发明名称 |
Flow control device and method of controlling flow |
摘要 |
The present invention relates to a flow control device and more particularly to reactive self-contained modular flow control device with deployable flow effectors. The present invention further relates to a method of operating the flow control device. One embodiment of the present invention includes a method of controlling air flow across a surface of an aircraft under certain flight conditions comprising the steps of sensing fluid separation from the surface by measuring the pressure on the surface; determining a standard deviation of the pressure measurements over a period of time; and deploying a flow effector in response to the standard deviation of the pressure measurements exceeding a predetermined threshold number.
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申请公布号 |
US7334760(B1) |
申请公布日期 |
2008.02.26 |
申请号 |
US20060523161 |
申请日期 |
2006.09.19 |
申请人 |
ORBITAL RESEARCH INC. |
发明人 |
LISY FREDERICK J.;MODARRESZADAH MOHAMMED;PATEL MEHUL P.;DICOCCO JACK M.;CARVER REED;SCHMIDT ROBERT N.;PRINCE TROY |
分类号 |
B64C13/16;B64C23/06 |
主分类号 |
B64C13/16 |
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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