| Citation: | Zhou Zhou, Liu Chuang, Zhu Xuezhong, et al. Recent developments in aircraft starter/generator and its embedding technology[J]. Journal of Aerospace Power, 2026, 41（10）：20250326 doi: 10.13224/j.cnki.jasp.20250326
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Aircraft starter/generator is a core component of the modern more electric aircraft (MEA) secondary power system. An overview of the mostly used generator type for starter/generator system was presented. Starter/generators were categorized according to whether the generator was embedded within the engine, and the development status of both categories was reviewed, together with typical structural layout schemes for embedded starter/generators. Five key technologies of starter/generator were analyzed: efficient cooling technology, light-weight and high-efficiency generator technology, fault-tolerant generator technology, high-temperature-tolerant generator technology and high-performance converter technology. Evolving trends towards structural integration, collaborative design and multi-task were envisioned. Result show that, common types of generators play essential roles in the application of starter/generators, and the realization of fully embedded starter/generators hinges on further breakthroughs in key figures of merit such as thermal management, power density, fault tolerance, and high-temperature endurance.
| [1] |
Tagge G E, Irish L A, Bailey A R. Systems study for an integrated digital/electric aircraft (IDEA) [R]. NASA-CR-3840, 1985.
|
| [2] |
Cronin M, Hays A, Green F B, et al. Integrated digital/electric aircraft concepts study[R]. NASA-CR-3841, 1985.
|
| [3] |
Weimer J. Past, present and future of aircraft electrical power systems[R]. AIAA 2001-1147, 2001.
|
| [4] |
Weimer J. Power electronics in the more electric aircraft[R]. AIAA 2002-727, 2002.
|
| [5] |
Moir I, Seabridge A. Aircraft systems: mechanical, electrical, and avionics subsystems integration, third edition[M]. Washington DC: AIAA, 2008.
|
| [6] |
Wiegand C. F-35 air vehicle technology overview[R]. AIAA 2018-3368, 2018.
|
| [7] |
Robbins D, Bobalik J, De Stena D, et al. F-35 subsystems design, development & verification[R]. AIAA 2018-3518, 2018.
|
| [8] |
Ostroff H S. F-15 secondary power systems[R]. SAE Technical Paper Series 740885, 1974.
|
| [9] |
Rodgers C. A jet fuel starter and expendable turbojet[R]. ASME Paper 86-GT-1, 1986.
|
| [10] |
Rodgers C. Pneumatic link secondary power systems for military aircraft[R]. SAE Technical Paper Series 881499, 1988.
|
| [11] |
Benham Jr D S, Koerner M S. Jet fuel and air system for starting auxiliary power unit: US6829899[P]. 2004-12-14.
|
| [12] |
Smyth J R, Morey R E, Schultze R W. Ceramic gas turbine technology development and applications[R]. ASME Paper 93-GT-361, 1993.
|
| [13] |
Secunde R R, Macosko P R, Repas S D. Integrated engine-generator concept for aircraft electric secondary power[R]. NASA TM X-2579, 1972.
|
| [14] |
Goodmanson L T, Schultz W H. Installation and integration of transonic transport propulsion systems[R]. SAE Technical Paper Series 710762, 1971.
|
| [15] |
Provost M J. The more electric aero-engine: a general overview from an engine manufacturer[C]//International Conference on Power Electronics Machines and Drives. London: IEE, 2002: 246-251.
|
| [16] |
于立, 张卓然, 张健, 等. 多电发动机内装式高速起动发电机研究与实践[J]. 中国电机工程学报, 2020, 40(14): 4615-4628, 4740. Yu Li, Zhang Zhuoran, Zhang Jian, et al. Study and implementation on high-speed starter/generator for more electric engine application[J]. Proceedings of the CSEE, 2020, 40(14): 4615-4628, 4740. (in Chinese
Yu Li, Zhang Zhuoran, Zhang Jian, et al. Study and implementation on high-speed starter/generator for more electric engine application[J]. Proceedings of the CSEE, 2020, 40(14): 4615-4628, 4740. (in Chinese)
|
| [17] |
刘伟峰. 多电发动机内装式电励磁双凸极起动发电系统关键技术研究[D]. 南京: 南京航空航天大学, 2022. Liu Weifeng. Research on key technologies of doubly salient electro-magnetic starter/generator system for more electric engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese
Liu Weifeng. Research on key technologies of doubly salient electro-magnetic starter/generator system for more electric engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese)
|
| [18] |
黄文新, 张兰红, 胡育文. 18 kW异步电机高压直流起动发电系统设计与实现[J]. 中国电机工程学报, 2007, 27(12): 52-58. Huang Wenxin, Zhang Lanhong, Hu Yuwen. Design and research on 18 kW HVDC induction starter/generator system[J]. Proceedings of the Chinese Society for Electrical Engineering, 2007, 27(12): 52-58. (in Chinese doi: 10.3321/j.issn:0258-8013.2007.12.010
Huang Wenxin, Zhang Lanhong, Hu Yuwen. Design and research on 18 kW HVDC induction starter/generator system[J]. Proceedings of the Chinese Society for Electrical Engineering, 2007, 27(12): 52-58. (in Chinese) doi: 10.3321/j.issn:0258-8013.2007.12.010
|
| [19] |
史建宇, 张宇飞, 郭子韬, 等. 多电辅助动力装置用双绕组感应发电机变频交流发电系统励磁控制技术[J]. 航空动力学报, 2024, 39(10): 20220549. Shi Jianyu, Zhang Yufei, Guo Zitao, et al. Excitation control technology of frequency conversion AC power generation system for dual-winding induction generators for multi-electric auxiliary power units[J]. Journal of Aerospace Power, 2024, 39(10): 20220549. (in Chinese
Shi Jianyu, Zhang Yufei, Guo Zitao, et al. Excitation control technology of frequency conversion AC power generation system for dual-winding induction generators for multi-electric auxiliary power units[J]. Journal of Aerospace Power, 2024, 39(10): 20220549. (in Chinese)
|
| [20] |
Bojoi R, Cavagnino A, Tenconi A, et al. Control of shaft-line-embedded multiphase starter/generator for aero-engine[J]. IEEE Transactions on Industrial Electronics, 2016, 63(1): 641-652. doi: 10.1109/TIE.2015.2472637
|
| [21] |
Ganev E, Fizer L A. DC bus short circuit compliant power generation systems using induction machine: US7459889[P]. 2008-12-02.
