CN106285946B - 双轴转动变形的通道无尖角内乘波式变几何进气道 - Google Patents
双轴转动变形的通道无尖角内乘波式变几何进气道 Download PDFInfo
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
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Families Citing this family (17)
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CN106837549B (zh) * | 2017-02-06 | 2018-07-17 | 厦门大学 | 内并联式高超声速双通道进气道的设计方法 |
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 |
CN107830986B (zh) * | 2017-11-29 | 2024-05-07 | 中国航空工业集团公司沈阳空气动力研究所 | 一种进气道模型流量调节机构 |
CN108194224B (zh) * | 2017-12-31 | 2019-08-27 | 厦门大学 | 埋入隔板内部的tbcc并联喷管调节机构设计方法 |
CN108717487A (zh) * | 2018-05-17 | 2018-10-30 | 中国航空发动机研究院 | 进气可调冲压发动机一体化流道优化设计方法 |
CN113420014A (zh) * | 2018-07-17 | 2021-09-21 | 北京洛必达科技有限公司 | 一种大数据的云计算数据处理方法 |
RU2020114996A (ru) * | 2019-06-12 | 2021-10-28 | Зе Боинг Компани | Входное устройство изменяемой геометрии с двумя наклонными элементами и компоновкой в виде графического знака вставки |
CN111075570A (zh) * | 2019-12-16 | 2020-04-28 | 北京动力机械研究所 | 一种几何可调流道伸缩补偿及动密封结构 |
CN113931747B (zh) * | 2020-06-29 | 2024-07-12 | 厦门大学 | 三维内转消膨胀波高性能双通道tbcc进气道设计方法 |
CN111797477B (zh) * | 2020-07-10 | 2023-05-23 | 南京航空航天大学 | 一种配合二元式超声速进气道的前掠前缘型侧板结构 |
CN112627983B (zh) * | 2020-12-25 | 2022-02-22 | 中国人民解放军国防科技大学 | 一种rbcc发动机内流道及rbcc发动机 |
CN113028449B (zh) * | 2021-02-26 | 2023-03-17 | 中国空气动力研究与发展中心设备设计与测试技术研究所 | 一种燃气发生器流线型燃料分流盘 |
CN113323756B (zh) * | 2021-06-22 | 2022-08-16 | 西安航天动力研究所 | 双流道分级可调宽范围进气道、发动机及进气调节方法 |
RU2766238C1 (ru) * | 2021-08-27 | 2022-02-10 | Федеральное Автономное Учреждение "Центральный институт авиационного моторостроения имени П.И. Баранова" | Воздухозаборник с изменяемой геометрией для сверхзвукового пассажирского летательного аппарата |
CN113915004B (zh) * | 2021-10-29 | 2023-02-03 | 南京航空航天大学 | Tbcc变几何进气道排除附面层与兼顾起动性能的侧板泄流槽 |
CN115217670B (zh) * | 2022-05-24 | 2024-04-26 | 中国民用航空飞行学院 | 一种三涵道超声速喷管构型的设计方法 |
CN117823281B (zh) * | 2024-03-06 | 2024-06-04 | 中国空气动力研究与发展中心空天技术研究所 | 一种品字形排列的多通道宽速域可调进气道 |
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US7216474B2 (en) * | 2004-02-19 | 2007-05-15 | Aerojet-General Corporation | Integrated air inlet system for multi-propulsion aircraft engines |
CN101418723B (zh) * | 2008-10-15 | 2010-06-02 | 南京航空航天大学 | 进出口形状可定制的内乘波式高超声速进气道及设计方法 |
CN201301752Y (zh) * | 2008-10-15 | 2009-09-02 | 南京航空航天大学 | 进出口形状可定制的内乘波式高超声速进气道 |
CN203958610U (zh) * | 2014-06-10 | 2014-11-26 | 厦门翔腾航空科技有限公司 | 双进气道高超声速乘波体飞行器装置 |
CN104632411B (zh) * | 2015-01-28 | 2016-08-24 | 南京航空航天大学 | 采用二元变几何方式的内乘波型涡轮基组合动力进气道 |
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Inventor after: Huang Guoping Inventor after: Huang Huihui Inventor after: Yu Zonghan Inventor after: Xia Chen Inventor after: Zuo Fengyuan Inventor after: Yue Ting Inventor after: Zhu Yu Inventor before: Huang Guoping Inventor before: Huang Huihui Inventor before: Xia Chen Inventor before: Zuo Fengyuan Inventor before: Yue Ting |