ZHU Bingjie , YANG Xixiang , ZONG Jian'an , DENG Xiaolong . Review of distributed hybrid electric propulsion aircraft technology[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022 , 43(7) : 25556 -025556 . DOI: 10.7527/S1000-6893.2021.25556

[1] FRIEDRICH C, ROBERTSON P A. Design of hybrid-electric propulsion systems for light aircraft[C]//14th AIAA Aviation Technology, Integration, and Operations Conference. Reston:AIAA, 2014:3008.
[2] OELBERG E. A hybrid optimal control approach to maximum endurance of aircraft[D]. Montreal:Concordia University, 2018:1-28.
[3] 石伟兴,刘培志,王晋华,等.一种油电混合动力多旋翼性能的计算方法[C]//第十二届全国信号和智能信息处理与应用学术会议论文集.北京:中国兵器工业计算机应用技术研究所, 2018:56-60. SHI W X, LIU P Z, WANG J H, et al. Calculate the performance of multi-rotor UAV[C]//The 12th National Conference on Signal and Intelligent Information Processing and Application. Beijing:North Institute of computer Application, 2018:56-60(in Chinese).
[4] 李延平.太阳能/氢能混合动力小型无人机总体设计[D].北京:北京理工大学, 2014:1-21. LI Y P. Conceptual design for solar/hydrogen hybrid powered small-scale UAV[D]. Beijing:Beijing Institute of Technology, 2014:1-21(in Chinese).
[5] FREDERICKS W J, MCSWAIN R G, BEATON B F, et al. Greased lightning (GL-10) flight testing campaign:NASA/TM-2017-219643[R]. Washington,D.C.:NASA, 2017.
[6] RIGHI H. Hybrid electric aircraft[D]. Mississippi:Mississippi State University, 2016:1-21.
[7] SAEED A S, YOUNES A B, ISLAM S, et al. A review on the platform design, dynamic modeling and control of hybrid UAVs[C]//2015 International Conference on Unmanned Aircraft Systems (ICUAS). Piscataway:IEEE Press, 2015:806-815.
[8] FINGER D F, BRAUN C, BIL C. A review of configuration design for distributed propulsion transitioning VTOL aircraft[C]//2017 ASIA-Pacific International Symposium on Aerospace Technology, 2017:1-15.
[9] SILVAS E, HOFMAN T, MURGOVSKI N, et al. Review of optimization strategies for system-level design in hybrid electric vehicles[J]. IEEE Transactions on Vehicular Technology, 2017, 66(1):57-70.
[10] 王元元.全球电动飞机发展概览[EB/OL].(2020-02-06)[2021-03-15]. http://www.360doc.com/content/21/0926/05/43397137_997123897.shtml. WANG Y Y. Overview of global electric aircraft development[EB/OL].(2020-02-06)[2021-03-15]. http://www.360doc.com/content/21/0926/05/43397137_997-123897.shtml (in Chinese).
[11] 李开省.电动飞机核心技术研究综述[J].航空科学技术, 2019, 30(11):8-17. LI K S. Summary of research on core technology of electric aircraft[J]. Aeronautical Science&Technology, 2019, 30(11):8-17(in Chinese).
[12] PORNET C, ISIKVEREN A T. Conceptual design of hybrid-electric transport aircraft[J]. Progress in Aerospace Sciences, 2015, 79:114-135.
[13] 美国"空中飞的"项目获1亿美元融资[EB/OL].(2018-03-06)[2021-03-15]. https://baijiahao.baidu.com/s?id=1594162323581888682&wfr=spider&for=pc.
[14] Kittyhawk Cora[EB/OL].(2018-03-01)[2021-03-15]. https://kittyhawk.aero/wp-content/uploads/2018/03/core_tile_KH-630x374.jpg.
[15] 金泽.波音公司完成自主客运飞机首飞[EB/OL].(2019-01-25)[2021-03-15]. https://www.youuav.com/news/detail/201901/29031.html JIN Z. Boeing has completed the first flight of an autonomous passenger plane[EB/OL].(2019-01-25)[2021-03-15]. https://www.youuav.com/news/detail/201901/29031.html (in Chinese).
[16] HARRINGTON J D, KAMLET M, KATHY B. NASA's X-57 electric research plane[R].Washington,D.C.:NASA, 2016.
[17] THAMM F P, BRIEGER N, NEITZKE K P, et al. Songbird-an innovativeuas combining the advantages of fixed wing and multi rotor uas[J]. The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, 2015, XL-1/W4:345-349.
[18] KREIMEIER M, STUMPF E. Benefit evaluation of hybrid electric propulsion concepts for CS-23 aircraft[J]. CEAS Aeronautical Journal, 2017, 8(4):691-704.
[19] KIM H D, BROWN G V, FELDER J L. Distributed turboelectric propulsion for hybrid wing body aircraft[C]//2008 International Powered Lift Conference, 2008:1-11.
