高温环境下结构模态试验技术

doi:10.6052/1000-0879-17-288

Abstract

Abstract:

Since the hypersonic vehicle is acted by a serious aerodynamic thermal load caused by the flight through the atmosphere, it is necessary to consider the effect of the high temperature in the ground test of the vehicle structures. But the structural modal experiment in a high temperature environment is far more complex than the normal modal experiment with many technical difficulties to be solved. In this paper, the advance of the thermal modal test technology is reviewed. The characteristics and the applicability of the excitation and measurement techniques to be used in the high temperature environment are discussed in detail. The development direction and the research focus of the structural modal test technology in the high temperature environment are suggested.

Key words:

hypersonic flight|high temperature environment|thermal modal test|test technique

CLC Number:

TH212

YU Kaiping, BAI Yunhe, ZHAO Rui, ZHOU Haotian. ADVANCE OF EXPERIMENTAL TECHNOLOGIES FOR STRUCTURAL MODAL TEST IN HIGH TEMPERATURE ENVIRONMENTS[J].Mechanics in Engineering, 2018, 40(1): 1-12.

References

[1] 杨亚政, 杨嘉陵, 方岱宁. 高超声速飞行器热防护材料与结构的研究进展. 应用数学和力学, 2008,29(1): 47-56
[2] Douglas D.Hypersonic international flight research and experimentation (HIFiRE)---fundamentalsciences and technology development strategy. 15th AIAA/AAAF International Conference, Dayton,Ohio, 2008
[3] 蒋持平,柴慧,严鹏. 近空间高超声速飞行器防热隔热与热力耦合研究进展. 力学与实践, 2011, 33(1): 1-9
[4] Mcnamara J, Friedmann P.Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present and future. AIAA Journal, 2011, 49(6): 1089-1122
[5] 陈予恕, 郭虎伦, 钟顺. 高超声速飞行器若干问题研究进展. 飞航导弹, 2009, (8): 26-33
[6] George C.NASA's space launch initiative: the next generation launch technology program. Huntsville, Marshall Space Flight Center, 2003
[7] Stephens C, Hudson L, Piazza A.Overview of an advanced hypersonic structural concept test program.Fundamental Aeronautics Program Annual Meeting, New Orleans, 2007
[8] Spivey ND.High-temperature modal survey of a hot-structure control surface. 27th International Congress of the Aeronautical Sciences, Nice, 2010
[9] Hudson L, Stephens C.X-37 C/SiC Ruddervator Subcomponent Test Program. NASA Dryden Flight Research Center, 2009
[10] Wu D, Wang Y, Shang L, et al.Experimental and computational investigations of thermal modal parameters for a plate-structure under 1 200\(^\circ\)C high temperature environment. Measurement,2016, 94: 80-91
[11] 吴大方,赵寿根,潘兵等.高速巡航导弹翼面结构热-振联合试验研究. 航空学报, 2012, 33(9):1633-1642
[12] Mohammadali M, Ahmadian H.Improvement in modal testing measurements by modeling and identification of shaker--stinger--structure interactions. Experimental Techniques, 2016, 40(1): 49-57
[13] 麻连净, 蔡骏文. 导弹舵面热模态试验激振方法研究. 战术导弹技术, 2013 (6): 20-25
[14] 苏华昌,骞永博,李增文等. 舵面热模态试验技术研究. 强度与环境, 2011, 38(5): 18-24
[15] 王应奇. 高温环境结构振动试验技术研究. [硕士论文]. 哈尔滨: 哈尔滨工业大学, 2012
[16] 东巳宙. 高温环境下复合材料层合板与蜂窝板力学性能分析. [硕士论文]. 哈尔滨: 哈尔滨工业大学, 2016
[17] Yu K, Yang K, Bai Y.Estimation of modal parameters using the sparse component analysis based underdetermined blind source separation. Mechanical Systems and Signal Processing, 2014, 45(2): 302
[18] 杨凯. 仅利用输出响应的时变模态参数辨识方法研究. [博士论文]. 哈尔滨: 哈尔滨工业大学, 2014
[19] Yu K, Yang K, Bai Y.Experimental investigation on the time-varying modal parameters of a trapezoidal plate in temperature-varying environments by subspace tracking-based method. Journal of Vibration and Control, 2015, 21(16): 3305-3319
[20] 吴家驹, 苏华昌, 王晓晖. 基础激励结构的试验模态分析. 强度与环境, 2010, 36(4): 28-35
[21] 胡秋霞. 热环境下基础激励结构模态参数识别研究. [硕士论文]. 南京: 南京航空航天大学, 2014
[22] 周思达,刘莉,杨武等. 基于响应传递率的非白随机激励仅输出结构模态参数辨识. 振动与冲击, 2014, 33(23):47-52,67
[23] Dumont M, Cook A, Kinsley N.Acceleration Measurement Optimization: mounting Considerations and Sensor Mass Effect//Mains M, ed. Conference Proceedings of the Society for Experimental Mechanics 2016. New York: Springer, 2016
