空天技术

参考文献

[1]王嘉钰，颜力，安凯，等.高超声速飞行器不确定性多学科设计优化综述[J].空天技术，2022(6):1-11.

[2]Newman R W. Oxidation-resistant high-temperature materials[J]. Johns Hopkins APL Technical Digest,1993(14):24-28.

[3]Polezhaev Y. Will there or will there not be a hypersonic airplane?[J]. Journal of Engineering Physics and Thermophysics,2000,73(1):3-8.

[4]赵国柱.超燃冲压发动机碳氢燃料再生冷却流动传热研究与应用[D].西安：西北工业大学，2017.

[5]李新春.基于热电转换的超燃冲压发动机主动冷却系统方案研究[D].长沙：国防科技大学，2017.

[6]苗鹤洋.基于超临界二氧化碳循环的超燃冲压发动机热电转换系统研究[D].长沙：国防科技大学，2021.

[7]Qi Y K,Ma X F,Jiang P X,et al. Review on heat-topower conversion technologies for hypersonic vehicles[J]. Chinese Journal of Aeronautics, 2023, 37(5):148-179.

[8]刘鑫，曾宏刚，高飞，等.高马赫数飞机能源生成技术分析与展望[C].第六届中国航空科学技术大会，乌镇，2023-09-26.

[9]李昊炜，刘俞聪，甘健洲，等.高超声速飞行器冷电联供技术研究现状综述[J].飞航导弹，2021(12):63-68.

[10]Cheng K L,Qin J,Sun H C,et al. Performance assessment of an integrated power generation and refrigeration system on hypersonic vehicles[J]. Aerospace Science and Technology,2019,89:192-203.

[11]廖孟豪.美国空军SBIR/STTR计划透露高超声速飞机若干指标构想[J].飞航导弹，2015(8):3-6.

[12]黄彦平，刘旻昀，卓文彬，等.超临界二氧化碳核能动力系统的兴起和发展[J].原子能科学技术，2023,57(9):1665-1680.

[13]苗旺，鲍军江，张宁，等.利用LNG冷能水合物海水淡化-冷电联产系统[J].工程热物理学报，2023,44(6):1452-1458.

[14]尹航，王强，朱佳华，等.耦合光热发电储热-有机朗肯循环的先进绝热压缩空气储能系统热力学分析[J].储能科学与技术，2023,12(12):3749-3760.

[15]秦江，鲍文，于达任.基于碱金属朗肯循环的超燃冲压发动机热管理方法[C]. 2006年中国工程热物理学会工程热力学与能源利用学术研讨会，重庆，2006-10-01.

[16]Sforza P. Electric power generation onboard hypersonic aircraft[C]. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference,Denver,USA,2009-08-02.

[17]Bao W,Qin J,Zhou W,et al. Parametric performance analysis of multiple re-cooled cycle for hydrogen fueled scramjet[J]. International Journal of Hydrogen Energy,2009,34:7334-7341.

[18]Bao W, Qin J, Zhou W X, et al. Performance limit analysis of recooled cycle for regenerative cooling systems[J]. Energy Conversion and Management, 2009, 50(8):1908-1914.

[19]Qin J,Bao W,Zhou W X,et al. Flow and heat transfer characteristics in fuel cooling channels of a recooling cycle[J]. International Journal of Hydrogen Energy,2010,35:10589-10598.

[20]Qin J,Zhou W,Bao W,et al. Thermodynamic optimization for a scramjet with re-cooled cycle[J]. Acta Astronautica,2010,66:1449-1457.

[21]Qin J,Bao W,Zhang S L,et al. Comparison during a scramjet regenerative cooling and recooling cycle[J].Journal of Thermophysics and Heat Transfer, 2012,26:612-618.

[22]Bao W,Qin J,Zhou W X,et al. Power generation and heat sink improvement characteristics of recooling cycle for thermal cracked hydrocarbon fueled scramjet[J]. Science China Technological Sciences, 2011, 54(4):955-963.

[23]王邦运.基于朗肯循环的超燃冲压发动机新型冷却循环设计研究[D].长沙：国防科技大学，2021.

[24]孙红闯.基于空气涡轮和ORC的机载电冷联供系统研究[D].哈尔滨：哈尔滨工业大学，2021.

[25]周维国，祝朝阳，陈栓俊，等.超临界CO2布雷顿循环燃煤发电研究进展[J].现代化工，2023, 43(S2):80-85.

