发明名称 Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators
摘要 Dielectric barrier discharge plasma actuators are used to manipulate exhaust flow within and behind a jet engine nozzle. The dielectric barrier discharge plasma actuators may be used to direct cooling airflow near the surface of the nozzle to reduce heating of the nozzle, create thrust vectoring, and reduce noise associated with the exhaust flow exiting the nozzle.
申请公布号 US8453457(B2) 申请公布日期 2013.06.04
申请号 US20090547635 申请日期 2009.08.26
申请人 GINN KERRY B.;JENKINS STEWART A.;WELLS DAVID M.;MCCALLUM BRENT N.;LOCKHEED MARTIN CORPORATION 发明人 GINN KERRY B.;JENKINS STEWART A.;WELLS DAVID M.;MCCALLUM BRENT N.
分类号 F02K1/46 主分类号 F02K1/46
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