|
| [22] |
Mellor P H, Drury D, Wrobel R, et al. Design considerations for aircraft generator with start function[R]. SAE Technical Paper Series 2008-1-2871, 2008.
|
| [23] |
Besnard J P, Biais F, Martinez M. Electrical rotating machines and power electronics for new aircraft equipment systems[C]//Proceedings of 25th International Congress of the Aeronautical Sciences. Hamburg: ICAS, 2006: 3479-3487.
|
| [24] |
Taneja D N, Huang H, Padgett G A, et al. Dual-structured aircraft engine starter/generator: US7687928B2[P]. 2010-3-30.
|
| [25] |
张卓然, 李进才, 韩建斌, 等. 多电飞机大功率高压直流起动发电机系统研究与实现[J]. 航空学报, 2020, 41(2): 323537. Zhang Zhuoran, Li Jincai, Han Jianbin, et al. Research and implementation of high-power high-voltage DC brushless starter generator system for more-electric-aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(2): 323537. (in Chinese
Zhang Zhuoran, Li Jincai, Han Jianbin, et al. Research and implementation of high-power high-voltage DC brushless starter generator system for more-electric-aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(2): 323537. (in Chinese)
|
| [26] |
Lafuze D, Webb R, Triebel C F, et al. 150 kVA samarium cobalt VSCF starter generator electrical system [R]. AFAPL-TR-78-104, 1978.
|
| [27] |
Koerner G P, Siddiqui E U A. Permanent magnet variable speed constant frequency power generation system[R]. AFWAL-TR-85-2112, 1986.
|
| [28] |
Siddiqui E U A. Permanent magnet generator rotor containment study[R]. AFWAL-TR-83-2031, 1983.
|
| [29] |
Balachandran A, Boden M, Sun Zhigang, et al. Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft[J]. The Journal of Engineering, 2019, 2019(17): 3474-3478.
|
| [30] |
Wan Y. Fault behavior and management of a permanent magnet aerospace starter-generator[D]. Sheffield, UK: University of Sheffield, 2019.
|
| [31] |
Bozhko S, Yang Tao, Le Peuvedic J M, et al. Development of aircraft electric starter-generator system based on active rectification technology[J]. IEEE Transactions on Transportation Electrification, 2018, 4(4): 985-996. doi: 10.1109/TTE.2018.2863031
|
| [32] |
Antonino L R. Thermal analysis of a high speed electrical machine[D]. Nottingham, UK: University of Nottingham, 2016.
|
| [33] |
Zhang Xiaochen, Zhang He, Gerada C, et al. Eddy current loss control in high speed PM starter-generator[C]//Proceedings of 2019 IEEE Workshop on Electrical Machines Design, Control and Diagnosis. Athens, US: IEEE, 2019: 46-50.
|
| [34] |
Guo Hong, He Xu, Xu Jinquan, et al. Design and analysis of a novel hybrid cooling method of high-speed high-power permanent magnet assisted synchronous reluctance starter/generator in aviation applications[J]. Chinese Journal of Aeronautics, 2023, 36(3): 285-302. doi: 10.1016/j.cja.2022.08.017
|
| [35] |
郭宏, 何旭, 孙青青, 等. 一种抗短路高速大功率永磁辅助式同步磁阻起动发电机系统: CN202011478060.6[P]. 2022-03-18.
|
| [36] |
Radun A, Richter E. A detailed power inverter design for a 250 kW switched reluctance aircraft engine starter/generator[R]. SAE Technical Paper Series 931388, 1993.
|
| [37] |
Ferreira C A, Richter E. Detailed design of a 250 kW switched reluctance starter/generator for an aircraft engine[R]. SAE Technical Paper Series 931389, 1993.
|
| [38] |
Richter E, Lyons J P, Ferreira C, et al. Initial testing of a 250 kW starter/generator for aircraft applications[R]. SAE Technical Paper Series 941160, 1994.
|
| [39] |
Ferreira C A, Legros C R. Switched reluctance starter/generator: US005523635A[P]. 1996-06-04.
|
| [40] |
胡子慧. 大功率开关磁阻起动/发电系统控制策略研究[D]. 武汉: 华中科技大学, 2021. Hu Zihui. Research on control strategy of high-power switched reluctance starter/generator system[D]. Wuhan: Huazhong University of Science and Technology, 2021. (in Chinese
Hu Zihui. Research on control strategy of high-power switched reluctance starter/generator system[D]. Wuhan: Huazhong University of Science and Technology, 2021. (in Chinese)
|
| [41] |
Wu Yiying, Li Zixin, Wang Shuanghong, et al. Angle position compensation control strategy for high-speed power generation of aerospace integrated switched reluctance starting/generating system[J]. IEEE Journal of Emerging and Selected Topics in Power Electronics, 2023, 11(6): 5690-5700. doi: 10.1109/JESTPE.2023.3307454
|
| [42] |
Latos T S, Mcarthur M J. System design considerations for an APU starter-generator[R]. SAE Technical Paper Series 932559, 1993.
|
| [43] |
Anghel C. A novel start system for an aircraft auxiliary power unit[R]. SAE Technical Paper Series 2000-1-3624, 2000.
