| Citation: | Li Xinyang, Ren Zongjin, Liu Wei, et al. Modeling and verification of assembly angle error of force measuring components in vector thrust testing system[J]. Journal of Aerospace Power, 2026, 41(8):20240783 doi: 10.13224/j.cnki.jasp.20240783 |
To address the unknown influence mechanism of force component assembly error on test accuracy in the vector thrust testing system, a method for analyzing and modeling the influence rule of force component angle error was proposed. Firstly, the deformation direction mainly affected by the angle error was analyzed. Next, the local analytical deformation model for flexible parts was established to drive the influence law of the angular error on the force measuring components' deformations. The numerical model of the flexible part and the force measuring component was simulated and analyzed. The deformation was calculated with the angle of rotation as the variable. Angular errors on the structure’s mechanical properties were obtained. Finally, the verification experiments of flexible parts and force measuring components were carried out. The deformation properties under different angular errors were analyzed experimentally. Through theoretical analysis, numerical calculation, and experiment, it can be seen that the assembly angular error had little influence on the structural deformation performance. The maximum performance error at different angles was only 4.09%. It showed that the angular error between components can be ignored during the assembly of force measuring components. The research results provide a basis for simplifying the assembly process of the test device.
| [1] |
孙聪. 从空战制胜机理演变看未来战斗机发展趋势[J]. 航空学报, 2021, 42(8): 525826. Sun Cong. Development trend of future fighter: a review of evolution of winning mechanism in air combat[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(8): 525826. (in Chinese
Sun Cong. Development trend of future fighter: a review of evolution of winning mechanism in air combat[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(8): 525826. (in Chinese)
|
| [2] |
Herbst W B. Future fighter technologies[J]. Journal of Aircraft, 1980, 17(8): 561-566. doi: 10.2514/3.44674
|
| [3] |
金鑫, 杨党国, 蔡广平, 等. 先进战斗机武器内埋发展趋势与关键气动问题[J]. 空气动力学学报, 2022, 40(3): 152-159. Jin Xin, Yang Dangguo, Cai Guangping, et al. Key aerodynamic issues and development tendency of internal weapons bay of advanced fighters[J]. Acta Aerodynamica Sinica, 2022, 40(3): 152-159. (in Chinese doi: 10.7638/kqdlxxb-2022.0060
Jin Xin, Yang Dangguo, Cai Guangping, et al. Key aerodynamic issues and development tendency of internal weapons bay of advanced fighters[J]. Acta Aerodynamica Sinica, 2022, 40(3): 152-159. (in Chinese) doi: 10.7638/kqdlxxb-2022.0060
|
| [4] |
朱纪洪, 张尚敏, 周池军, 等. 飞机超机动状态动力学特征及对控制系统的挑战[J]. 控制理论与应用, 2014, 31(12): 1650-1662. Zhu Jihong, Zhang Shangmin, Zhou Chijun, et al. Dynamic characteristics and challenges for control system of super-maneuverable aircraft[J]. Control Theory & Applications, 2014, 31(12): 1650-1662. (in Chinese
Zhu Jihong, Zhang Shangmin, Zhou Chijun, et al. Dynamic characteristics and challenges for control system of super-maneuverable aircraft[J]. Control Theory & Applications, 2014, 31(12): 1650-1662. (in Chinese)
|
| [5] |
郑天慧, 郭琦, 曾海霞, 等. F119核心机研制技术途径及发展趋势[J]. 燃气涡轮试验与研究, 2014, 27(2): 54-58. Zheng Tianhui, Guo Qi, Zeng Haixia, et al. Development approach and derivatives of F119’s core engine[J]. Gas Turbine Experiment and Research, 2014, 27(2): 54-58. (in Chinese
Zheng Tianhui, Guo Qi, Zeng Haixia, et al. Development approach and derivatives of F119’s core engine[J]. Gas Turbine Experiment and Research, 2014, 27(2): 54-58. (in Chinese)
|
| [6] |
范子强, 方振平. 过失速机动飞机的鲁棒非线性控制律设计[J]. 航空学报, 2002, 23(3): 193-196. Fan Ziqiang, Fang Zhenping. Robust, nonlinear control design for a poststall maneuver aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(3): 193-196. (in Chinese
Fan Ziqiang, Fang Zhenping. Robust, nonlinear control design for a poststall maneuver aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(3): 193-196. (in Chinese)
|
| [7] |
张力, 王立新. 推力矢量飞机控制律设计及过失速机动仿真研究[J]. 飞行力学, 2008, 26(4): 1-3, 7. Zhang Li, Wang Lixin. Research on flight control law design of fighter with vectoring thrust and post-stall maneuver simulation[J]. Flight Dynamics, 2008, 26(4): 1-3, 7. (in Chinese doi: 10.13645/j.cnki.f.d.2008.04.002
Zhang Li, Wang Lixin. Research on flight control law design of fighter with vectoring thrust and post-stall maneuver simulation[J]. Flight Dynamics, 2008, 26(4): 1-3, 7. (in Chinese) doi: 10.13645/j.cnki.f.d.2008.04.002
|
| [8] |
Gunzinger M, Rehberg C, Autentied L. Five priorities for the air force’s future combat air force[R]. Washington, DC: Center for Strategic and Budgetary Assessment, 2020.
