发明名称 |
Microjet-based control system for cavity flows |
摘要 |
A dynamic cavity air flow system reduces the highly unsteady flow over exposed aircraft cavities by incorporating a series of microjets proximate the leading edge of a cavity. The microjets, which may articulate, issue a supersonic jet flow toward the rear or trailing edge of the cavity whenever the cavity is exposed during flight. The microjets receive the air for the flow from either a dedicated pressurized gas source aboard the aircraft or from bleed air taken from an engine of the aircraft. Appropriate sensors and controllers are provided for control of the system.
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申请公布号 |
US7213788(B1) |
申请公布日期 |
2007.05.08 |
申请号 |
US20050143103 |
申请日期 |
2005.06.01 |
申请人 |
FLORIDA STATE UNIVERSITY RESEARCH FOUNDATION |
发明人 |
ALVI FARRUKH S.;SHIH CHIANG;KROTHAPALLI ANJANEYULU |
分类号 |
B64C21/04 |
主分类号 |
B64C21/04 |
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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