| Citation: | LI Jiacheng, SHENG Hanlin, CHEN Xin, et al. System design of hybrid distributed electric propulsion aircraft[J]. Journal of Aerospace Power, 2024, 39（9）：20220693 doi: 10.13224/j.cnki.jasp.20220693
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The Y-7 aircraft was used as the reference model to carry out the overall design and performance analysis of the distributed electric propulsion aircraft. The power system of the distributed electric propulsion aircraft was designed, including design of propeller parameters, correction of wing parameters, calculation of motor power and type selection and aerodynamic design of propeller, and finally the design of hybrid power system was completed. The mass increase and decrease of each part of the distributed electric propulsion aircraft were completely calculated and its flight performance was analyzed. Compared with the reference model, the range and duration increased by 540 km and 1.2 h respectively, up by 20%. Finally, the three-dimensional modeling was established and aerodynamic characteristics of the distributed electric propulsion aircraft were analyzed. The result provides a theoretical basis for the modeling, simulation and control of distributed electric propulsion aircraft and its engineering applications.
| [1] |
饶崇,张铁军,魏闯,等. 一种分布式电动飞机螺旋桨滑流影响机理[J]. 航空学报,2021,42(增刊1): 157-167. RAO Chong,ZHANG Tiejun,WEI Chuang,et al. Influence mechanism of propeller slipstream on wing of a distributed electric aircraft scheme[J]. Acta Aeronautica et Astronautica Sinica,2021,42(Suppl. 1): 157-167. (in Chinese
RAO Chong, ZHANG Tiejun, WEI Chuang, et al. Influence mechanism of propeller slipstream on wing of a distributed electric aircraft scheme[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(Suppl. 1): 157-167. (in Chinese)
|
| [2] |
KIRNER R,RAFFAELLI L,ROLT A,et al. An assessment of distributed propulsion: Part B advanced propulsion system architectures for blended wing body aircraft configurations[J]. Aerospace Science and Technology,2016,50: 212-219.
|
| [3] |
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 Xianghao,ZHANG Zhuoran,LU Jiawei,et al. Review of electric power system of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica,2018,39(1): 021651. (in Chinese
KONG Xianghao, ZHANG Zhuoran, LU Jiawei, et al. Review of electric power system of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 021651. (in Chinese)
|
| [4] |
DEERE K A,VIKEN J K,VIKEN S,et al. Computational analysis of a wing designed for the X-57 distributed electric propulsion aircraft[R]. AIAA 2017-3923,2017.
|
| [5] |
CONNOLLY J W,CHAPMAN J W,STALCUP E J,et al. Modeling and control design for a turboelectric single aisle aircraft propulsion system[C]//2018 AIAA/IEEE Electric Aircraft Technologies Symposium. Piscataway,US: IEEE,2018: 1-19.
|
| [6] |
NGUYEN N T,REYNOLDS K,TING E,et al. Distributed propulsion aircraft with aeroelastic wing shaping control for improved aerodynamic efficiency[J]. Journal of Aircraft,2018,55(3): 1122-1140.
|
| [7] |
ZHANG Jing,KANG Wenwen,LI Ang,et al. Integrated flight/propulsion optimal control for DPC aircraft based on the GA-RPS algorithm[J]. Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering,2016,230(1): 157-171.
|
| [8] |
雷涛,孔德林,王润龙,等. 分布式电推进飞机动力系统评估优化方法[J]. 航空学报,2021,42(6): 624047. LEI Tao,KONG Delin,WANG Runlong,et al. Evaluation and optimization method for power systems of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica,2021,42(6): 624047. (in Chinese
LEI Tao, KONG Delin, WANG Runlong, et al. Evaluation and optimization method for power systems of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(6): 624047. (in Chinese)
|
| [9] |
达兴亚,范召林,熊能,等. 分布式边界层吸入推进系统的建模与分析[J]. 航空学报,2018,39(7): 122048. DA Xingya,FAN Zhaolin,XIONG Neng,et al. Modeling and analysis of distributed boundary layer ingesting propulsion system[J]. Acta Aeronautica et Astronautica Sinica,2018,39(7): 122048. (in Chinese
DA Xingya, FAN Zhaolin, XIONG Neng, et al. Modeling and analysis of distributed boundary layer ingesting propulsion system[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(7): 122048. (in Chinese)
|
| [10] |
刘沛清. 空气螺旋桨理论及其应用[M]. 北京: 北京航空航天大学出版社,2006.
|
| [11] |
丁兴国,陈昌荣. 民航运输机飞行性能与计划[M]. 北京: 清华大学出版社,2012.