|
| [9] |
Wright A, Wright A, Born T, et al. Design and calibration of a six degree-of-freedom thrust sensor for a lab-scale hybrid rocket[R]. AIAA-2013-1016, 2013.
|
| [10] |
Araki M, Tsukamoto M, Kojima T, et al. Thrust measurement of a rectangular hypersonic nozzle using an inclined baffle plate[J]. Journal of Propulsion and Power, 2012, 28(6): 1258-1267. doi: 10.2514/1.B34546
|
| [11] |
Miloš P, Davidović N, Jojić B, et al. A novel 6 DOF thrust vector control test stand[J]. Tehnički Vjesnik, 2015, 22(5): 1247-1254. doi: 10.17559/tv-20140621064603
|
| [12] |
王颐, 雷亚琴. 固体火箭发动机多分力测量方法简介[J]. 固体火箭技术, 2000, 23(3): 70-74. Wang Yi, Lei Yaqin. The multi-component measurement for solid rocket motor[J]. Journal of Solid Rocket Technology, 2000, 23(3): 70-74. (in Chinese doi: 10.3969/j.issn.1006-2793.2000.03.016
Wang Yi, Lei Yaqin. The multi-component measurement for solid rocket motor[J]. Journal of Solid Rocket Technology, 2000, 23(3): 70-74. (in Chinese) doi: 10.3969/j.issn.1006-2793.2000.03.016
|
| [13] |
张军, 温晓杰, 李新阳, 等. 矢量推力台架中测力传感器组件的性能仿真与试验[J]. 航空发动机, 2025, 51(2): 137-141. Zhang Jun, Wen Xiaojie, Li Xinyang, et al. Performance simulation and testing of load cell train in vector thrust stand[J]. Aeroengine, 2025, 51(2): 137-141. (in Chinese doi: 10.13477/j.cnki.aeroengine.2025.02.017
Zhang Jun, Wen Xiaojie, Li Xinyang, et al. Performance simulation and testing of load cell train in vector thrust stand[J]. Aeroengine, 2025, 51(2): 137-141. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2025.02.017
|
| [14] |
Wright A M, Wright A B, Born T, et al. A six degree-of-freedom thrust sensor for a labscale hybrid rocket[J]. Measurement Science and Technology, 2013, 24(12): 125104. doi: 10.1088/0957-0233/24/12/125104
|
| [15] |
张有, 吴锋, 何培垒. 航空发动机推力测量台架原理误差分析[J]. 航空发动机, 2016, 42(4): 76-80. Zhang You, Wu Feng, He Peilei. Principle errors analysis of thrust measurement test bench system for aeroengine[J]. Aeroengine, 2016, 42(4): 76-80. (in Chinese
Zhang You, Wu Feng, He Peilei. Principle errors analysis of thrust measurement test bench system for aeroengine[J]. Aeroengine, 2016, 42(4): 76-80. (in Chinese)
|
| [16] |
刘勃锴, 高宏力, 吴颖川, 等. 脉冲燃烧风洞新型悬挂式测力系统[J]. 浙江大学学报(工学版), 2018, 52(4): 619-627. Liu Bokai, Gao Hongli, Wu Yingchuan, et al. New suspension force measuring system in impulse combustion wind tunnel[J]. Journal of Zhejiang University (Engineering Science), 2018, 52(4): 619-627. (in Chinese doi: 10.3785/j.issn.1008-973X.2018.04.002
Liu Bokai, Gao Hongli, Wu Yingchuan, et al. New suspension force measuring system in impulse combustion wind tunnel[J]. Journal of Zhejiang University (Engineering Science), 2018, 52(4): 619-627. (in Chinese) doi: 10.3785/j.issn.1008-973X.2018.04.002
|
| [17] |
张有, 张斌山, 吴锋, 等. 六分力台架设计与矢量推力定位[J]. 航空动力学报, 2019, 34(11): 2324-2330. Zhang You, Zhang Binshan, Wu Feng, et al. Six-component stand design and vector thrust positioning[J]. Journal of Aerospace Power, 2019, 34(11): 2324-2330. (in Chinese
Zhang You, Zhang Binshan, Wu Feng, et al. Six-component stand design and vector thrust positioning[J]. Journal of Aerospace Power, 2019, 34(11): 2324-2330. (in Chinese)
|
| [18] |
吴锋, 杨桥, 张有, 等. 航空发动机矢量推力测量系统的静态校准及不确定度评定方法研究[J]. 测控技术, 2021, 40(1): 83-89. Wu Feng, Yang Qiao, Zhang You, et al. Static calibration and uncertainty evaluation of aero-engine thrust vectoring measurement system[J]. Measurement & Control Technology, 2021, 40(1): 83-89. (in Chinese doi: 10.19708/j.ckjs.2020.07.287
