| Citation: | QI Haitao, LIU Xu, LIU Duo, et al. Multi-objective optimization design of binary variable geometry inlet regulating mechanism for aircraft[J]. Journal of Aerospace Power, 2025, 40（1）：20230118 doi: 10.13224/j.cnki.jasp.20230118
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Considering the design requirements of hypersonic aircraft’s binary variable geometry inlet regulating mechanism for light weight, low energy consumption and high accuracy, multi-objective optimization was carried out for the mechanism, the design scheme with the best comprehensive performance was obtained and the feasibility of the scheme was verified. Firstly, through force analysis and ADAMS software simulation, the minimum driving force required for the wedge plate and throat plate was obtained. Then the mathematical model of the mass, energy consumption and stiffness of the mechanism was established, the design variables and constraints of the mechanism were determined, and the Pareto solution set was obtained by multi-objective optimization using NSGA-Ⅱ optimization algorithm. The visualization of Pareto frontier was realized by drawing the level diagram, and a group of optimal solutions were selected for the design scheme. Finally, the feasibility of the scheme was verified by mechatronics concept designer (MCD) kinematics simulation analysis. The results showed that the weight of the mechanism was reduced by 6.48% and the energy consumption reduced by 8.35% compared with that before optimization, and also it can meet the displacement demand of actuation.
| [1] |
FIELDING J P. Introduction to aircraft design[M]. Cambridge,UK: Cambridge University Press,1999.
|
| [2] |
齐伟呈,程思野,李堃. 高超声速飞行器及推进系统研究进展[J]. 科技创新与应用,2022,12(31): 18-21. QI Weicheng,CHENG Siye,LI Kun. Research progress of hypersonic vehicle and propulsion system[J]. Technology Innovation and Application,2022,12(31): 18-21. (in Chinese
QI Weicheng, CHENG Siye, LI Kun. Research progress of hypersonic vehicle and propulsion system[J]. Technology Innovation and Application, 2022, 12(31): 18-21. (in Chinese)
|
| [3] |
王渊,田巨,邓君香,等. 高超声速飞行器进气道技术研究进展[J]. 飞航导弹,2019(4): 56-61. WANG Yuan,TIAN Ju,DENG Junxiang,et al. Research progress of hypersonic vehicle inlet technology[J]. Aerodynamic Missile Journal,2019(4): 56-61. (in Chinese
WANG Yuan, TIAN Ju, DENG Junxiang, et al. Research progress of hypersonic vehicle inlet technology[J]. Aerodynamic Missile Journal, 2019(4): 56-61. (in Chinese)
|
| [4] |
KOBAYASH H,MARU Y,HONGOH M,et al. Study on variable-shape supersonic inlets and missiles with MRD device[J]. Acta Astronautica,2006,61(11): 978-988.
|
| [5] |
HIDEYUKI T,HISAO F,KAZUO S,et al. Design study on hypersonic engine components for TBCC space planes[C]//12th AIAA International Space Planes and Hypersonic Systems and Technologies. Virginia,US: AIAA,2012: 1-10.
|
| [6] |
蒲永彬. 一体化二元变几何进气道设计及气动性能研究[D]. 南京: 南京航空航天大学,2018. PU Yongbin. Variable geometry design and aerodynamic performance research of integrated two-dimensional inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2018. (in Chinese
PU Yongbin. Variable geometry design and aerodynamic performance research of integrated two-dimensional inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2018. (in Chinese)
|
| [7] |
李永洲,李光熙,刘晓伟,等. 马赫数1.5~4.5的曲面轴对称变几何进气道设计[J]. 火箭推进,2018,44(4): 30-35. LI Yongzhou,LI Guangxi,LIU Xiaowei,et al. Design of a curved axisymmetric variable geometry inlet with Mach number from 1.5 to 4.5[J]. Journal of Rocket Propulsion,2018,44(4): 30-35. (in Chinese doi: 10.3969/j.issn.1672-9374.2018.04.005
LI Yongzhou, LI Guangxi, LIU Xiaowei, et al. Design of a curved axisymmetric variable geometry inlet with Mach number from 1.5 to 4.5[J]. Journal of Rocket Propulsion, 2018, 44(4): 30-35. (in Chinese) doi: 10.3969/j.issn.1672-9374.2018.04.005
|
| [8] |
刘天赐. 某型飞机进气道气流调节装置的优化设计与性能分析[D]. 哈尔滨: 哈尔滨工业大学,2021. LIU Tianci. Optimized design and performance analysis of air flow regulating device in an aircraft inlet[D]. Harbin: Harbin Institute of Technology,2021. (in Chinese
LIU Tianci. Optimized design and performance analysis of air flow regulating device in an aircraft inlet[D]. Harbin: Harbin Institute of Technology, 2021. (in Chinese)
|
| [9] |
于波,吴帅,尚耀星,等. 电静液作动器多目标优化设计[J]. 液压与气动,2018(5): 26-31. YU Bo,WU Shuai,SHANG Yaoxing,et al. The study of multi-objective optimization design of EHA[J]. Chinese Hydraulics & Pneumatics,2018(5): 26-31. (in Chinese doi: 10.11832/j.issn.1000-4858.2018.05.005
YU Bo, WU Shuai, SHANG Yaoxing, et al. The study of multi-objective optimization design of EHA[J]. Chinese Hydraulics & Pneumatics, 2018(5): 26-31. (in Chinese) doi: 10.11832/j.issn.1000-4858.2018.05.005
|
| [10] |
李海旺,张大伟,由儒全. 考虑热应力的冲击发散冷却结构参数敏感性分析及优化设计[J]. 航空动力学报,2022,37(11): 2455-2464. LI Haiwang,ZHANG Dawei,YOU Ruquan. Sensitivity analysis and optimal design of impingement/effusion cooling structural parameters considering thermal stress[J]. Journal of Aerospace Power,2022,37(11): 2455-2464. (in Chinese
LI Haiwang, ZHANG Dawei, YOU Ruquan. Sensitivity analysis and optimal design of impingement/effusion cooling structural parameters considering thermal stress[J]. Journal of Aerospace Power, 2022, 37(11): 2455-2464. (in Chinese)
|
| [11] |
高吴浩,陈永琴,苏三买,等. 反推力装置结构优化设计[J]. 航空动力学报,2022,37(8): 1724-1731. GAO Wuhao,CHEN Yongqin,SU Sanmai,et al. Structural optimization design of thrust reverser[J]. Journal of Aerospace Power,2022,37(8): 1724-1731. (in Chinese
GAO Wuhao, CHEN Yongqin, SU Sanmai, et al. Structural optimization design of thrust reverser[J]. Journal of Aerospace Power, 2022, 37(8): 1724-1731. (in Chinese)
|
| [12] |
BUDINGER M,LISCOUËT J,HOSPITAL F,et al. Estimation models for the preliminary design of electromechanical actuators[J]. Proceedings of the Institution of Mechanical Engineers: Part G Journal of Aerospace Engineering,2012,226(3): 243-259.