|
| [44] |
Haag J E, Jennings C H. VSCF cycloconverter reliability review of the 30/40 kVA F/A-18 electrical generating system[R]. SAE Technical Paper Series 892228, 1989.
|
| [45] |
VanNocker R C, Carmine W A. Cost of ownership advantages with a shared oil system[R]. SAE Technical Paper Series 811082, 1981.
|
| [46] |
Smith R A. Joint strike fighter integrated subsystems technology (J/IST) demonstration program overview[R]. SAE Technical Paper Series 962259, 1996.
|
| [47] |
Demel H F, Richter E, Triebel C F, et al. Samarium cobalt (SmCo) generator/engine integration study[R]. AFWAL-TR-80-2022, 1980.
|
| [48] |
Richter E, Anstead D H, Bartos J W, et al. Preliminary design of an internal starter/generator for application in the F110-129 engine[R]. SAE Technical Paper Series 951406, 1995.
|
| [49] |
Mitcham A J. Permanent magnet generator options for the More Electric Aircraft[C]//Proceedings of 2002 International Conference on Power Electronics, Machines and Drives. Bath: IET, 2002: 241-245.
|
| [50] |
Lemmers G C, Spierling T A. Tail cone generator with integral speed increasing gearbox: US20160149469[P]. 2016-05-26.
|
| [51] |
Mcloughlin A. Engine powerplant electrical systems[C]//Proceedings of More Electric Aircraft Forum. Barcelona, Spain: MOET Project Consortium, 2009: 1-9.
|
| [52] |
James P D. Modelling of high power density electrical machines for aerospace[D]. Sheffield, UK: University of Sheffield, 2004.
|
| [53] |
Jacobs S, Liebermann E, Babad C. Altitude performance test results for low pressure turbine mounted generator[R]. SAE Technical Paper Series 2006-1-3056, 2006.
|
| [54] |
Klaass R M F, McFadden B. More-electric aircraft integrated power unit designed for dual use[R]. SAE Technical Paper Series 941159, 1994.
|
| [55] |
Klaass R M, DellaCorte C. The quest for oil-free gas turbine engines[R]. SAE Technical Paper Series 2006-01-3055, 2006.
|
| [56] |
Dower J H. Feasibility demonstration of a turbine engine rotor mounted electrical generator[R]. SAE Technical Paper 760520, 1976.
|
| [57] |
Jacobs S, Liebermann E, Babad C. Generator survivability in the hot environment associated with low pressure turbine installation[R]. SAE Technical Paper Series 2004-01-3155, 2004.
|
| [58] |
Liebermann E. Rotor cooling arrangement: US6661133[P]. 2003-12-09.
|
| [59] |
Brand J H, Dooley K A, Dowhan M J, et al. More electric small turbofan[R]. SAE Technical Paper Series 2004-01-1804, 2004.
|
| [60] |
Bhangu B S, Rajashekara K. Electric starter generators: their integration into gas turbine engines[J]. IEEE Industry Applications Magazine, 2014, 20(2): 14-22. doi: 10.1109/MIAS.2013.2288398
|
| [61] |
Ganev E, Koerner M. Power and thermal management for future aircraft[R]. SAE Technical Paper Series 2013-01-2273, 2013.
|
| [62] |
Chen Yuzheng, Yang Tao, Khowja M R, et al. Mild hybridization of turboprop engine with high-power-density integrated electric drives[J]. IEEE Transactions on Transportation Electrification, 2022, 8(4): 4148-4162. doi: 10.1109/TTE.2022.3160153
|
| [63] |
Hill J E. Control of a variable speed, fault-tolerant permanent magnet generator[C]//Proceedings of 2002 International Conference on Power Electronics, Machines and Drives. Bath: IET, 2002: 492-497.
|
| [64] |
Ede J, Jewell G, Atallah K, et al. Design of a 250 kW, fault-tolerant PM generator for the more-electric aircraft[R]. AIAA 2005-5644, 2005.
|
| [65] |
Sun Zhigan, Ede J, Wang Jiabin, et al. Experimental testing of a 250 kW fault-tolerant permanent magnet power generation system for large civil aero-engines[R]. AIAA 2007-4829, 2007.
|
| [66] |
Ismagilov F R, Papini L, Vavilov V E, et al. Design and performance of a high-speed permanent magnet generator with amorphous alloy magnetic core for aerospace applications[J]. IEEE Transactions on Industrial Electronics, 2020, 67(3): 1750-1758. doi: 10.1109/TIE.2019.2905806
|
| [67] |
MacMinn S R, Jones W D. A very high speed switched-reluctance starter-generator for aircraft engine applications[C]//Proceedings of the IEEE National Aerospace and Electronics Conference. Piscataway, US: IEEE, 1989: 1758-1764.
|
| [68] |
Jones W D, Fletcher A R. Electric drives on the LV100 gas turbine engine[R]. ASME Paper 93-GT-7, 1993.
|
| [69] |
Ferreira C A, Jones S R, Heglund W S, et al. Detailed design of a 30 kW switched reluctance starter/generator system for a gas turbine engine application[J]. IEEE Transactions on Industry Applications, 1995, 31(3): 553-561. doi: 10.1109/28.382116
|
| [70] |
Richter E, Anderson R E, Severt C. The integral starter/generator development progress[R]. SAE Technical Paper Series 920967, 1992.
|
| [71] |
Himes M, Schauer J. Measurement of heat transfer in a switched reluctance generator[R]. AIAA 1998-2463, 1998.
|
| [72] |
Smith G, Halsey D, Hoffman E P. Integrated power unit-advanced development[R]. SAE Technical Paper Series 981281, 1998.
|
| [73] |
Grennan R, Greenlee W, Halsey D, et al. Air cooled dynamoelectric machine: US005994804A[P]. 1999-11-30.
