Abstract:The ground 3-D thermal vibration tests can effectively simulate the actual load environment when an aircraft is flying freely, so studying 3-D thermal vibration test technique is particularly critical.Here, a 3-D test system of anti-heat vibration simultaneously satisfying structural stiffness, force transmission and long-term thermal insulation features was designed and constructed.According to the geometric model of the 3-D anti-heat vibration connection system and test conditions, the system’s finite element model was established.The finite element model’s connection boundary was set and adjusted for several times according to test results.Through analyzing test and modal simulation results, the specific connection form of the 3-axis hinged vibration boundary was determined.It was shown that this boundary connection form can simulate a product’s free flight state in sky to the utmost extent.The performance of a contact type high temperature acceleration sensor was studied and verified.3-D control modes within high temperature zone and normal temperature one were studied contrastively.The technical problem to perform multi-dimensional vibration test control in high temperature zones using high temperature acceleration sensors was broken through in China for the first time to realize effective engineering application of 3-D thermal vibration test technique in China.
韩文龙,逯志国,胡彦平,卫国,张群. 三维防热振动连接边界及试验技术研究[J]. 振动与冲击, 2019, 38(15): 115-120.
HAN Wenlong, LU Zhiguo, HU Yanping, WEI Guo, ZHANG Qun. Connection boundary and test technique for 3-D anti-thermal vibration. JOURNAL OF VIBRATION AND SHOCK, 2019, 38(15): 115-120.
[1] 吴大方,赵寿根,潘兵,王岳武,牟朦,吴爽. 高速巡航导弹翼面结构热-振联合试验研究 [J]. 航空学报. 2012 (09)
WUDF, ZHAO S G, PAN B, et al. Research on thermal-Vibration joint test for wing structure of high-speed Cruise miss le[J]. Acta Aeronautica et Astronautica Sinica,2012, 33(9):1633-1642 (in Chinese).
[2]. 吴大方,赵寿根,晏震干.巡航导弹防热部件热-振联合试验[J].航空动力学报,2009,24(7):1507-1511.
Wu Dafang,Zhao Shougen,Yan Zhenqian. Experimental study on thermal-vibration test of thermal insulating component for cruise missile[J].Journal of Aerospace Power,2009, 24(7):1507-1511(in Chinese).
[3]. Jeon B H, Kang H W, Lee Y S. Free vibration characteristics of rectangular plate under rapid thermal loading [C]. The 9th International Congress on thermal stresses. Budapest, 2011.
[4]. 邱吉宝,张正平等.全尺寸航天器振动台多维振动试验的天地一致性研究(上)[J]. 强度与环境, 2015, 42(1): 1-11.
QIU Jibao ZHANG Zhengping. The consistency of dynamic responses of a full scale spacecraft
between ground tests and its space missions(I)[J]. Structure & Environment engineering, 2015, 42(1): 1-11.
[5]. 邱吉宝,张正平等.全尺寸航天器振动台多维振动试验的天地一致性研究(下)[J]. 强度与环境, 2015, 42(2): 1-12.
QIU Jibao ZHANG Zhengping. The consistency of dynamic responses of a full scale spacecraft
between ground tests and its space missions(Ⅱ)[J]. Structure & Environment engineering, 2015, 42(Ⅱ): 1-12.
[6]. Underwood M A, Keller T. Testing civil structures using multiple shaker excitation techniques[J]. Sound and Vibration, 2008, 42(4): 10-15
[7]. 吴家驹. 多维振动环境试验控制策略的分析基础[J]. 强度与环境, 2008, 35(4): 1-6.
WU Jia-ju. Analytical basis for the control strategy of the multi-dimension vibration environment testing [J]. Structure & Environment engineering, 2008, 35(4): 1-6
[8]. Underwood M A, Russell A, Keller T. Filling in the MIMO matrix: using measured data to run a multi-axis vibration test[C]∥The 80th Shock & Vibration Symposium, 2009-10
[9]. 吴家驹, 荣克林. 多维振动环境试验方法[J]. 导弹与航天运载技术, 2003, 264(4): 27-32.
WU J J, RONG K L. Multi-dimentional vibration environmental Test method[J]. Missiles and Space Vehicles, 2003( 4) : 27-32 (in Chinese)
[10]. 张治君,成竹,王琦,等.热振联合环境试验技术研究[J].实验力学,2013, 28 (04): 30-35.
Zhang Zhijun, Cheng Zhu, Wang Qi, et al. Experimental technology Study for thermo-vibration united enviro[J]ment[J]. Journal Of Experimental Mechanics, 2013, 28 (04): 30-35. (in Chinese).
[11]. XU Y H, HU X, YANG Y X, et al. Dynamic simulation of insulation material ablation process in solid propellant Rocket motor[J]. Journal of Aerospace Engineering,2015, 28(5):04014118.
[12]. SPIVEY N D. High-temperature modal survey of a hot structure Control surface: NASA/ TM-2011-215965 [R].Washington, D. C. : NASA, 2011.
[13]. MIL STD 810 G. Department of defense test method standard [S].
[14].贺光宗,陈怀海,贺旭东. 一种多轴向随机激励下结构疲劳寿命分析方法[J]. 振动与冲击,2015,34 ( 7 ) : 59- 63.
HE Guangzong, CHEN Huaihai, HE Xudong.Vibration fatigue life prediction method for structures under multi-axial andom excitations [J].Journal of Vibration and Shock,2015,34( 7) : 59 - 63.
[15].姜双燕,陈怀海,贺旭东,等. 多轴振动试验控制的整型权函数法[J]. 振动与冲击,2011,30(9):136—139.
JIANG Shuang-yan,CHEN Huai-hai,HE Xu-dong,et al.Method of Loop-shaping Weighting Functions for Multi-axis Vibration Test Control[J].Journal of Vibration and Shock,
2011,30(9):136—139.