基于弹性阻尼的全机疲劳试验约束点动态载荷抑制方法

doi:10.7527/S1000-6893.2025.32283

Abstract

Abstract:

To address the problem of structural fatigue failure at the constraint locations caused by dynamic loads exceeding tolerance limits at the constraint points in full-scale aircraft fatigue tests， the main factors contributing to dynamic load imbalance at the constraint points are studied. The excitation-response characteristics of multi-channel coordinated loading control and the structural dynamic load response process are analyzed. It is revealed that the coupling between the excitation-response phase difference of the control system and the structural dynamic response is the primary cause of the imbalanced dynamic load at the constraint points. Based on the fundamental principle of damping control， an elastic damping constraint method is proposed， and an elastic damping constraint device is designed. The feasibility of the method is demonstrated through structural strength analysis， flow field analysis and transient dynamic simulation， and the optimal ranges for key design parameters are determined. The method and device are validated in the full-scale fatigue test of a certain aircraft model. The results show that the elastic damping constraint effectively reduces the dynamic load imbalance during testing. The research findings are widely applicable to the full-scale fatigue tests of other aircraft models.

Key words: full-scale aircraft structure, fatigue test, constraint point, elastic damping constraint, dynamic load suppression

CLC Number:

V216.1⁺1

Jianjun ZHENG, Mengmeng WANG, Bin MU, Sha WEI. Dynamic load suppression method for constraint point in full-scale aircraft fatigue test using elastic damping[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(21): 532283.

