发明申请
US20100224733A1 Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
有权
等离子致动器，用于在机翼，机舱和/或垂直起飞和着陆飞机机身上进行减阻
- 专利标题： Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
- 专利标题（中）： 等离子致动器，用于在机翼，机舱和/或垂直起飞和着陆飞机机身上进行减阻
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申请号： US11519770申请日： 2006-09-13
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公开(公告)号： US20100224733A1公开(公告)日： 2010-09-09
- 发明人: Tommie L. Wood , Thomas C. Corke , Martiqua Post
- 申请人： Tommie L. Wood , Thomas C. Corke , Martiqua Post
- 申请人地址： US TX Hurst
- 专利权人： BELL HELICOPTER TEXTRON INC.
- 当前专利权人： BELL HELICOPTER TEXTRON INC.
- 当前专利权人地址： US TX Hurst
- 主分类号： B64C21/00
- IPC分类号： B64C21/00
摘要：
An aircraft includes a surface over which an airflow passes. A plasma actuator is configured to generate a plasma above the surface, the plasma coupling a directed momentum into the air surrounding the surface to reduce separation of the airflow from the surface. A method of reducing separation of an airflow from a surface of an aircraft includes generating a plasma in air surrounding the surface at a position where the airflow would separate from the surface in the absence of the plasma.
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