|
| [74] |
Powell D, Jewell G, Ede J, et al. An integrated starter/generator for a large civil aero-engine[R]. AIAA 2005-5550, 2005.
|
| [75] |
Leon R. High temperature embedded electrical machines for aerospace turbine applications[D]. Sheffield, UK: University of Sheffield, 2013.
|
| [76] |
Song S. Detailed design of a 30 kW switched reluctance starter/generator system used in more/all electric aircraft[D]. Berlin: Technical University of Berlin, 2009.
|
| [77] |
Sun Guilin, Song Shoujun, Jiang Jianan, et al. Characteristics testing and torque control of aero-engine shaft-line-embedded switched reluctance starter/generator[J]. IEEE Transactions on Industry Applications, 2023, 59(6): 7295-7305. doi: 10.1109/TIA.2023.3299895
|
| [78] |
Sawata T, Paskell L, Dinu A, et al. Initial test results for the fan shaft driven generator[C]//Proceedings of 25th International Congress of the Aeronautical Sciences. Hamburg, Germany: ICAS, 2006: 1-8.
|
| [79] |
张健. 高速电励磁双凸极电机损耗分析与热管理技术研究[D]. 南京: 南京航空航天大学, 2020. Zhang Jian. Research on loss analysis and thermal management technology of high-speed doubly salient electromagnetic machine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020. (in Chinese
Zhang Jian. Research on loss analysis and thermal management technology of high-speed doubly salient electromagnetic machine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020. (in Chinese)
|
| [80] |
于立. 多电发动机高速双凸极起动发电机系统关键技术研究[D]. 南京: 南京航空航天大学, 2019. Yu Li. Research on key technologies of high-speed doubly salient starter/generator system for more electric engine application[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese
Yu Li. Research on key technologies of high-speed doubly salient starter/generator system for more electric engine application[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese)
|
| [81] |
蒋思远. 应用于多电发动机的电励磁双凸极电机电磁热分析与设计研究[D]. 南京: 南京航空航天大学, 2022. Jiang Siyuan. Electromagnetic-thermal analysis and design research of doubly salient electro-magnetic machine for more electric engine application[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese
Jiang Siyuan. Electromagnetic-thermal analysis and design research of doubly salient electro-magnetic machine for more electric engine application[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese)
|
| [82] |
Hirst M, Mcloughlin A, Norman P J, et al. Demonstrating the more electric engine: a step towards the power optimised aircraft[J]. IET Electric Power Applications, 2011, 5(1): 3-13. doi: 10.1049/iet-epa.2009.0285
|
| [83] |
Ganev E. High-reactance permanent magnet machine for high-performance power generation systems[R]. SAE Technical Paper Series 2006-01-3076, 2006.
|
| [84] |
Powell D J, Jewell G W, Howe D, et al. Rotor topologies for a switched-reluctance machine for the ‘more-electric’ aircraft engine[J]. IEE Proceedings - Electric Power Applications, 2003, 150(3): 311-318. doi: 10.1049/ip-epa:20030121
|
| [85] |
Xu Z, Galea M, Tighe C, et al. Mechanical and thermal management design of a motor for an aircraft wheel actuator[C]//2014 17th International Conference on Electrical Machines and Systems. Hangzhou: IEEE, 2014: 3268-3273.
|
| [86] |
Balachandran T, Srimmana S, Anderson A, et al. Assembly and qualification of a slotless stator assembly for a MW class permanent magnet synchronous machine[R]. AIAA 2020-3584, 2020.
|
| [87] |
Anghel C, Davis T S, Phielix T, et al. Compact high speed generator having respective oil and air cooling passages: US10715013[P]. 2020-07-14.
|
| [88] |
Vannini A, Di Nardo M, La Rocca A, et al. Design and testing of a direct oil-cooled homopolar synchronous generator with dual DC-link via diode rectifiers[J]. IEEE Transactions on Transportation Electrification, 2025, 11(4): 10099-10112. doi: 10.1109/TTE.2025.3564349
|
| [89] |
Dai Hang, Yagielski J, Jahns T, et al. Supercritical carbon dioxide (sCO2)-cooled current source inverter-based integrated motor drive for MW-scale electric aviation applications[C]//Proceedings of 2025 IEEE Applied Power Electronics Conference and Exposition (APEC). San Antonio, US: IEEE, 2025: 3174-3180.
|
| [90] |
Zhang Jian, Zhu Xiqing, Zhang Zhuoran, et al. AC loss calculation and analysis of hollow conductor for doubly salient brushless DC generator[J]. IEEE Transactions on Magnetics, 2022, 58(8): 8106805. doi: 10.1109/tmag.2022.3156603
|
| [91] |
Mecrow B C, Jack A G, Atkinson D J, et al. Design and testing of a four-phase fault-tolerant permanent-magnet machine for an engine fuel pump[J]. IEEE Transactions on Energy Conversion, 2004, 19(4): 671-678. doi: 10.1109/TEC.2004.832074
|
| [92] |
Sangha P S, Sawata T, Yon J, et al. Assessment of fluid drag loss in a flooded rotor electro-hydrostatic actuator motor[C]//2015 IEEE International Electric Machines & Drives Conference. Coeur d’Alene, US: IEEE, 2015: 139-142.
|
| [93] |
Al-timimy A, Giangrande P, Degano M, et al. Design and losses analysis of a high power density machine for flooded pump applications[J]. IEEE Transactions on Industry Applications, 2018, 54(4): 3260-3270. doi: 10.1109/TIA.2018.2821623
|
| [94] |
Xu Jinquan, Jin Wenbo, Guo Hong, et al. Design and analysis of a high-speed wet-type fault-tolerant permanent magnet motor considering oil frictional loss for aerospace electrohydrostatic actuator application[J]. IEEE Transactions on Transportation Electrification, 2024, 10(3): 4667-4677. doi: 10.1109/TTE.2023.3319337
|
| [95] |
Denk J, Ashmore J H, Kouyoumjian O, et al. 270 VDC varible speed generator and control unit, aircraft electric power system[R]. NADC-80014-60, 1980.
