircraft forebody aft of the forebody nose apex a distance of about 0.5 times the forebody diameter at about 45.degree. to either side of the symmetry plane of the forebody, each thrust nozzle oriented to direct a fluid jet at an angle of about 10.degree. from the surface of the forebody and generally rearwardly toward the symmetry plane at about 60.degree. .+-.10.degree. to the symmetry plane, and a source of pressurized fluid operatively connected to the thrust nozzles for generating the jets.
公开/授权文献
- US5899922A Manipulation of nervous systems by electric fields 公开/授权日:1999-05-04