Wu Feng, Yang Qiao, Zhang You, et al. Static calibration and uncertainty evaluation of aero-engine thrust vectoring measurement system[J]. Measurement & Control Technology, 2021, 40(1): 83-89. (in Chinese) doi: 10.19708/j.ckjs.2020.07.287
|
| [19] |
李海涛. 火箭发动机推力矢量测量理论、方法与自动测试技术研究[D]. 长沙: 国防科学技术大学, 2005. Li Haitao. Research on the theory & method of trust vector measurement and the automatic test technology in rocket engine ground test[D]. Changsha: National University of Defense Technology, 2005. (in Chinese
Li Haitao. Research on the theory & method of trust vector measurement and the automatic test technology in rocket engine ground test[D]. Changsha: National University of Defense Technology, 2005. (in Chinese)
|
| [20] |
张龙飞, 胡全星. 固体火箭发动机试车架中板簧弹阻力有限元计算方法[J]. 火炮发射与控制学报, 2015, 36(4): 50-54. Zhang Longfei, Hu Quanxing. The finite element method for calculating elastic resistance of plate spring in SRM test frame[J]. Journal of Gun Launch & Control, 2015, 36(4): 50-54. (in Chinese doi: 10.3969/j.issn.1673-6524.2015.04.011
Zhang Longfei, Hu Quanxing. The finite element method for calculating elastic resistance of plate spring in SRM test frame[J]. Journal of Gun Launch & Control, 2015, 36(4): 50-54. (in Chinese) doi: 10.3969/j.issn.1673-6524.2015.04.011
|
| [21] |
张龙飞. 固体火箭发动机试车架结构分析及其MATLAB实现[D]. 西安: 航天动力技术研究院, 2015. Zhang Longfei. Structure analysis and matlab implementation of solid rocket engine test frame[D]. Xi’an: Academy of Aerospace Solid Propulsion Technology, 2015. (in Chinese
Zhang Longfei. Structure analysis and matlab implementation of solid rocket engine test frame[D]. Xi’an: Academy of Aerospace Solid Propulsion Technology, 2015. (in Chinese)
|
| [22] |
赵磊, 纪明, 王佳, 等. 万向柔性铰链连接快速反射镜的设计与仿真[J]. 红外与激光工程, 2019, 48(2): 0218002. Zhao Lei, Ji Ming, Wang Jia, et al. Design and simulation of fast steering mirrors connected by universal flexure hinges[J]. Infrared and Laser Engineering, 2019, 48(2): 0218002. (in Chinese doi: 10.3788/IRLA201948.0218002
Zhao Lei, Ji Ming, Wang Jia, et al. Design and simulation of fast steering mirrors connected by universal flexure hinges[J]. Infrared and Laser Engineering, 2019, 48(2): 0218002. (in Chinese) doi: 10.3788/IRLA201948.0218002
|
| [23] |
白涛. 六分量试车台结构特性数值模拟研究[D]. 大连: 大连理工大学, 2022. Bai Tao. Numerical simulation research on structural characteristics of six-component test stand[D]. Dalian: Dalian University of Technology, 2022. (in Chinese
Bai Tao. Numerical simulation research on structural characteristics of six-component test stand[D]. Dalian: Dalian University of Technology, 2022. (in Chinese)
|
| [24] |
齐芊枫, 郑椰琴, 吴立伟, 等. 柔性结构技术在精密工件台中的应用[J]. 电子工业专用设备, 2011, 40(9): 1-6, 53. Qi Qianfeng, Zheng Yeqin, Wu Liwei, et al. Application of flexible structure technology in design of wafer stage[J]. Equipment for Electronic Products Manufacturing, 2011, 40(9): 1-6, 53. (in Chinese
Qi Qianfeng, Zheng Yeqin, Wu Liwei, et al. Application of flexible structure technology in design of wafer stage[J]. Equipment for Electronic Products Manufacturing, 2011, 40(9): 1-6, 53. (in Chinese)
|
| [25] |
Li Xinyang, Ren Zongjin, Zhang Jun, et al. Research on the performance of force measuring component–the key unit of vector thrust measuring system[J]. Measurement, 2024, 235: 115017. doi: 10.1016/j.measurement.2024.115017
|