[24] 李德葆, 诸葛鸿程, 王波. 实验应变模态分析原理和方法. 清华大学学报(自然科学版), 1990, 30(2): 105-112
[25] 陆秋海, 李德葆. 模态理论的进展. 力学进展, 1996, 26(4): 464-472
[26] Dos Santos FLM, Peeters B, Desmet W, et al.Strain-based experimental modal analysis on planar structures: Concepts and practical aspects//Mains M, ed. Topic in Modal Analysis and Testing. New York:Springer, 2016
[27] Kranjc T, Slavi\u{c}J, Bolte\u{z}ar M. A comparison of strain and classic experimental modal analysis. Journal of Vibration and Control, 2016, 22(2): 37381
[28] Ma L, Wu T, Zhao L.Development of temperature- compensated resistance strain gages for use to 700\(^\circ\)C. Experimental Techniques, 1990, 30(1): 17
[29] Lei J.Development and characterization of PdCr temperature-compensated wire resistance strain gage. NASA STI/Recon Technical Report N, 1989
[30] Hudson LD.Hostile environments and high temperature measurements. The Conference of Experiment Mechanics, Kansas City,MO, 1989
[31] Lei JF, Okimura H, Brittain JO.Evaluation of some thin film transition metal compounds for high temperature resistance strain gauge application. Materials Science & Engineering A, 1989,111(89): 145-154
[32] 吴东, 陈德江, 周玮等. 高热环境下前缘结构高温应变测量. 实验流体力学, 2016, 30(3): 92-97
[33] Piazza A, Hudson LD, Richards WL.Development and ground-test validation of fiber optic sensor attachment techniques for hot structures applications. NASA Dryden Flight Research Center, 2005
[34] Piazza A, Richards LW, Hudson LD.High-temperature strain sensing for aerospace applications. NASA Dryden Flight Research Center, 2008
[35] Tahir BA, Ali J, Rahman RA.Strain measurements using fiber bragg grating sensor. American Journal of Applied Science, 2005, (Sp.issue): 40-48
[36] Liu JG, Schmidt-Hattenberger C, Borm G.Dynamic strain measurement with a fiber bragg grating sensor system. Measurement, 2002, 32(2): 15161
[37] Lee S, Ahn K, Sirkis J.Planar optical waveguide temperature sensor based on etched Bragg gratings considering nonlinear thermo-optic effect. KSME International Journal, 2001, 15(3): 309-319
[38] Adamovsky G, Mackey JR, Kren LA, et al.Development and performance verification of fiber optic temperature sensors in high temperature engine environments. AIAA Propulsion and Energy Conference, Cleveland, OH, 2014
[39] Pena F, Richards WL, Piazza A, et al.Fiber-optic sensing for in-space inspection. NASA Armstrong Flight Research Center, 2014
[40] 崔嵩. 基于激光非接触测量的热模态试验技术. [硕士论文]. 南京: 南京航空航天大学, 2012
[41] Jin H, Sciammarella C, Yoshida S, et al.Advancement of Optical Methods in Experimental Mechanics. New York: Springer, 2015
[42] 刘浩,李晓东,杨文岐等. 考虑气动加热的翼面结构热模态试验方法研究. 振动与冲击, 2015, (13): 101-108
[43] Ewins D.Modal analysis and modal testing//Crocker MJ, ed. Handbook of Noise and Vibration Control. Hoboken: John Wiley & Sons, Inc., 2007, 565-574
[44] Ehrhardt D, Yang S, Beberniss T, et al.Linear and nonlinear response of a rectangular plate measured with continuous-scan laser Doppler vibrometry and 3D-digital image correlation//Zimmerman KB, ed. Conference Proceeding of the Society for Experimental Mechanics 2015, New York: Springer, 2015
[45] Lal A, Hess C, Zhang H, et al.Multi-beam heterodyne laser doppler vibrometer: US, US 6972846 B2, 2005
[46] Pingle P, Sailhamer J, Avitabile P.Comparison of 3D laser vibrometer and accelerometer frequency measurements. The IMAC XXVII, Orlando,Florida, 2009
[47] Warren C, Niezrecki C, Avitabile P, et al.Comparison of FRF measurements and mode shapes determined using optically image based, laser, and accelerometer measurements. Mechanical Systems and Signal Processing, 2011, 25(6): 2192202
[48] 陈骥, 王鑫, 曹久大等. 高速CCD激光位移传感器. 光学精密工程, 2008, 16(4): 611-616
