高超声速飞行器碳基结构高温应变测量

doi:10.7527/S1000-6893.2022.27733

Abstract

Abstract:

The hypersonic aircraft structures are affected greatly by thermal stress. The carbon-based composite material is widely used in the high temperature structures of the hypersonic vehicles. Therefore， it is necessary to measure and analyze the high temperature strain field for carbon-based composite material. In view of the reliable installation of strain gage on carbon-based materials and the difference of thermal characteristics of strain gage， high temperature strain measurement research was conducted for carbon-based composite material and end model. The high temperature strain measurement research for carbon-based composite material were conducted considering four kinds of strain gages installation technics including paste and spray. Validation experiments of high temperature strain measurement on carbon-based flat under high temperature flow field were also carried out. The temperature of strain measurement was up to 900 ℃. High temperature strain measurement applicable experiment for carbon-based end model was carried out in the arc heated wind-tunnel up to 850 ℃. The experimental data of carbon-based end model were analyzed and compared by the finite element method， suggesting the reliability of the experimental results. The highest compression stress of carbon-based end model was 220 MPa. The experimental results showed that stress state of carbon end model was normal.

Key words: hypersonic, thermal stress, carbon-based composite material, wind tunnel, spry

CLC Number:

V411.4

Dong WU, Hong YANG, Wenfeng ZHAO, Yue LUO. High temperature strain measurement of hypersonic aircraft carbon-based composite material structures[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 160-169.

Figures/Tables 16

Fig.1

Fig.2

Fig.3

Fig.4

Fig.5

Fig.6

Table 1

Table 2

Table 3

Fig.7

Fig.8

Fig.9

Fig.10

Fig.11

Fig.12

Fig.13

References 23

1	孟松鹤, 杨强, 霍施宇, 等. 一体化热防护技术现状和发展趋势[J]. 宇航学报, 2013, 34(10): 1295-1302.
	MENG S H, YANG Q, HUO S Y, et al. State-of-arts and trend of integrated thermal protection systems[J]. Journal of Astronautics, 2013, 34(10): 1295-1302 (in Chinese).
2	PERAFÁN-LÓPEZ J C, SIERRA-PÉREZ J. An unsupervised pattern recognition methodology based on factor analysis and a genetic-DBSCAN algorithm to infer operational conditions from strain measurements in structural applications[J]. Chinese Journal of Aeronautics, 2021, 34(2): 165-181.
3	LU L L, SONG H W, WANG Y W, et al. Deformation behavior of non-rigid airships in wind tunnel tests[J]. Chinese Journal of Aeronautics, 2019, 32(3): 611-618.
4	邹学锋, 郭定文, 潘凯, 等. 综合载荷环境下高超声速飞行器结构多场联合强度试验技术[J]. 航空学报, 2018, 39(12): 222326.
	ZOU X F, GUO D W, PAN K, et al. Test technique for multi-load combined strength of hypersonic vehicle structure under complex loading environment[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(12): 222326 (in Chinese).
5	吴东, 陈德江, 马昊军. 气动热环境下玻璃窗口热应力试验分析[J]. 空气动力学学报, 2016, 34(5): 592-597.
	WU D, CHEN D J, MA H J. Experimental thermal stress analysis of glass window in aerodynamic thermal environment[J]. Acta Aerodynamica Sinica, 2016, 34(5): 592-597 (in Chinese).
6	陶冶, 田琳, 解梦涛, 等. 大涵道比涡扇发动机风扇叶片动应力测量试飞[J]. 航空发动机, 2017, 43(3): 68-73.
	TAO Y, TIAN L, XIE M T, et al. Flight test on fan-blade vibration stress of high bypass ratio turbofan engine[J]. Aeroengine, 2017, 43(3): 68-73 (in Chinese).
7	李金洋, 毛国培, 李龙, 等. 高温光纤EFPI应变传感技术研究及应用[J]. 载人航天, 2021, 27(5): 633-638.
	LI J Y, MAO G P, LI L, et al. Study on fiber EFPI strain sensor for high temperature and its application[J]. Manned Spaceflight, 2021, 27(5): 633-638 (in Chinese).
8	杨伸勇, 张丛春, 杨卓青, 等. 高温ITO薄膜应变计制备及压阻性能[J]. 材料工程, 2020, 48(4): 145-150.
	YANG S Y, ZHANG C C, YANG Z Q, et al. Fabrication and piezoresistance of high temperature ITO thin film strain gauge[J]. Journal of Materials Engineering, 2020, 48(4): 145-150 (in Chinese).
9	胡挺, 王文瑞, 尹曰雷, 等. 高温应变片参数标定系统的设计与实验研究[J]. 传感技术学报, 2015, 28(9): 1341-1346.
	HU T, WANG W R, YIN Y L, et al. Design and experiment research of high temperature strain calibration system[J]. Chinese Journal of Sensors and Actuators, 2015, 28(9): 1341-1346 (in Chinese).
10	李丽霞, 蒋军亮, 郝庆瑞, 等. 某种高温合金550℃高温应变测试[J]. 应用力学学报, 2015, 32(3): 378-383, 3.
	LI L X, JIANG J L, HAO Q R, et al. Thermal strain test of high temperature alloy at 550 ℃[J]. Chinese Journal of Applied Mechanics, 2015, 32(3): 378-383, 3 (in Chinese).
11	李翔, 傅波. 高超声速飞行器复杂结构热试验技术 [J]. 航空学报, 2016, 37(S1): 73-79.
	LI X, FU B. Thermal test technique of complex structure of hypersonic aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(S1): 73-79 (in Chinese).
12	王成亮, 曹志伟, 武小峰, 等. 高温环境下电阻应变测试技术研究[J]. 强度与环境, 2020, 47(3): 51-56.
	WANG C L, CAO Z W, WU X F, et al. Research on resistance strain measuring technology in high temperature environment[J]. Structure ＆ Environment Engineering, 2020, 47(3): 51-56 (in Chinese).
13	MENG S H, DU C, XIE W H, et al. Application of high-temperature optical fiber sensor in temperature and strain testing of hot structure[J]. Journal of Solid Rocket Technology, 2013, 36(5): 701-705.
14	吴东, 陈德江, 周玮, 等. 高热环境下前缘结构高温应变测量[J]. 实验流体力学, 2016, 30(3): 92-97.
	WU D, CHEN D J, ZHOU W, et al. High temperature strain measurement of the front edge structure in high thermal environment[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(3): 92-97 (in Chinese).
15	许艳芝, 雷晓波, 文敏, 等. 某发动机喷管构件高温载荷测量[J]. 机械强度, 2019, 41(3): 696-701.
	XU Y Z, LEI X B, WEN M, et al. High temperature load measurement for nozzle component of a certain aero-engine[J]. Journal of Mechanical Strength, 2019, 41(3): 696-701 (in Chinese).
16	张再德, 文华. 涡轴发动机燃气涡轮叶片动应力测试技术研究及验证[J]. 燃气涡轮试验与研究, 2019, 32(3): 8-12.
	ZHANG Z D, WEN H. Research and verification of dynamic stress measurement technology for turboshaft engine gas turbine blade[J]. Gas Turbine Experiment and Research, 2019, 32(3): 8-12 (in Chinese).
17	王则力, 乔通, 宫文然, 等. 碳基复合材料结构800 ℃光纤高温应变测量[J]. 强度与环境, 2019, 46(3): 1-6.
	WANG Z L, QIAO T, GONG W R, et al. High temperature strain measurement for composite material structure by fiber optical sensor technique[J]. Structure ＆ Environment Engineering, 2019, 46(3): 1-6 (in Chinese).
18	张佳明, 王文瑞, 王刚. 基于接触式高温应变测试试验的涡轮叶片强度分析[J]. 燃气涡轮试验与研究, 2020, 33(2): 25-29, 6.
	ZHANG J M, WANG W R, WANG G. Strength analysis of turbine blade based on contact high temperature strain test experiment[J]. Gas Turbine Experiment and Research, 2020, 33(2): 25-29, 6 (in Chinese).
19	TORRES B, PAYÁ-ZAFORTEZA I, CALDERÓN P A, et al. Analysis of the strain transfer in a new FBG sensor for structural health monitoring[J]. Engineering Structures, 2011, 33(2): 539-548.
20	ANTHONY P. Application of high-temperature extrinsic fabry-perot interferometer strain sensor[C]∥Aeronautic Sensors Working Group, 2008.
21	GREGORY O J, CHEN X M. A low TCR nanocomposite strain gage for high temperature aerospace applications[C]∥ 2007 IEEE SENSORS. Piscataway: IEEE Press, 2007: 624-627.
22	GLASS D, BELVIN H. Airframe technology development for next generation launch vehicle [C]∥ 12th AIAA International Space Planes and Hypersonic Systems and Technologies. Reston: AIAA, 2003.
23	BHOWMIK K, PENG G D, LUO Y H, et al. High intrinsic sensitivity etched polymer fiber Bragg grating pair for simultaneous strain and temperature measurements[J]. IEEE Sensors Journal, 2016, 16(8): 2453-2459.