|
| [12] |
刘静,郗超. 民用运输类飞机最大可用速率抬前轮试飞技术研究[J]. 航空科学技术,2015,26(5): 44-47. LIU Jing,XI Chao. Flight test technology of maximum practicable rotation rate for civil transport category airplanes[J]. Aeronautical Science & Technology,2015,26(5): 44-47. (in Chinese
LIU Jing, XI Chao. Flight test technology of maximum practicable rotation rate for civil transport category airplanes[J]. Aeronautical Science & Technology, 2015, 26(5): 44-47. (in Chinese)
|
| [13] |
BORER N K,PATTERSON M D,VIKEN J K,et al. Design and performance of the NASA SCEPTOR distributed electric propulsion flight demonstrator[R]. AIAA 2016-3920,2016.
|
| [14] |
STOLL A M,BEVIRT J,MOORE M D,et al. Drag reduction through distributed electric propulsion [R]. AIAA 2014-2851,2014.
|
| [15] |
JOHNSON W. NDARC NASA design and analysis of rotorcraft[R]. Moffett Field, CA,US: NASA Ames Research Center ARC-E-DAA-TN46522,2017.
|
| [16] |
吴炎烜,范宁军,KOMAROV V A. 机翼载荷传递结构的质量估算[J]. 北京理工大学学报,2008,28(1): 19-23. WU Yanxuan,FAN Ningjun,KOMAROV V A. Mass evaluation for load carrying structures of aircraft wing[J]. Transactions of Beijing Institute of Technology,2008,28(1): 19-23. (in Chinese
WU Yanxuan, FAN Ningjun, KOMAROV V A. Mass evaluation for load carrying structures of aircraft wing[J]. Transactions of Beijing Institute of Technology, 2008, 28(1): 19-23. (in Chinese)
|
| [17] |
刘虎. 飞机总体设计[M]. 北京: 北京航空航天大学出版社,2019.
|
| [18] |
史永运,钟易成,邓君湘,等. 涡轮螺旋桨动力飞机桨发匹配性能仿真研究[J]. 机械制造与自动化,2019,48(4): 116-120. SHI Yongyun,ZHONG Yicheng,DENG Junxiang,et al. Research on prop-engine cooperation performance simulation of propeller powered aircraft[J]. Machine Building & Automation,2019,48(4): 116-120. (in Chinese
SHI Yongyun, ZHONG Yicheng, DENG Junxiang, et al. Research on prop-engine cooperation performance simulation of propeller powered aircraft[J]. Machine Building & Automation, 2019, 48(4): 116-120. (in Chinese)
|
| [19] |
刘远强,郭金锁,项松,等. 基于片条理论的螺旋桨性能计算[J]. 沈阳航空航天大学学报,2013,30(1): 43-46. LIU Yuanqiang,GUO Jinsuo,XIANG Song,et al. Aerodynamic performances calculation of propellers based on standard strip analysis[J]. Journal of Shenyang Aerospace University,2013,30(1): 43-46. (in Chinese
LIU Yuanqiang, GUO Jinsuo, XIANG Song, et al. Aerodynamic performances calculation of propellers based on standard strip analysis[J]. Journal of Shenyang Aerospace University, 2013, 30(1): 43-46. (in Chinese)
|
| [20] |
中国航空工业总公司. 航空发动机手册[M]. 北京: 航空工业出版社,2001.
|
| [21] |
黄波. 无人直升机混合动力驱动技术研究[D]. 成都: 电子科技大学,2018. HUANG Bo. Research on hybrid power driving technology of unmanned helicopter[D]. Chengdu: University of Electronic Science and Technology of China,2018. (in Chinese
HUANG Bo. Research on hybrid power driving technology of unmanned helicopter[D]. Chengdu: University of Electronic Science and Technology of China, 2018. (in Chinese)
|
| [22] |
JOHNSON W,SILVA C,SOLIS E. Concept vehicles for VTOL air taxi operations[R]. Moffett Field, CA,US: NASA Ames Research Center ARC-E-DAA-TN50731, 2018.
|
| [23] |
薛奎举. 分布式油电组合动力无人机设计及性能分析[D]. 沈阳: 沈阳航空航天大学,2018. XUE Kuiju. Design and performance analysis of distributed oil-electricity combined UAV[D]. Shenyang: Shenyang Aerospace University,2018. (in Chinese
XUE Kuiju. Design and performance analysis of distributed oil-electricity combined UAV[D]. Shenyang: Shenyang Aerospace University, 2018. (in Chinese)
|
| [24] |
沈炎宾,陈立桅. 高能量密度动力电池材料电化学[J]. 科学通报,2020,65(增刊1): 117-126. SHEN Yanbin,CHEN Liwei. Materials electrochemistry for high energy density power batteries[J]. Chinese Science Bulletin,2020,65(Suppl. 1): 117-126. (in Chinese
SHEN Yanbin, CHEN Liwei. Materials electrochemistry for high energy density power batteries[J]. Chinese Science Bulletin, 2020, 65(Suppl. 1): 117-126. (in Chinese)
|
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