发明名称 Compressor and gas turbine engine with a plasma actuator
摘要 <p>A compression system is disclosed, the compression system comprising a rotor having a plurality of blades arranged around a centerline axis, each blade having a blade airfoil and a blade tip, and at least one plasma actuator located on a blade. Exemplary embodiments of a detection system for detecting an instability in a compression system rotor and a mitigation system comprising at least one plasma actuator mounted on a blade to facilitate the improvement of the stability of the rotor are disclosed.</p>
申请公布号 GB201011323(D0) 申请公布日期 2010.08.18
申请号 GB20100011323 申请日期 2008.12.23
申请人 GENERAL ELECTRIC COMPANY 发明人
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代理机构 代理人
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