|
| [96] |
El-refaie A M, Shah M R, Huh K K. High-power-density fault-tolerant PM generator for safety-critical applications[J]. IEEE Transactions on Industry Applications, 2014, 50(3): 1717-1728. doi: 10.1109/TIA.2013.2282852
|
| [97] |
Golovanov D, Gerada D, Sala G, et al. 4 MW class high-power-density generator for future hybrid-electric aircraft[J]. IEEE Transactions on Transportation Electrification, 2021, 7(4): 2952-2964. doi: 10.1109/TTE.2021.3068928
|
| [98] |
Wang Jin, Jahns T M, Mccluskey P, et al. 2 kV 1 MW 20 000 r/min integrated modular motor drive for electrified aircraft propulsion[J]. IEEE Journal of Emerging and Selected Topics in Power Electronics, 2025, 13(1): 394-407. doi: 10.1109/JESTPE.2023.3283538
|
| [99] |
Shortte M. Electro-thermal optimisation of a 50 kW synchronous permanent magnet generator for aerospace application[D]. Sheffield, UK: University of Sheffield, 2016.
|
| [100] |
陆嘉伟, 张卓然, 李进才, 等. 电推进飞机移相双绕组永磁电机特性分析[J]. 航空学报, 2022, 43(5): 325230. Lu Jiawei, Zhang Zhuoran, Li Jincai, et al. Characteristic analysis of dual-winding permanent magnet synchronous machine with phase-shifted windings for electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(5): 325230. (in Chinese
Lu Jiawei, Zhang Zhuoran, Li Jincai, et al. Characteristic analysis of dual-winding permanent magnet synchronous machine with phase-shifted windings for electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(5): 325230. (in Chinese)
|
| [101] |
王立坤, 李靖琰, 乔治, 等. 大容量隐极同步电机冷却关键技术综述[J/OL]. 中国电机工程学报, (2025-04-15). https://doi.org/10.13334/j.0258-8013.pcsee.242512. Wang Likun, Li Jingyan, Qiao Zhi, et al. Review of cooling key technology of large capacity non-salient pole synchronous generator[J/OL]. Proceedings of the CSEE, (2025-04-15). https://doi.org/10.13334/j.0258-8013.pcsee.242512. (in Chinese
Wang Likun, Li Jingyan, Qiao Zhi, et al. Review of cooling key technology of large capacity non-salient pole synchronous generator[J/OL]. Proceedings of the CSEE, (2025-04-15). https://doi.org/10.13334/j.0258-8013.pcsee.242512. (in Chinese)
|
| [102] |
Ghanekar M. Vapor cycle system for the F-22 raptor[R]. SAE Technical Paper Serie 2000-01-2268, 2000.
|
| [103] |
屠敏, 袁耿民, 薛飞, 等. 综合热管理在先进战斗机系统研制中的应用[J]. 航空学报, 2020, 41(6): 523629. Tu Min, Yuan Gengmin, Xue Fei, et al. Application of integrated thermal management in development of advanced fighter system[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 523629. (in Chinese
Tu Min, Yuan Gengmin, Xue Fei, et al. Application of integrated thermal management in development of advanced fighter system[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 523629. (in Chinese)
|
| [104] |
Cakal G, Sarlioglu B. Two-phase immersion cooling of high-performance electric traction motors[J]. IEEE Transactions on Transportation Electrification, 2025, 11(2): 6866-6874. doi: 10.1109/TTE.2024.3517695
|
| [105] |
Chen Yuankang, Spakovszky Z S, Greitzer E M, et al. Novel channel-type heat exchanger for a megawatt-class integrated motor drive technology demonstrator[R]. AIAA 2023-4159, 2023.
|
| [106] |
Booker J D, Yon J, Williamson S, et al. Development of a power generation system and quadruplex direct electric drive for a helicopter tail rotor[R]. AIAA-2020-0118, 2020.
|
| [107] |
Stephenson J M. Improvements in electric reluctance machines: US5780949[P]. 1998-07-14.
