发明名称 |
PLASMAAKTUATOREN ZUR WIDERSTANDSREDUZIERUNG AUF FLÜGELN, GONDELN UND/ODER RUMPF EINES SENKRECHT STARTENDEN ODER LANDENDEN FLUGZEUGS |
摘要 |
<p>An aircraft includes a surface over which an airflow passes. A plasma actuator (1) 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 |
AT512876(T) |
申请公布日期 |
2011.07.15 |
申请号 |
AT20060851273T |
申请日期 |
2006.08.17 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
WOOD, TOMMIE;CORKE, THOMAS;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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