CN109915263B - 用于组合发动机的轴对称双模态进气道及模态切换方法 - Google Patents
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CN110793062A (zh) * | 2019-10-30 | 2020-02-14 | 北京空天技术研究所 | 采用中心燃烧的超燃冲压发动机流道构型及超燃冲压发动机 |
CN111255569B (zh) * | 2020-01-13 | 2021-06-22 | 南京航空航天大学 | 一种模态转换联合变几何调节的内并联型进气道及控制方法 |
CN111692013A (zh) * | 2020-07-03 | 2020-09-22 | 南京航空航天大学 | 一种轴对称内并联涡轮基旋转爆震冲压组合发动机及控制方法 |
CN112627981B (zh) * | 2020-11-18 | 2022-06-28 | 南京航空航天大学 | 一种用于rbcc发动机的轴对称内并联式双模态进气道及控制方法 |
CN114837811A (zh) * | 2022-04-19 | 2022-08-02 | 南京航空航天大学 | 一种延伸外机匣的组合动力模态转换方法 |
CN116902210B (zh) * | 2023-09-13 | 2023-12-05 | 中国航空工业集团公司金城南京机电液压工程研究中心 | 一种飞机机载系统的供能方法及装置 |
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CN102155331A (zh) * | 2011-05-05 | 2011-08-17 | 西北工业大学 | 一种基于爆震燃烧的涡轮冲压组合发动机 |
CN105156228A (zh) * | 2015-09-29 | 2015-12-16 | 清华大学 | 一种引射辅助式涡轮冲压组合循环发动机 |
CN106050472A (zh) * | 2016-07-08 | 2016-10-26 | 西北工业大学 | 涡轮火箭组合冲压发动机及其工作方法 |
CN107448296B (zh) * | 2017-08-07 | 2018-08-31 | 南京航空航天大学 | 气动式/机械式组合调节的马赫数0-7级组合发动机进气道 |
CN109236472B (zh) * | 2018-11-27 | 2019-08-16 | 北京航空航天大学 | 一种适应宽广马赫数飞行的轴对称变几何双模态进气道 |
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Inventor after: Zhang Yue Inventor after: Wang Ziyun Inventor after: Chen Liang Inventor after: Tan Huijun Inventor after: Wang Chao Inventor after: Lin Zhengkang Inventor before: Zhang Yue Inventor before: Wang Ziyun Inventor before: Tan Huijun Inventor before: Chen Liang Inventor before: Wang Chao Inventor before: Lin Zhengkang |
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