|
| [108] |
Hebala A, Nuzzo S, Connor P H, et al. Passive in-slot heat path realization for extending the operating limits of an aircraft propulsion motor[J]. IEEE Transactions on Transportation Electrification, 2025, 11(2): 6952-6961. doi: 10.1109/TTE.2024.3520380
|
| [109] |
Hebala A, Connor P H, Nuzzo S, et al. A holistic analysis and experimental testing of a passive heat path for electric motors slots[J]. IEEE Transactions on Transportation Electrification, 2025, 11(3): 8128-8138. doi: 10.1109/TTE.2025.3537161
|
| [110] |
Wrobel R, Hussein A. A feasibility study of additively manufactured heat guides for enhanced heat transfer in electrical machines[J]. IEEE Transactions on Industry Applications, 2020, 56(1): 205-215. doi: 10.1109/TIA.2019.2949258
|
| [111] |
Wu Fan, El-refaie A M, Al-qarni A. Additively manufactured hollow conductors integrated with heat pipes: design tradeoffs and hardware demonstration[J]. IEEE Transactions on Industry Applications, 2021, 57(4): 3632-3642. doi: 10.1109/TIA.2021.3076423
|
| [112] |
Vahid S, Koushan S, Chowdhury T, et al. A comprehensive characterization of hollow conductor additively manufactured coils and thermal management system for a 250 kW SPM machine[J]. IEEE Transactions on Industry Applications, 2025, 61(1): 115-125. doi: 10.1109/TIA.2024.3472634
|
| [113] |
李立毅, 张江鹏, 闫海媛, 等. 高功率密度电机三维温度场计算及导热优化研究[J]. 中国电机工程学报, 2016, 36(13): 3642-3650, 3384. Li Liyi, Zhang Jiangpeng, Yan Haiyuan, et al. Study on the optimization of thermal conductivity and 3D temperature filed calculation for the high power density motor[J]. Proceedings of the Chinese Society for Electrical Engineering, 2016, 36(13): 3642-3650, 3384. (in Chinese doi: 10.13334/j.0258-8013.pcsee.151396
Li Liyi, Zhang Jiangpeng, Yan Haiyuan, et al. Study on the optimization of thermal conductivity and 3D temperature filed calculation for the high power density motor[J]. Proceedings of the Chinese Society for Electrical Engineering, 2016, 36(13): 3642-3650, 3384. (in Chinese) doi: 10.13334/j.0258-8013.pcsee.151396
|
| [114] |
Nategh S, Boglietti A, Barber D, et al. Thermal and manufacturing aspects of traction motors potting: a deep experimental evaluation[J]. IEEE Transactions on Energy Conversion, 2020, 35(2): 1026-1035. doi: 10.1109/TEC.2020.2966606
|
| [115] |
Widmer J D, Spargo C M, Atkinson G J, et al. Solar plane propulsion motors with precompressed aluminum stator windings[J]. IEEE Transactions on Energy Conversion, 2014, 29(3): 681-688. doi: 10.1109/TEC.2014.2313642
|
| [116] |
Ou J. Improving high-speed electrical machines by amorphous metals[D]. Karlsruhe, Germany: Karlsruhe Institute of Technology, 2019.
|
| [117] |
Zhang Di, He Jiangbiao, Pan Di, et al. Development of a high power density megawatt-scale medium-voltage power converter for aircraft hybrid-electric propulsion systems[R]. AIAA-2019-4472, 2019.
|
| [118] |
Gwynne B, Lyon P. Magnesium alloys in aerospace applications, past concerns, current solutions[C]//Proceedings of 5th triennial international aircraft fire and cabin safety research conference. Atlantic, US: FAA, 2007.
|
| [119] |
Fetter S. JSF/F-35 pollution prevention activities[C]//Proceedings of ESTCP/SERDP DoD Metal Finishing Workshop. Washington DC: DoD, 2006.
|
| [120] |
Swanke J, Bobba D, Jahns T, et al. Design of high-speed permanent magnet machine for aerospace propulsion[R]. AIAA-2019-4483, 2019.
|
| [121] |
周凤争. 高速永磁无刷直流电机转子涡流损耗的研究[D]. 杭州: 浙江大学, 2008. Zhou Fengzheng. Investigation of rotor eddy-current loss in high-speed PM BLDC motors[D]. Hangzhou: Zhejiang University, 2008. (in Chinese
Zhou Fengzheng. Investigation of rotor eddy-current loss in high-speed PM BLDC motors[D]. Hangzhou: Zhejiang University, 2008. (in Chinese)
|
| [122] |
Guo Hong, He Xu, Xu Jinquan, et al. Design of an aviation dual-three-phase high-power high-speed permanent magnet assisted synchronous reluctance starter-generator with antishort-circuit ability[J]. IEEE Transactions on Power Electronics, 2022, 37(10): 12619-12635. doi: 10.1109/TPEL.2022.3172339
|
| [123] |
Mcmurray W. Frequency converter technology for aircraft power systems[J]. Journal of Energy, 1982, 6(5): 328-333. doi: 10.2514/3.62613
|
| [124] |
Fingers R T. Creep behavior of thin laminates of iron-cobalt alloys for use in switched reluctance motors and generators[D]. Blacksburg: Virginia Polytechnic Institute and State University, 1998.
|
| [125] |
Fingers R T. Creep Behavior of thin laminates of iron-cobalt alloys for use in switched reluctance motors and generators[R]. AFRL-PR-WP-TR-1999-2053, 1999.
|
| [126] |
De Groh Iii H C, Geng S M, Niedra J M, et al. Magnetic properties of Fe-49Co-2V alloy and pure Fe at Room and Elevated Temperatures[R]. NASA/TM-2018-219872, 2018.
|
| [127] |
Geist B, Peterson T, Horwath J C, et al. Effect of high-temperature aging on electrical properties of Hiperco® 27, Hiperco® 50, and Hiperco® 50 HS alloys[J]. Journal of Applied Physics, 2003, 93(10): 6686-6688. doi: 10.1063/1.1556104
|
| [128] |
Horwath J, Turgut Z, Fingers R. High temperature properties and aging-stress related changes of FeCo materials[R]. AFRL-PR-WP-TR-2006-2176. 2006.
|
| [129] |
Tshiloz K, Smith A C, Tuohy P M, et al. Investigation of wire insulation for high-temperature motor windings[J]. The Journal of Engineering, 2019, 2019(17): 4442-4445. doi: 10.1049/joe.2018.8113
|
| [130] |
Le Fang. High temperature electrical machine insulation for aircraft systems[D]. Manchester, UK: University of Manchester, 2015.
|
| [131] |
Wang Zijing, Fang Le, Cotton I, et al. Ni–Cu interdiffusion and its implication for ageing in Ni-coated Cu conductors[J]. Materials Science and Engineering: B, 2015, 198: 86-94. doi: 10.1016/j.mseb.2015.04.006
|
| [132] |
Montague G, Jansen M, Ebihara B, et al. Design and fabrication of high-temperature radial magnetic bearing for turbomachinery[R]. NASA/TM-2003-212300, 2003.