[26]Bao W, Qin J, Yu D R. Integrated thermal management method of energy based on closed Brayton cycle for scramjet[C]. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference,Sacramento,USA,2006-07-09.

[27]Qin J,Zhou W X,Bao W,et al. Thermodynamic analysis and parametric study of a closed Brayton cycle thermal management system for scramjet[J]. International Journal of Hydrogen Energy,2010,35(1):356-364.

[28]马喆，张兴娟，杨春信.高超声速飞行器热防护的布雷顿热电转化技术[J].战术导弹技术，2014(4):20-25.

[29]Cheng K L,Qin J,Dang C L,et al. Thermodynamic analysis for high-power electricity generation systems based on closed-Brayton-cycle with finite cold source on hypersonic vehicles[J]. International Journal of Hydrogen Energy,2018,43(31):14762-14774.

[30]Cheng K L,Qin J,Sun H C,et al. Performance assessment of a closed-recuperative-Brayton-cycle based integrated system for power generation and engine cooling of hypersonic vehicle[J]. Aerospace Science and Technology,2019,87:278-288.

[31]姜培学，张富珍，胥蕊娜，等.高超声速飞行器发动机热防护与发电一体化系统[J].航空动力学报，2021,36(1):1-7.

[32]Cheng K L,Wang Y L,Xu J,et al. A novel liquid metal MHD enhanced closed-Brayton-cycle power generation system for hypersonic vehicles:Thermodynamic analysis and performance evaluation with finite cold source[J]. Energy Conversion and Management,2022,268:116068.

[33]Wang Y,Cheng K,Xu J,et al. Coupling study of onboard power generation system of magnetohydrodynamics enhanced Brayton cycle[J]. Applied Thermal Engineering,2024,257:124250.

[34]Dang C L, Cheng K L, Fan J H, et al. Performance analysis of fuel vapor turbine and closed-Brayton-cycle combined power generation system for hypersonic vehicles[J]. Energy,2023,266:126426.

[35]Dang C,Cheng K,Xu J,et al. Performance analysis of a thermal management system based on hydrocarbonfuel regenerative cooling technology for scramjets[J]. Energy,2023,285:128720.

[36]Qi X, Zhou Z, Liu H, et al. Study on multi-heatsource thermal management of hypersonic vehicle based on SCO2 Brayton cycle[J]. Aerospace,2025,12(7):575.

[37]周林，孟凡凯，陈华伟，等.钎料层对热电模块力学性能的影响分析[J].工程力学，2023,42(6):1-11.

[38]陶佳霖，刘伟，李振明，等.基于LNG冷能利用的半导体温差发电性能试验研究[J].低温工程，2023(4):48-54+62.

[39]徐庆，赵琨鹏，魏天然，等.热电材料的研究现状与未来展望[J].硅酸盐学报，2021,49(7):1296-1305.

[40]Cheng K L,Feng Y,Lv C W,et al. Performance evaluation of waste heat recovery systems based on semiconductor thermoelectric generators for hypersonic vehicles[J]. Energies,2017,10(4):570.

[41]Jia X D,Fan S F,Zhang Z,et al. Performance assessment of thermoelectric generators with application on aerodynamic heat recovery[J]. Micromachines, 2021,12(11):1399.

[42]Qiao Y,Liu W,Pan Y,et al. Design and decoupling analysis of thermal-electric energy comprehensive utilization scheme based on“diamond” active cooling thermal protection system for hypersonic vehicle[J]. Energy,2024,294:130906.

[43]熊屠安，林尚超，何淼生，等.高超声速飞行器前缘气动热固态温差发电技术研究[J].航空动力学报，2026,41(4):148-157.

[44]Cheng K L,Qin J,Jiang Y G,et al. Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference[J].Applied Thermal Engineering, 2018, 130:1598-1609.

[45]李益文，张百灵，李应红，等.磁流体动力学在航空工程中的应用与展望[J].力学进展，2017,47(1):452-502.

[46]Li Y W,Li Y H,Lu H Y,et al. Preliminary experimental investigation on MHD power generation using seeded supersonic argon flow as working fluid[J]. Chinese Journal of Aeronautics,2011,24(6):701-708.

[47]Harada Nob,Takashi K. Numerical simulation for hypersonic vehicle on-board magnetohydrodynamic power generation[C]. 2008 IEEE 2nd International Power and Energy Conference,Johor Bahru,Malaysia,2008-11-30.