[49] Pan B, Wang Y, Tian L.Automated initial guess in digital image correlation aided by Fourier--Mellin transform. Optical Engineering, 2017, 56(1): 14103
[50] Luo P, Chao Y, Sutton M, et al.Accurate measurement of three-dimensional deformations in deformable and rigid bodies using computer vision. Experimental Mechanics, 1993, 3(2): 123-132
[51] Hild F, Roux S.Digital image correlation: from displacement measurement to identification of elastic properties---A review. Strain, 2005, 42(2): 69-80
[52] 王伟. 数字图像相关方法在热结构材料高温变形测试中的应用. [硕士论文]. 哈尔滨: 哈尔滨工业大学, 2014
[53] 张蕊. 数字图像相关及其在若干工程测试中的应用. [博士论文]. 广州: 华南理工大学, 2011
[54] 王翔,高速高温数字图像相关方法及热冲击实验研究. [硕士论文]. 北京: 清华大学,2010
[55] Paulsen U, Erne O, M\"{o}ller T, et al. Wind turbine operational and emergency stop measurements using point tracking videogrammetry. SEM Annual Conference and Exposition on Experimental and Applied Mechanics, Albuquerque, NM, 2009
[56] 潘兵, 吴大方, 谢惠民等. 基于梯度的数字体图像相关方法测量物体内部变形. 光学学报, 2011, 31(6): 120-126
[57] Pan B, Wu D, Wang Z, et al.High-temperature digital image correlation method for full-field deformation measurement at 1200\(^\circ\)C. Measurement science and technology, 2011, 22: 15701
[58] Avitabile P, Niezrecki C, Helfrick M, et al.Noncontact measurement techniques for model correlation.Sound and Vibration, 2010, (1): 8-12
[59] 黄亿辉,袁武,宋宏伟等. CW激光辐照薄板热力响应全场测量. 强激光与粒子束,2014, 26(11): 111012
[60] 潘兵, 江天云, 吴大方. 时变热辐射环境下高温合金蜂窝板三维热变形测量. 北京航空航天大学学报, 2015,41(6): 969-975
[61] Zhu FP, Bai PX, Zhang JB, et al.Measurement of true stress--strain curves and evolution of plastic zone of low carbon steel under uniaxial tension using digital image correlation. Optics and Lasers in Engineering, 2015, 65(2): 81-88
[62] 李婧宇,朱飞鹏,雷冬. 三维DIC在铸铁拉伸试验中的应变测量精度研究. 力学季刊, 2015, 36(3): 434-441
[63] 潘兵,吴大方,高镇同等. 1 200\(^\circ\)C高温热环境下全场变形的非接触光学测量方法研究. 强度与环境, 2011, 38(1): 52-59
[64] Helfrick M, Niezrecki C, Avitabile P, et al.3D digital image correlation methods for full-field vibration measurement. Mechanical Systems and Signal Processing, 2011, 25(3): 917-927
[65] Patterson E.Challenges in experimental strain analysis: interfaces and temperature extremes. The Journal of Strain Analysis for Engineering Design, 2015, 50(5): 282-283
[66] 董维中, 高铁锁, 丁明松等. 高超声速飞行器表面温度分布与气动热耦合数值研究. 航空学报, 2015, 36(1):31324
[67] 刘宝瑞,孔凡金,张伟等. C/SiC舵结构热试验瞬态温度场预示技术. 强度与环境, 2015, (1): 40-45
[68] 吴大方,潘兵,郑力铭等. 高超声速飞行器材料与结构气动热环境模拟方法及试验研究. 航天器环境工程, 2012,29(3): 250-258
[69] 王乐善, 王庆盛. 结构热试验技术的新发展. 导弹与航天运载技术, 2000 (2): 7-13
[70] Hudson LD.10.2 thermal-structural testing, 20080013159. NASA Dryden Flight Research Center, 2008
[71] 吴大方, 潘兵, 高镇同等. 超高温、大热流、非线性气动热环境试验模拟及测试技术研究. 实验力学, 2012,27(3): 255-271
[72] 王智勇, 黄世勇, 巨亚堂. 石英灯辐射加热试验热流分布优化研究. 强度与环境, 2011, 38(2): 18-23
[73] 秦永烈. 表面温度测量. 北京: 中国计量出版社, 1989
[74] 孟松鹤, 丁小恒, 易法军等. 高超声速飞行器表面测热技术综述. 航空学报, 2014, 35(7): 1759-1775
[75] Adamovsky G, Bramante R, Holguin A, et al.Fiber bragg based optical sensors for extreme temperatures. Aerospace 2011 Conference, St. Louis, Missouri, 2011
[76] Mihailov SJ.Fiber Bragg grating sensors for harsh environments. Sensors, 2012, 12(2):1898-1918
[77] Hunter GW.An overview of the development of high temperature wireless smart sensor technology. NASA Glenn Research Center, 2015
[78] Canning J, Stevenson M, Bandyopadhyay S, et al.Extreme silica optical fibre gratings. Sensors, 2008, 8(10): 6448-6452
[79] 杨庆涛, 白菡尘, 张涛等. 快速响应热流/温度传感器设计与特性分析. 兵工学报, 2014, 35(6): 927-934
[80] 金华,曾庆轩,孟松鹤等. 一种恶劣环境下材料表面温度的非接触式测量方法及装置: CN105222917A.2016-01-06
[81] Zhang X, Yu K, Bai Y, et al.Thermal vibration characteristics of fiber-reinforced mullite sandwich structure with ceramic foams core. Composite Structures, 2015, 131(1): 99-106
[82] 刘浩, 李晓东, 杨文岐等.高速飞行器翼面结构热振动试验的TARMA模型方法. 航空学报, 2015, 36(7): 2225-2235

ADVANCE OF EXPERIMENTAL TECHNOLOGIES FOR STRUCTURAL MODAL TEST IN HIGH TEMPERATURE ENVIRONMENTS

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