Exclusive: Advanced Combined Cycle Powered Vehicle

Research progress of pre-cooled air-breathing combined engines and analysis of the key technology

  • MA Xiaoqiu
Expand
  • Beijing Aerospace Propulsion Institute, Beijing 100076, China

Received date: 2019-10-10

  Revised date: 2020-03-19

  Online published: 2020-08-05

Abstract

Based on an analysis of the characteristics of pre-cooled air-breathing combined engine, the research progress of five types of engines in the world are summarized. Key techniques, advantages and disadvantages of the engines are also analyzed and discussed. Finally a proposal for future development of the engine is presented.

Cite this article

MA Xiaoqiu . Research progress of pre-cooled air-breathing combined engines and analysis of the key technology[J]. Science & Technology Review, 2020 , 38(12) : 85 -95 . DOI: 10.3981/j.issn.1000-7857.2020.12.007

References

[1] Peter W M. Mach 3 legend:Design and development of the lockheed blackbird[R]. Edwards:NASA Dryden Flight Research Center, 2012.
[2] Peter W M. Design and development of the blackbird:challenges and lessons learned[C]//47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando:AIAA, 2009.
[3] Richard V, Alan B. A comparison of propulsion concepts for SSTO reusable launchers[J]. JBIS, 2003, 56:108-117.
[4] Maita M, Miyajima H, Mori T. System studies on space plane powered by scram/LACE propulsion system[C]//AIAA Fourth International Aerospace Planes Conference. Orlando:AIAA, 1992.
[5] Webber H, Feast S, Bond A. Heat exchanger design in combined cycle engines[J]. Journal of the British Interplanetary Society, 2009, 62(4):122-130.
[6] Parkinson R, Conchie P. HOTOL[C]//AIAA 2nd International Aerospace Planes Conference. Orlando:AIAA, 1990.
[7] 孙广勃. 霍托尔的发动机揭秘[J]. 中国航天, 1994(1):37-41.
[8] Sato T, Kobayashi H, Tanatsugu N. Development study of the precooler of ATREX engine[C]//12th AIAA International Space Planes and Hypersonic Systems and Technologies. Norfolk:AIAA, 2003.
[9] Isomura K, Omi J. A Comparative Study of an ATREX Engine and a Turbo Jet Engine[C]//37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Utah:AIAA, 2001.
[10] Kojima T, Taguchi H, Kobayashi H, et al. Design and fabrication of variable nozzle for precooled turbojet engine[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen:AIAA, 2009.
[11] Longstaff R, Bond A. The Skylon Project[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco:AIAA, 2011.
[12] Varvill R. Heat exchanger development at reaction engines ltd[C]//59th International Astronautical Congress. Glasgow:International Astronautical Federation, 2008.
[13] Hempsell M. Progress on SKYLON and SABRE[C]//64th International Astronautical Congress. Beijing:IAC, 2013.
[14] Bartha J E, Webbera H. SABRE technology development[R]. Guadalajara:IAC, 2016.
[15] Jivraj F, Varvill R, Paniagua A B G. The scimitar precooled Mach 5 engine[C]//2nd European Conference for Aerospace Sciences. Brussels:EUCASS, 2007.
[16] 聂万胜, 周思引, 雷旭. 协同吸气式火箭发动机研究进展[J]. 装备学院学报, 2016, 27(6):57-64.
[17] 玉选斐, 王聪, 秦江, 等. 预冷吸气式发动机热力循环分析[J]. 工程热物理学报, 2018, 39(1):31-36.
[18] 邓帆, 谭慧俊, 董昊, 等. 预冷组合动力高超声速空天飞机关键技术研究进展[J]. 推进技术, 2018, 39(1):1-13.
[19] 郭海波, 肖洪, 南向谊, 等. 复合预冷吸气式火箭发动机热力循环分析[J]. 火箭推进, 2013, 39(3):15-20.
[20] 邹正平, 刘火星, 唐海龙, 等. 高超声速航空发动机强预冷技术研究[J]. 航空学报, 2015, 36(8):2544-2562.
[21] 张友法, 张文文, 郑日恒, 等. 高超声速组合发动机预冷器抗结霜涂层技术研究[J]. 推进技术, 2017, 38(2):463-470.
Outlines

/