[48]Vatazhin A B,Gus’kov O V,Danilov M K,et al. Magnetogasdynamic generation of electrical energy in models of aircraft with a high-speed jet engine[J]. Fluid Dynamics,2009,44(4):612-620.

[49]黄浩，黄护林，张义宁，等.高超声速等截面磁流体发电机性能研究[J].航空动力学报，2013,28(3):573-582.

[50]李灏，黄护林，张义宁，等.高超声速飞行器尾喷管中磁流体发电机性能数值研究[J].推进技术，2023,44(8):160-172.

[51]刘琛源，武劭恂，孟皓.包括燃烧室后磁流体发电的超燃冲压发动机性能分析[J].推进技术，2025,46(8):15-28.

[52]张涛，杨文将，李晓东，等.超导磁体技术在航天推进领域的应用及技术问题[J].低温物理学报，2016,38(6):1-8.

[53]程昆林.基于冷源梯级利用的高超声速飞行器联合发电系统性能研究[D].哈尔滨：哈尔滨工业大学，2021.

[54]Al-Nimr M A,Dawahdeh A I,Abu Irshed A. An integrated alkali metal thermoelectric converter with sodium hydroxide thermoelectric water splitter and organic Rankine cycle for efficient power and hydrogen production[J]. Applied Thermal Engineering,2024,240:122257.

[55]Jia Y F,Sardari F. Study of employing a thermoelectric generator and an alkali metal thermal electric converter for waste heat recovery of a solid oxide fuel cell[J]. Alexandria Engineering Journal,2023,69:403-418.

[56]秦江，程昆林，鲍文，等.基于碱金属热电直接转换的高超声速飞行器冷却/发电系统：201511008984.9[P]. 2016-05-11.

[57]詹景坤，王小辉，蔡昱.热电转换技术在高超声速飞行器中的应用设想[J].电子测试，2018(4):27-29+19.

[58]石佳，张兴娟，李芳勇，等.高超声速飞行器气动热利用方法研究[J].战术导弹技术，2015(1):31-36.

[59]Twi-Yeboah N, Osei D, Danquah M K. Advances in solar-derived chemical fuel systems[J]. Energies,2023,16(6):2864.

[60]Pham T T, Mollaamin F, Monajjemi M, et al. A review of 2019 fuel cell technologies:Modelling and controlling[J]. International Journal of Nanotechnology,2020,17(7):498.

[61]Chen S G, Zhang H X, Yao C G, et al. Review of SOFC cathode performance enhancement by surface modifications:Recent advances and future directions[J].Energy&Fuels,2023,37(5):3470-3487.

[62]Wachsman E D,Lee K T. Lowering the temperature of solid oxide fuel cells[J]. Science,2011,334(6058):935-939.

[63]付全荣.固体氧化物燃料电池电堆性能退化研究与结构优化设计[D].大连：大连理工大学，2023.

[64]Singh M, Zappa D, Comini E. Solid oxide fuel cell:Decade of progress,future perspectives and challenges[J]. International Journal of Hydrogen Energy, 2021,46(54):27643-27674.

[65]Zhang W,Wei J,Yin F,et al. Recent advances in carbon-resistant anodes for solid oxide fuel cells[J]. Materials Chemistry Frontiers,2023,7(10):1943-1991.

[66]Ji Z X,Qin J,Cheng K L,et al. Comparative performance analysis of solid oxide fuel cell turbine-less jet engines for electric propulsion airplanes:Application of alternative fuel[J]. Aerospace Science and Technology,2019,93:105286.

[67]Giacoppo G, Barbera O, Briguglio N,et al. Thermal study of a SOFC system integration in a fuselage of a hybrid electric mini UAV[J]. International Journal of Hydrogen Energy,2017,42:28022-28033.

[68]Ji Z X,Qin J,Cheng K L,et al. Thermodynamics analysis of a turbojet engine integrated with a fuel cell and steam injection for high-speed flight[J]. Energy,2019,185:190-201.

[69]Litherland B L,Borer N K,Geuther S. A study on the use of solid-oxide fuel cells for increased power generation on small aircraft[C]. AIAA Aviation 2019 Forum,Dallas,USA,2019-06-17.