[20] 孔祥浩,张卓然,陆嘉伟,等.分布式电推进飞机电力系统研究综述[J].航空学报, 2018, 39(1):021651. KONG X H, ZHANG Z R, LU J W, et al. Review of electric power system of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1):021651(in Chinese).
[21] DAE KIM H, FELDER J L, TONG M T, et al. Turboelectric distributed propulsion benefits on the N3-X vehicle[J]. Aircraft Engineering and Aerospace Technology, 2014, 86(6):558-561.
[22] YOON S, LEE H C, PULLIAM T H. Computational analysis of multi-rotor flows[C]//54th AIAA Aerospace Sciences Meeting. Reston:AIAA, 2016.
[23] LEI G, WANG T S, ZHU J G, et al. System-level design optimization method for electrical drive systems-robust approach[J]. IEEE Transactions on Industrial Electronics, 2015, 62(8):4702-4713.
[24] DIEKMANN J H, HAHN K U. Effect of an active high-lift system failure during landing approaches[J]. CEAS Aeronautical Journal, 2015, 6(2):181-196.
[25] 毛鞠盛,王云,宗剑.通用飞机油电混合动力系统设计与陆上性能仿真[J].国际航空航天科学, 2016, 4(2):41-48. MAO J S, WANG Y, ZONG J. Design and simulation performance on land for general aircraft oil-electric hybrid system[J]. International Journalof Aerospace Science and Technology 2016, 4(2):41-48(in Chinese).
[26] HUNG J Y, GONZALEZ L F. On parallel hybrid-electric propulsion system for unmanned aerial vehicles[J]. Progress in Aerospace Sciences, 2012, 51:1-17.
[27] LORENZ L, SEITZ A, KUHN H. Hybrid power trains for future mo-bility[C]//Deutscher Luft-und Raumfahrtkongress, 2013:1-17.
[28] ISIKVEREN A T, KAISER S, PORNET C, et al. Pre-design strategies and sizing techniques for dual-energy aircraft[J]. Aircraft Engineering and Aerospace Technology, 2014, 86(6):525-542.
[29] FRIEDRICH C, ROBERTSON P A. Hybrid-electric propulsion for aircraft[J]. Journal of Aircraft, 2014, 52(1):176-189.
[30] PORNET C, KAISER S, ISIKVEREN A T, et al. Integrated fuel-battery hybrid for a narrow-body sized transport aircraft[J]. Aircraft Engineering and Aerospace Technology, 2014, 86(6):568-574.
[31] FINGER D F, BRAUN C, BIL C. Case studies in initial sizing for hybrid-electric general aviation aircraft[C]//2018 AIAA/IEEE Electric Aircraft Technologies Symposium. Reston:AIAA, 2018:5005.
[32] DE VRIES R, BROWN M, VOS R. Preliminary sizing method for hybrid-electric distributed-propulsion aircraft[J]. Journal of Aircraft, 2019, 56(6):2172-2188.
[33] 刘莉,杜孟尧,张晓辉,等.太阳能/氢能无人机总体设计与能源管理策略研究[J].航空学报, 2016, 37(1):144-162. LIU L, DU M Y, ZHANG X H, et al. Conceptual design and energy management strategy for UAV with hybrid solar and hydrogen energy[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1):144-162(in Chinese).
[34] THAMM F P, BRIEGER N, NEITZKE K P, et al. Songbird-an innovativeuas combining the advantages of fixed wing and multi rotor uas[J]. The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, 2015, XL-1/W4:345-349.
[35] VERSTRAETE D, LEHMKUEHLER K, GONG A, et al.Characterisation of a hybrid, fuel-cell-based propulsion system for small unmanned aircraft[J]. Journal of Power Sources, 2014, 250:204-211.
[36] NISHIZAWA A, KALLO J, GARROT O, et al. Fuel cell and Li-ion battery direct hybridization system for aircraft applications[J]. Journal of Power Sources, 2013, 222:294-300.
[37] LIU W. Hybrid electric vehicle system modeling and control[M]. Chichester:WILEY, 2017:243-287.
[38] 王少杰,侯亮,方奕凯,等.考虑产品运行大数据的装载机变速箱优化设计[J].机械工程学报, 2018, 54(22):218-232. WANG S J, HOU L, FANG Y K, et al. Optimization design of wheel loader gearbox considering product operational big data[J]. Journal of Mechanical Engineering, 2018, 54(22):218-232(in Chinese).
[39] 王少杰.基于作业谱分析与模式识别的工程车辆智能换挡技术研究与应用[D].厦门:厦门大学, 2016:27-45. WANG S J. Research and application of intelligent shift technology for construction vehicles based on job spectrum analysis and pattern recognition[D]. Xiamen:Xiamen University, 2016:27-45(in Chinese).