发明名称 |
ACTIVE FLOW CONTROL SYSTEM |
摘要 |
An aircraft is provided and includes a fuselage including a top and a tail, a main rotor apparatus disposed at the top of the fuselage, which rotates one or more rotors to generate lift, and an active flow control (AFC) system. The AFC system includes plasma actuators configured to generate plasma at a location adjacent to the main rotor apparatus and/or at the tail of the fuselage. |
申请公布号 |
WO2016126301(A2) |
申请公布日期 |
2016.08.11 |
申请号 |
WO2015US61600 |
申请日期 |
2015.11.19 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
WAKE, BRIAN E.;MATALANIS, CLAUDE G.;BOWLES, PATRICK |
分类号 |
B64C27/08 |
主分类号 |
B64C27/08 |
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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