Figures/Tables 14

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References 35

[1]	中国民用航空局. 中国民用航空规章-第25部-运输类飞机适航标准： CCAR-25-R4 ［S］. 北京：中国民用航空局政策法规司， 2016．
	China Civil Aviation Administration. China civil aviation regulations-Part 25-Airworthiness standards for transport aircraft： CCAR-25-R4 ［S］. Beijing： Policy and Regulation Department， China Civil Aviation Administration， 2016 （in Chinese）.
[2]	王彬文，王育鹏. 飞机强度试验［M］. 北京：航空工业出版社， 2021．
	WANG B W， WANG Y P. Aircraft strength tests［M］. Beijing： Aviation Industry Press， 2021 （in Chinese）.
[3]	孙侠生，苏少普，孙汉斌，等. 国外航空疲劳研究现状及展望［J］. 航空学报， 2021， 42（5）： 524791.
	SUN X S， SU S P， SUN H B， et al. Current status and prospect of overseas research on aeronautical fatigue［J］. Acta Aeronautica et Astronautica Sinica， 2021， 42（5）： 524791 （in Chinese）.
[4]	王彬文，陈先民，苏运来，等. 中国航空工业疲劳与结构完整性研究进展与展望［J］. 航空学报， 2021， 42（5）： 524651.
	WANG B W， CHEN X M， SU Y L， et al. Research progress and prospect of fatigue and structural integrity for aeronautical industry in China［J］. Acta Aeronautica et Astronautica Sinica， 2021， 42（5）： 524651 （in Chinese）.
[5]	ARDIANTO Y， BÖSCH P， NIELSEN T. Test program for the A380 major fatigue test［C］∥Symposium of the International Committee on Aeronautical Fatigue. 2005： 8-10.
[6]	田文朋，宋鹏飞，夏峰，等. 民机疲劳试验载荷谱简化研究与验证［J］. 机床与液压， 2022， 50（7）： 78-81．
	TIAN W P， SONG P F， XIA F， et al. Research and verification on load spectrum simplification of civil aircraft fatigue test［J］. Machine Tool & Hydraulics， 2022， 50（7）： 78-81 （in Chinese）.
[7]	HEALEY R， WANG J， CHIU W K， et al. A review on aircraft spectra simplification techniques for composite structures ［J］. Composites Part C： Open Access， 2021， 5： 100131.
[8]	JOO Y S， LEE W J， SEO B H， et al. Introduction of developing fatigue load spectrum for full-scale fatigue test of composite aircraft［J］. International Journal of Aeronautical and Space Sciences， 2020， 21： 681-692.
[9]	ALI D， SHAHZAD A， KHAN T A. Development of fatigue loading spectra from flight test data［J］. Procedia Structural Integrity， 2016， 2： 3296-3304.
[10]	张立新. 全机疲劳试验几个问题的探讨［J］. 航空工程进展， 2024， 15（4）： 10-15， 26.
	ZHANG L X. Discussions on some problems of full-scale aircraft fatigue test［J］. Advances in Aeronautical Science and Engineering， 2024， 15（4）： 10-15， 26 （in Chinese）.
[11]	刘春艳，唐吉运，强宝平，等. 全机结构疲劳试验载荷优化技术模拟研究［J］. 科学技术与工程， 2019， 19（7）： 284-288.
	LIU C Y， TANG J Y， QIANG B P， et al. Simulation study on full-scale aircraft structure fatigue test load optimization technology［J］. Science Technology and Engineering， 2019， 19（7）： 284-288 （in Chinese）.
[12]	贺谦. 飞机结构疲劳试验载荷处理系统架构设计［J］. 电子技术与软件工程， 2020（6）： 70-72.
	HE Q. Architecture design of load processing system for aircraft structural fatigue test ［J］. Electronic Technology & Software Engineering， 2020（6）： 70-72 （in Chinese）.
[13]	孟繁沛，王建邦，李令芳，等. 飞机结构疲劳试验载荷的优化设计［J］. 航空学报， 2001， 22（6）： 553-555．
	MENG F P， WANG J B， LI L F， et al. Optimum design of fatigue testing loads for airplane structures［J］. Acta Aeronautica et Astronautica Sinica， 2001， 22（6）： 553-555 （in Chinese）.
[14]	牧彬. 基于特征根的结构强度试验控制系统参数优化［J］. 工程与试验， 2020， 60（1）： 4-5， 42.
	MU B. Parameter optimization of structural strength test control system based on characteristic root［J］. Engineering & Test， 2020， 60（1）： 4-5， 42 （in Chinese）.
[15]	GOWTHAM G， JAGAN RAJ R. Mathematical modelling and PID control system implementation for quadcopter frame Tarot FY650［J］. Aircraft Engineering Aerospace Technology： An International Journal， 2024， 96（2）：273-284.
[16]	赵洪伟，冯建民，韩涛，等. 多通道结构疲劳试验系统闭环交叉补偿控制［J］. 控制工程， 2021， 28（2）： 395-400．
	ZHAO H W， FENG J M， HAN T， et al. Closed-loop cross-compensation control for multi-channel structural fatigue testing system［J］. Control Engineering of China， 2021， 28（2）： 395-400 （in Chinese）.
[17]	王刚，宋鹏飞，张柁. 多系统复杂机构试验同步控制技术研究［J］. 今日制造与升级， 2024（3）： 169-171.
	WANG G， SONG P F， ZHANG T. Research on synchronization control technology of multi-system complex mechanism test［J］. Manufacturing and Upgrading Today， 2024（3）： 169-171 （in Chinese）.
[18]	刘振宇，米征. 机翼疲劳试验控制精度提升方法研究［J］. 计算机测量与控制， 2020， 28（6）： 252-256， 275.
	LIU Z Y， MI Z. Research on Method of Improving control accuracy of wing fatigue test［J］. Computer Measurement & Control， 2020， 28（6）： 252-256， 275 （in Chinese）.
