发明名称 |
SISTEMA PARA FLUJOS AERODINAMICOS Y METODO ASOCIADO. |
摘要 |
A system and method for controlling boundary layer flow over an aircraft wing are provided. The system includes at least one wing element, and a plurality of ports defined in the wing element and in fluid communication with one another. The system also includes at least one fluidic device operable to continuously ingest the fluid through at least one of the ports and eject the fluid out of at least one other port to control boundary layer flow of the fluid over the wing element.
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申请公布号 |
ES2357219(T3) |
申请公布日期 |
2011.04.20 |
申请号 |
ES20060788625T |
申请日期 |
2006.07.26 |
申请人 |
THE BOEING COMPANY |
发明人 |
SHMILOVICH, ARVIN;YADLIN, YORAM;CLARK, ROGER;MANLEY, DAVID |
分类号 |
B64C21/02 |
主分类号 |
B64C21/02 |
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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