|
| [133] |
Rosswurm M A. Design considerations of DC-link aircraft generation systems[J]. SAE Technical Paper Series, 1981, 1: 811081. doi: 10.4271/811081
|
| [134] |
Bozhko S, Yeoh S S, GAO Fei, et al. Control design for electric starter-generator based on a high-speed permanent-magnet machine fed by an active front-end rectifier[R]. SAE Technical Paper Series 2014-01-2139, 2014.
|
| [135] |
Chen Ruirui, Niu Jiahao, Ren Ren, et al. A cryogenically-cooled MW inverter for electric aircraft propulsion[C]//Proceedings of 2020 AIAA/IEEE Electric Aircraft Technologies Symposium. New Orleans, US: AIAA/IEEE, 2020: 1-10.
|
| [136] |
Yuan Zhao, Emon A I, Wang Zhongjing, et al. A low inductance, high power density 3L-TNPC power module for more-electric aircraft applications[J]. IEEE Transactions on Transportation Electrification, 2022, 8(4): 4291-4302. doi: 10.1109/TTE.2022.3183227
|
| [137] |
Hornberger J, Mcpherson B, Bourne J, et al. High temperature silicon carbide power modules for high performance systems[J]. Additional Conferences (Device Packaging, HiTEC, HiTEN, and CICMT), 2011, 2011: 159-166.
|
| [138] |
Schupbach R, Cilio E, Hornberger J, et al. A very high-temperature (400+℃) inverter for energy storage applications utilizing silicon on insulator (SOI) and silicon carbide (SiC) electronics[C]//Proceedings of 2005 IEEE Electrical Energy Storage Systems Applications and Technologies. San Franciso, US: IEEE, 2005: 1-7.
|
| [139] |
Bergogne D, Morel H, Planson D, et al. Towards an airborne high temperature SiC inverter[C]//Proceedings of 2008 IEEE Power Electronics Specialists Conference. Rhodes, US: IEEE, 2008: 3178-3183.
|
| [140] |
Ahmed S, Lai Pengyu, Chinnaiyan S, et al. High-temperature (250 ℃) SiC power module integrated with LTCC-based isolated gate driver[C]//Proceedings of 2023 IEEE Applied Power Electronics Conference and Exposition. Orlando, US: IEEE, 2023: 2588-2595.
|
| [141] |
Reese B, Mcpherson B, Shaw R, et al. High temperature (250 ℃) silicon carbide power modules with integrated gate drive boards[J]. Additional Conferences (Device Packaging, HiTEC, HiTEN, and CICMT), 2010, 2010: 297-304. doi: 10.4071/hitec-rschupbach-wp23
|
| [142] |
Esler D. GE SiC semiconductor device operation at extreme temperatures[J]. Journal of Microelectronics and Electronic Packaging, 2022, 19(3): 83-88. doi: 10.4071/2380-4491.2021.hitec.000041
|
| [143] |
Ryu S H, Krishnaswami S, Hull B A, et al. A comparison of high temperature performance of SiC DMOSFETs and JFETs[R]. AFRL-PR-WP-TP-2007-216, 2007.
|
| [144] |
Stockmeier T, Beckedahl P, Göbl C, et al. SKiN: Double side sintering technology for new packages[C]//Proceedings of 2011 IEEE 23rd International Symposium on Power Semiconductor Devices and ICs. San Diego, US: IEEE, 2011: 324-327.
|
| [145] |
Beckedahl P, Buetow S, Maul A, et al. 400 A, 1200 V SiC power module with 1nH commutation inductance[C]//Proceedings of 9th International Conference on Integrated Power Electronics Systems. Nuremberg, Germany: VDE, 2016: 1-6.
|
| [146] |
Beckedahl P, Bogen I, Steger J. SiC automotive power module with laser welded, ultra low inductive terminals and up to 900Arms phase current[C]//Proceedings of 12th International Conference on Integrated Power Electronics Systems. Berlin: VDE, 2022: 39-43.
|
| [147] |
Pautsch A G, Gowda A, Stevanovic L, et al. Double-sided microchannel cooling of a power electronics module using power overlay[C]//Proceedings of 2009 International Electronic Packaging Technical Conference and Exhibition. San Francisco, US: ASME, 2009: 427-436.
|
| [148] |
Chang H R, Bu Jiankang, Kong G, et al. 300 A 650 V 70 um thin IGBTs with double-sided cooling[C]//IEEE 23rd International Symposium on Power Semiconductor Devices and ICs. San Diego, US: IEEE, 2011: 320-323.
|
| [149] |
Anwar M, Teimor M, Savagian P, et al. Compact and high power inverter for the Cadillac CT6 rear wheel drive PHEV[C]//2016 IEEE Energy Conversion Congress and Exposition. Milwaukee, US: IEEE, 2016: 1-7.
|
| [150] |
Le Henaff F, Greca G, Salerno P, et al. Double side sintered IGBT + FRD, 650 V/200 A, in a STO247 package for high performance automotive applications[C]//Proceedings of 2017 International Exhibition and Conference for Power Electronics, Intelligent Motion, Renewable Energy and Energy Management. Nuremberg, Germany: VDE, 2017: 1-5.
|
| [151] |
Yin Liang, Kapusta C, Gowda A, et al. A wire-bondless packaging platform for silicon carbide power semiconductor devices[J]. Journal of Electronic Packaging, 2018, 140(3): 031009. doi: 10.1115/1.4040499
|
| [152] |
Brinkfeldt K, Ottosson J, Neumaier K, et al. Design and fabrication of a SiC-based power module with double-sided cooling for automotive applications[C]//Proceedings of 19th International Forum on Advanced Microsystems for Automotive Applications. Berlin: Springer, 2015: 157-171.
|
| [153] |
Liang Zhenxian. Integrated double sided cooling packaging of planar SiC power modules[C]//Proceedings of 2015 IEEE Energy Conversion Congress and Exposition. Montreal, Canada: IEEE, 2015: 4907-4912.
