发明名称 |
PLASMA ACTUATORS FOR DRAG REDUCTION ON WINGS, NACELLES AND/OR FUSELAGE OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
摘要 |
<p>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.</p> |
申请公布号 |
KR20080058405(A) |
申请公布日期 |
2008.06.25 |
申请号 |
KR20087009113 |
申请日期 |
2008.04.16 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
WOOD TOMMIE;CORKE THOMAS C.;POST MARTIQUA |
分类号 |
B64C23/00;B64C21/00 |
主分类号 |
B64C23/00 |
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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