[19]	刘振宇. 基于加载频率的飞机结构疲劳试验谱优化研究［J］. 今日制造与升级， 2021（9）： 46-48， 51.
	LIU Z Y. Optimization of fatigue test spectra of aircraft structures based on loading frequency［J］. Manufacturing & Upgrading Today， 2021（9）： 46-48， 51 （in Chinese）.
[20]	吝继锋，陈戈，冯建民. 大变形结构地面强度试验应急卸载控制技术研究［J］. 工程与试验， 2020， 60（4）： 37-40.
	LIN J F， CHEN G， FENG J M. Research on control technology for emergency unload in ground strength test of large deformation structure［J］. Engineering & Test， 2020， 60（4）： 37-40 （in Chinese）.
[21]	GAO X S， YOU S， SCHULTZ A， et al. Development of high performance multi-axial hybrid simulation system for full-scale testing［C］∥ 12th Canadian Conference on Earthquake Engineering. 2019：1-8.
[22]	YANG M S， JEONG J G， SEOL C W， et al. Technical papers： Floating set-up method for full scale airframe durability test［J］. Journal of the Korean Society for Aeronautical & Space Sciences， 2004， 32（2）： 88-94.
[23]	SCHORR F， TUSCH O， WU D， et al. Fatigue testing of new generation wide body aircraft at benchmark level ［C］∥35th ICAF Conference and 29th ICAF Symposium： ICAF 2017. 2017.
[24]	ZHENG J J， WANG B W， ZHU L G， et al. Research on attitude control and constraint system design of full-scale aircraft static test based on barycenter［C］∥32nd Congress of the International Council of the Aeronautical Sciences. 2021.
[25]	裴连杰，郭俊毫，郑建军. 新型战斗机全机疲劳试验飞机支持系统设计［J］. 今日制造与升级， 2020（8）： 66-68.
	PEI L J， GUO J H， ZHENG J J. Design of aircraft support system for full-scale fatigue test of new fighter jet［J］. Manufacturing & Upgrading Today， 2020（8）： 66-68 （in Chinese）.
[26]	王鑫涛，杜星. 飞机结构强度试验应急载荷限定系统［J］. 航空学报， 2020， 41（2）： 223332.
	WANG X T， DU X. Emergency load limited system for aircraft structural strength test［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（2）： 223332 （in Chinese）.
[27]	ZHENG J J， JIN F， WANG B， et al. Research on automatic attitude control technology of six-degree-of-freedom displacement compensation for full-scale aircraft static test ［J］. Experimental Techniques， 2025： 1-18 （in press）.
[28]	崔明，冯建民，米征，等. 大型无人机主结构耐久性试验加载技术［J］. 航空学报， 2022， 43（6）： 525887.
	CUI M， FENG J M， MI Z， et al. Loading technology for main structure of large UAV durability test［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（6）： 525887 （in Chinese）.
[29]	郭琼，刘玮，裴连杰，等. 全尺寸复合材料机身筒段静力/疲劳试验技术［J］. 航空学报， 2022， 43（6）： 525816.
	GUO Q， LIU W， PEI L J， et al. Static and fatigue test technology for full-scale composite fuselage barrels［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（6）： 525816 （in Chinese）.
[30]	裴连杰，王育鹏，张建锋，等. 战斗机全机疲劳试验技术发展概述［J］. 航空工程进展， 2023， 14（2）： 136-144.
	PEI L J， WANG Y P， ZHANG J F， et al. Overview of the development of full-scale fatigue test technology for fighter［J］. Advances in Aeronautical Science and Engineering， 2023， 14（2）： 136-144 （in Chinese）.
[31]	王育鹏，裴连杰，李秋龙，等. 新一代战斗机全机地面强度试验技术［J］. 航空学报， 2020， 41（6）： 523482.
	WANG Y P， PEI L J， LI Q L， et al. Full-scale aircraft strength test technology of next generation fighter［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（6）： 523482 （in Chinese）.
[32]	HILFER G， TUSCH O， WU D， et al. Changing the philosophy of full-scale-fatigue-tests derived from 50 years of IABG experience towards a virtual environment［C］∥ICAF 2019-Structural Integrity in the Age of Additive Manufacturing. 2019： 723-735.
[33]	CHIARIELLO A， PERILLO G， LINARI M， et al. Virtual full scale static test of a civil tilt rotor composite wing in non-linear regime［J］. Aerospace Engineering Technology， 2024， 11（4）： 278.
[34]	王彬文，聂小华，万春华，等. 全机静强度虚拟试验技术研究及应用［J］. 航空学报， 2022， 43（6）： 526273.
	WANG B W， NIE X H， WAN C H， et al. Research and application of virtual test technology for static strength of full scale aircraft structure［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（6）： 526273 （in Chinese）.
[35]	丁兰，杨吉新，朱伟伟. 基于粘滞阻尼器不同计算模型的斜拉桥地震反应分析［J］. 中外公路， 2011， 31（2）： 140-145.
	DING L， YANG J X， ZHU W W. Seismic response analysis of cable-stayed bridges based on different computational models of viscous dampers［J］. Journal of China & Foreign Highway， 2011， 31（2）： 140-145 （in Chinese）.

Dynamic load suppression method for constraint point in full-scale aircraft fatigue test using elastic damping

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