|
| [154] |
Wang Yangang, Li Yun, Wu Yibo, et al. High power compact automotive IGBT module with planar packaging technology[C]//2017 International Exhibition and Conference for Power Electronics, Intelligent Motion, Renewable Energy and Energy Management. Shanghai: VDE, 2017: 255-259.
|
| [155] |
Huang Si, Chen Zhong. A SiC double-sided stacked wire-bondless power module for high-frequency power electronic applications[J]. Journal of Microelectronics and Electronic Packaging, 2021, 18(3): 113-122. doi: 10.4071/imaps.1426127
|
| [156] |
Ding Chao, Liu Heziqi, Ngo K D T, et al. A double-side cooled SiC MOSFET power module with sintered-silver interposers: I-design, simulation, fabrication, and performance characterization[J]. IEEE Transactions on Power Electronics, 2021, 36(10): 11672-11680. doi: 10.1109/TPEL.2021.3070326
|
| [157] |
Ostmann A, Hofmann T, Neeb C, et al. Embedded power electronics for automotive applications[C]//Proceedings of 7th International Microsystems, Packaging, Assembly and Circuits Technology Conference. Taipei: IEEE, 2012: 163-166.
|
| [158] |
Neeb C, Teichrib J, De Doncker R W, et al. A 50 kW IGBT power module for automotive applications with extremely low DC-link inductance[C]//Proceedings of 16th European Conference on Power Electronics and Applications. Lappeenranta, Finland: IEEE, 2014: 1-10.
|
| [159] |
Kearney D J, Kicin S, Bianda E, et al. PCB embedded semiconductors for low-voltage power electronic applications[J]. IEEE Transactions on Components, Packaging and Manufacturing Technology, 2017, 7(3): 387-395. doi: 10.1109/TCPMT.2017.2651646
|
| [160] |
Stippich A, Kamp T, Sewergin A, et al. A highly-integrated SiC power module for fast switching DC-DC converters[C]//Proceedings of 2019 IEEE Energy Conversion Congress and Exposition. Baltimore, US: IEEE, 2019: 5329-5336.
|
| [161] |
Moniz T O, Cooker P, Orlando R J. Gas turbine engine assembly and method of assembling same: US7997085[P]. 2011-08-16.
|
| [162] |
Madavan N. The electrifying future of air transportation[C]//Proceedings of 2017 IEEE Energy Conversion Congress and Exposition. Cincinnati, US: IEEE, 2017: 1-7.
|
| [163] |
王辉坪, 罗智浩. 涡扇发动机低压转子轴功率提取方法及试验验证[J]. 科技经济市场, 2019(3): 18-19. Wang Huiping, Luo Zhihao. Power extraction method and experimental verification of low pressure rotor shaft of turbofan engine[J]. Science & Technology Ecnony Market, 2019(3): 18-19. (in Chinese
Wang Huiping, Luo Zhihao. Power extraction method and experimental verification of low pressure rotor shaft of turbofan engine[J]. Science & Technology Ecnony Market, 2019(3): 18-19. (in Chinese)
|
| [164] |
Miller C, Zumberge J, Michael Corbett, et al. Low spool electrical power extraction using hardware-in-the-loop methods[R]. AIAA-2010-7091, 2010.
|
| [165] |
Bash M, Boyd M, Miller C. Transient engine emulation within a laboratory testbed for aircraft power systems[J]. SAE International Journal of Aerospace, 2014, 7(2): 191-198. doi: 10.4271/2014-01-2170
|
| [166] |
Enalou H B, Lang Xiaoyu, Rashed M, et al. Time-scaled emulation of electric power transfer in the more electric engine[J]. IEEE Transactions on Transportation Electrification, 2020, 6(4): 1679-1694. doi: 10.1109/TTE.2020.2999400
|
| [167] |
Fang Jun, Zhang Tianhong, Cen Zhaohui, et al. Multi-electric aero engine control and hardware-in-the-loop verification with starter generator coordination[J]. Aerospace, 2024, 11(4): 271. doi: 10.3390/aerospace11040271
|
| [168] |
骆嘉凡. 功率提取条件下航空发动机半物理仿真及控制策略研究[D]. 哈尔滨: 哈尔滨工程大学, 2023. Luo Jiafan. Research on semi-physical simulation and control strategy of aero-engine under power extraction conditions[D]. Harbin: Harbin Engineering University, 2023. (in Chinese
Luo Jiafan. Research on semi-physical simulation and control strategy of aero-engine under power extraction conditions[D]. Harbin: Harbin Engineering University, 2023. (in Chinese)
|
| [169] |
Chapman J W. A study of large scale power extraction and insertion on turbofan performance and stability[R]. AIAA 2020-3547, 2020.
|
| [170] |
Balaghi Enalou H, Le-Peuvedic J M, Rashed M, et al. Potential improvements in turbofan’s performance by electric power transfer[R]. SAE Technical Paper Series 2018-01-1962, 2018.
|
| [171] |
Culley D E, Kratz J L, Thomas G L. Turbine electrified energy management (TEEM) for enabling more efficient engine designs[R]. AIAA 2018-4798, 2018.
|
| [172] |
Wheeler P, Clare J, Bozhko S, et al. Regeneration in aircraft electrical power systems [R]. SAE Technical Paper Series 2008-01-2898, 2008.
|
| [173] |
Ganev E, Sarlioglu B. Improving load regeneration capability of an aircraft[R]. SAE Technical Paper Series 2009-01-3189, 2009.
|
| [174] |
Xu Yanwu, Zhang Zhuoran. Regenerated energy absorption methods for more electric aircraft starter/generator system[J]. IEEE Transactions on Power Electronics, 2023, 38(6): 7525-7534. doi: 10.1109/TPEL.2023.3250208
|
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