[70]刘禾，王静贻，秦江，等.燃料串/并联的航空SOFC-GT混合系统性能对比分析[J].推进技术，2024,45(3):116-126.

[71]李程镐，李成杰，郭发福，等.再生冷却与燃料电池发电一体化系统性能分析[C].第七届空天动力联合会议暨中国航天第三专业信息网第四十三届技术交流会，苏州，2023-05-10.

[72]Liu Y M,Tan J G,Zhang D D,et al. Modeling and performance analysis of solid oxide fuel cell power generation system for hypersonic vehicles[J]. Aerospace,2024,11(10):846.

[73]Kuai Z H,Zhang D D,Tan J G,et al. A comparative analysis of performance of solid oxide fuel cell-scramjet engine system for different reforming modes and fuels[J].Thermal Science and Engineering Progress,2025,62:103605.

[74]Li C H,Cheng K L,Li C J,et al. Performance assessment of pressurized SOFC power generation system for hypersonic vehicles:Thermodynamic analysis, system configuration optimization[J]. Energy, 2025, 315:134377.

[75]Kuai Z H,Zhang D D,Tan J G,et al. Effects of gas recirculation on the performance of solid oxide fuel cellbased auxiliary power system(SOFC-APS)[J]. Applied Thermal Engineering,2026,282:128855.

[76]Li X C,Wang Z W. Exergy analysis of integrated TEG and regenerative cooling system for power generation from the scramjet cooling heat[J]. Aerospace Science and Technology,2017,66:12-19.

[77]Li C H,Cheng K L,Li C J,et al. Performance analysis of multi turbines and SOFC combined power generation system for hypersonic vehicles[J]. Applied Thermal Engineering,2024,257:124461.

[78]曹学伟，王向盈，文哲希.超临界CO2布雷顿循环在高速飞行器中的应用可行性分析与展望[J].空天技术，2024(4):13-23+42.

[79]张昊春，张秀，刘秀婷，等.空间堆碱金属热电转换系统性能分析与优化[J].工程热物理学报，2020,41(2):277-284.

[80]Yang C, Li Y H. Fuel-saving performance and main losses of an organic-Rankine-cycle-based exhaust heat recovery system in heavy truck application scenarios[J].Applied Thermal Engineering,2021,193:117025.

[81]Leverone F, Pini M, Cervone A, et al. Solar energy harvesting on-board small satellites[J]. Renewable Energy,2020,159:954-972.

[82]Narasimhan A,Kamal R,Almatrafi E. Novel synergetic integration of supercritical carbon dioxide Brayton cycle and adsorption desalination[J]. Energy, 2022,238:121844.

[83]Li Z X,Li K,Guo X H,et al. Influence of timing between magnetic field and fluid flow in a rotary magnetic refrigerator[J]. Applied Thermal Engineering, 2021,187:116477.

[84]李辉.飞行器热电转换系统的分析与数值模拟[D].哈尔滨：哈尔滨工程大学，2024.

[85]彭一帆.针对SP-100空间堆设计的堆芯中子物理特性计算分析[D].上海：上海交通大学，2022.

[86]王志鹏，孙俊，石磊.采用磁流体发电的空间核反应堆系统效率分析[C].第十六届全国反应堆热工流体学术会议暨中核核反应堆热工水力技术重点实验室2019年学术年会，兰州，2019-11-06.

[87]秦江，姬志行，郭发福，等.航空用燃料电池及混合电推进系统发展综述[J].推进技术，2022,43(7):6-23.

[88]刘易明，王甫，王珺，等.燃料电池船舶应用形式及其关键技术[J].船舶工程，2021,43(3):18-26+33.

[89]阿嵘，庞丽萍，杨东升，等.高速飞行器机载综合热管理系统设计与优化[J].化工学报，2020, 71(S1):315-321.

[90]Karaduman N S, Karaduman Y, Ozdemir H, et al.Textile reinforced structural composites for advanced applications[M]. UK:IntechOpen,2017:116-117.

[91]张劲.整体叶盘叶片曲面的构建与拼接[D].武汉：华中科技大学，2020.

[92]赵巍，隋秀明，赵庆军，等.对转涡轮内部流动机理及设计方法研究[J].中国科学：技术科学，2020,50(10):1376-1390.

[93]廖文和，戴宁.航空航天结构轻量化设计制造技术发展现状与挑战[J].南京航空航天大学学报，2023,55(3):347-360.