|
| [13] |
闻邦椿. 机械设计手册[M]. 5版. 北京: 机械工业出版社,2010. WEN Bangchun. Mechanical design manual[M]. 5th ed. Beijing: China Machine Press,2010. (in Chinese
WEN Bangchun. Mechanical design manual[M]. 5th ed. Beijing: China Machine Press, 2010. (in Chinese)
|
| [14] |
李倩. 电动执行器能耗模型的建立与分析[D]. 成都: 电子科技大学,2015. LI Qian. Modeling and analyzing of energy consumption of electric actuator[D]. Chengdu: University of Electronic Science and Technology of China,2015. (in Chinese
LI Qian. Modeling and analyzing of energy consumption of electric actuator[D]. Chengdu: University of Electronic Science and Technology of China, 2015. (in Chinese)
|
| [15] |
FRANCISCO S,NORBERTO C,NARANJO JOSÉ E. Optimization of the energy consumption of electric motors through metaheuristics and PID controllers[J]. Electronics,2020,9(11): 1842. doi: 10.3390/electronics9111842
|
| [16] |
尚玲玲,王海峰,口启慧,等. 平流层飞艇三叶螺旋桨结构优化方法[J]. 航空动力学报,2022,37(8): 1714-1723. SHANG Lingling,WANG Haifeng,KOU Qihui,et al. Structure optimization method of three-blade propeller for stratospheric airship[J]. Journal of Aerospace Power,2022,37(8): 1714-1723. (in Chinese
SHANG Lingling, WANG Haifeng, KOU Qihui, et al. Structure optimization method of three-blade propeller for stratospheric airship[J]. Journal of Aerospace Power, 2022, 37(8): 1714-1723. (in Chinese)
|
| [17] |
TIAN Ye,CHENG Ran,ZHANG Xingyi,et al. PlatEMO: a MATLAB platform for evolutionary multi-objective optimization[educational forum][J]. IEEE Computational Intelligence Magazine,2017,12(4): 73-87. doi: 10.1109/MCI.2017.2742868
|
| [18] |
杨弘枨,刘山,靳广在,等. 基于遗传算法优化小波网络的柔性喷管力矩特性辨识方法[J]. 航空动力学报,2022,37(9): 1936-1945. YANG Hongcheng,LIU Shan,JIN Guangzai,et al. Identification of flexible nozzle torque properties based on wavelet neural network optimized by genetic algorithm[J]. Journal of Aerospace Power,2022,37(9): 1936-1945. (in Chinese
YANG Hongcheng, LIU Shan, JIN Guangzai, et al. Identification of flexible nozzle torque properties based on wavelet neural network optimized by genetic algorithm[J]. Journal of Aerospace Power, 2022, 37(9): 1936-1945. (in Chinese)
|
| [19] |
杨洪涛,游广飞,徐亮,等. 超声速风洞喷管冷却结构的多目标优化设计[J]. 航空动力学报,2023,38(5): 1047-1057. YANG Hongtao,YOU Guangfei,XU Liang,et al. Multi-objective optimization design of supersonic wind-tunnel nozzle cooling structure[J]. Journal of Aerospace Power,2023,38(5): 1047-1057. (in Chinese
YANG Hongtao, YOU Guangfei, XU Liang, et al. Multi-objective optimization design of supersonic wind-tunnel nozzle cooling structure[J]. Journal of Aerospace Power, 2023, 38(5): 1047-1057. (in Chinese)
|
| [20] |
BLASCO X,HERRERO J M,SANCHIS J,et al. A new graphical visualization of n-dimensional Pareto front for decision-making in multiobjective optimization[J]. Information Sciences,2008,178(20): 3908-3924. doi: 10.1016/j.ins.2008.06.010
|
| [21] |
孟庆波. 生产线数字化设计与仿真(NX MCD)[M]. 北京: 机械工业出版社,2020. MENG Qingbo. Digital design and simulation of production line (NX MCD)[M]. Beijing: China Machine Press,2020. (in Chinese
MENG Qingbo. Digital design and simulation of production line (NX MCD)[M]. Beijing: China Machine Press, 2020. (in Chinese)
|
| [22] |
WANG Jujie,DAI Chunxiang,SHI Karen,et al. Research on rigid body motion tracing in space based on NX MCD[C]//Proceedings of International Conference on Robotics and Mechatronics (ICROM). Hong Kong,China: The Institute of Physics (IOP),2018: 1-7.
|
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