INTEGRATED AIR INLET SYSTEM FOR MULTI-PROPULSION A

更新时间:2023-07-22 12:27:53 阅读: 评论:0

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描写祖国的句子专利名称:INTEGRATED AIR INLET SYSTEM FOR
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MULTI-PROPULSION AIRCRAFT ENGINES 发明人:BULMAN, Melvin, J.,BILLIG, Frederick, S.
申请号:EP05851149.4
申请日:20050216香蕉怎么炸
公开号:EP1718857A2
人事不知公开日:
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20061108
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专利内容由知识产权出版社提供
摘要:An air inlet duct for an air-breathing combined-cycle aircraft engines is internally divided into parate channels for low-speed and high-speed components of the engine, and contains one or more movable panels that are fully contained within the duct and pivotal between an open position in which incoming air is directed to both channels and a clod position in which all incoming air is directed to the channel leading to the high-speed engine. This integrated duct utilizes all incoming air at all stages of flight with no change in either the geometry of the air capture portion of the engine or the engine itlf, and no exposure of movable leading edges. The result is a minimum of shock waves and a high degree of efficiency in operation of the engine.
申请人:AEROJET-GENERAL CORPORATION
地址:P.O Box 13222 Sacramento, California 95813-6000 US
国籍:US
代理机构:Jacob, Reuben Ellis
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