空天组合动力技术挑战及解决途径的思考

推进技术 ›› 2018, Vol. 39 ›› Issue (10): 2171-2176.

空天组合动力技术挑战及解决途径的思考

凌文辉^1,2,侯金丽¹,韦宝禧^1,2,冮强^1,2

北京动力机械研究所，北京 100074; 北京动力机械研究所高超声速冲压发动机技术重点实验室，北京 100074,北京动力机械研究所，北京 100074,北京动力机械研究所，北京 100074; 北京动力机械研究所高超声速冲压发动机技术重点实验室，北京 100074,北京动力机械研究所，北京 100074; 北京动力机械研究所高超声速冲压发动机技术重点实验室，北京 100074

发布日期:2021-08-15
作者简介:凌文辉，男，博士，研究员，研究领域为冲压发动机、空天组合动力技术。E-mail: lingwenhui@2008.sina.com 通讯作者:侯金丽，女，硕士，工程师，研究领域为空天组合动力技术。

Technical Challenge and Potential Solution for Aerospace Combined Cycle Engine

Beijing Power Machinery Institute，Beijing 100074，China; Science and Technology on Scramjet Laboratory，Beijing Power Machinery Institute，Beijing 100074，China,Beijing Power Machinery Institute，Beijing 100074，China,Beijing Power Machinery Institute，Beijing 100074，China; Science and Technology on Scramjet Laboratory，Beijing Power Machinery Institute，Beijing 100074，China and Beijing Power Machinery Institute，Beijing 100074，China; Science and Technology on Scramjet Laboratory，Beijing Power Machinery Institute，Beijing 100074，China

Published:2021-08-15

摘要/Abstract

摘要： 瞄准临近空间及空天飞行器对动力系统提出的水平起降、极宽速域和空域工作、综合油耗低、推重比高、重复使用易维护等极高要求，从力、热、域、效、智五个方面分析了空天组合动力面临的推力陷阱、高超声速下面临热力循环效率低及结构热防护难、宽域及跨域面临能否可靠工作、热力循环效率及推进效率等飞行效率优化难度高、多任务适应及多点设计最佳难度极高等技术挑战。在此基础上，综合研判国际技术发展趋势，分别给出了五个方面的技术解决途径建议。

关键词: 空天组合动力；技术挑战；解决途径

Abstract: Aim at extremely high needs of propulsion for aerospace vehicle，technical challenge for aerospace combined cycle engine on five aspects of thrust，heat，region，efficiency，and intelligence are analyzed，which mainly includes thrust gap，thermal protection difficult，reliable work for wide domain，flight efficiency optimization，the beat for multiple design point etc. After comprehensive study of international developing trend，some potential solutions have been encountered severally，which give references for investigation of aerospace combined cycle engine.

Key words: Aerospace combined cycle engine；Technical challenge；Potential solution

凌文辉,侯金丽,韦宝禧,冮强. 空天组合动力技术挑战及解决途径的思考[J]. 推进技术, 2018, 39(10): 2171-2176.

LING Wen-hui^1,2,HOU Jin-li¹,WEI Bao-xi^1,2,GANG Qiang^1,2. Technical Challenge and Potential Solution for Aerospace Combined Cycle Engine[J]. Journal of Propulsion Technology, 2018, 39(10): 2171-2176.

参考文献

[1] Thomas J Stueber. Combined Cycle Engine (CCE) Mode Transition[EB/OL]. http://www.nasa.gov,2012-10-25.
[2] Daniel A Haid, Eric J Gamble. Integrated Tutbine-Based Combined Cycle Dynamic Simulation Model[C]. Arlington: 58th JANNAF (JPM/CS/APS/EPSS/PHHS) Propulsion Meeting, 2011.
[3] Kevin Bowcutt, Dave Saunders, Jack Edwards. TBCC Dual-Inlet Mode Transition[C]. USA: National Center for Hypersonic Combined Cycle Propulsion, 2011.
[4] Foster L, Saunders J, Sanders B, et al. Highlights from a Mach 4 Experimental Demonstration of Inlet Mode Transition for Turbine-Based Combined Cycle Hypersonic Propulsion[R]. NASA/TM 2012-217724.
[5] Guy Norris. Exclusive: Skunk Works Reveals SR-71 Successor Plan[EB/OL]. http://www.aviationweek.com/Article.aspx?Id=/article-xml/awx_11_01_2013_p0-632731.xml, 2013-11-01.
[6] Roger Longstaff, Alan Bond. The SKYLON Project[R].AIAA 2011-2244.
[7] Murray J J, Guha A, Bond A. Overview of the Development of Heat Exchangers for Use in Air-Breathing Propulsion Pre-Coolers[J]. Acta Astronautica, 1997, 41(11): 723-729.
[8] Webber H, Taylor N. Tunnel Development for Heat Transfer Analysis in Compact Heat Exchangers[R]. AIAA 2010-4537.
[9] Liu W Q, Chen Q Z. Transpiration Cooling of Rocket Thrust Chamber with Liquid Oxygen[R]. AIAA 98-0890.
[10] Haidn O, Greuel D, Herbertz A, et al. Transpiration Cooling Applied to C/C Liners of Cryogenic Liquid Rocket Engines[R]. AIAA 2004-3682.
[11] Haeseler D, Madding C, Rubinskiy V, et al. Experimental Investigation of Transpiration Cooled Hydrogen-Oxygen Subscale Chambers[R]. AIAA 98-3364.
[12] Adam Siebenhaar, Thomas J Bogar. Integration and Vehicle Performance Assessment of the Aerojet“Trijet”Combined-Cycle Engine[R]. AIAA 2009-7420.
[13] HAN Qi-xiang, WANG Jia-hua, WANG Bo. Investigation of Detonative Combustion Characteristics[J]. Chinese Journal of Aeronautics, 2002, 15(2): 72-76.
[14] HAN Qi-xiang, WANG Jia-hua, WANG Bo. Investigation of Detonative Combustion Characteristics[J]. Chinese Journal of Aeronautics, 2002, 15(2): 72-76.
[15] Banerjee N, Long X, Du R, et al. Human-Supervised Control of the Atlas Humanoid Robot for Traversing Doors[C]. Seoul: IEEE-RAS International Conference on Humanoid Robots, 2015.
[16] Feng S, Xinjilefu X, Atkeson C G, et al. Optimization Based Controller Design and Implementation for the Atlas Robot in the DARPA Robotics Challenge Finals[C]. Seoul: IEEE-RAS International Conference on Humanoid Robots, 2015.
[17] FU Xiu-li, WANG Yong, PAN Yong-zhi, et al. Friction-Reducing, Anti-Wear and Self-Repairing Properties of Sulfonated Graphene[J]. Journal of Wuhan University of Technology(Materials Science), 2017, 32(2): 272-277.
[18] Pang J W C, Bond I P. “Bleeding Composites” -Damage Detection and Self-Repair Using a Biomimetic Approach[J] . Applied Science and Manufacturing, 2005, 36(2): 183-188.　　　　　　　　　　　　　*　收稿日期:2018-01-23；修订日期:2018-06-03。作者简介:凌文辉,男,博士,研究员,研究领域为冲压发动机、空天组合动力技术。E-mail: lingwenhui@2008.sina.com通讯作者:侯金丽,女,硕士,工程师,研究领域为空天组合动力技术。E-mail: houjinli618@126.com(编辑:朱立影)