加载编号	应变计测试数据/με
加载编号	1号	2号	3号	4号
平均值	-463.7	-463.6	467.9	467.1
第1次	-462.6	-462.6	466.5	467.7
第2次	-464.9	-464.5	468.9	467.5
第3次	-463.6	-463.8	468.2	466.1

加载编号	应变计测试数据重复性/%
加载编号	1号	2号	3号	4号
平均值	0.173	0.149	0.195	0.143
第1次	0.237	0.223	0.292	0.128
第2次	0.259	0.187	0.221	0.086
第3次	0.022	0.036	0.071	0.214

校准温度/℃	高温应变计灵敏系数		偏差/%
校准温度/℃	校准值	北科大校准值	偏差/%
室温	2.182	2.20	0.82
200	2.062	2.036	-1.28
400	1.99	1.955	-1.79
600	1.952	1.894	-3.06
800	1.788	1.738	-2.88

[1]	Shanjie XU, Hongqiang LYU, Zhongchen LIU, Yan LENG, Xuejun LIU. Data analysis of sonic boom test based on probability model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626269-626269.
[2]	Zhongchen LIU, Zhansen QIAN, Xuefei LI, Yan LENG, Dapeng GUO. Wind tunnel test techniques for exhaust nozzle plume effects on near-field sonic boom [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626952-626952.
[3]	Jun SHU, Dongguang XU, Zhirong HAN, Si LI, Xiong HUANG. Hybrid wing design of icing wind tunnel supercooled large droplet icing test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627182-627182.
[4]	Weizhuo HUA, Ling GAO, Ge CHEN, Yiwen LI, Geng GONG, Yantao WANG, Biao WEI. Experimental magneto-hydrodynamic system based on plasma torch [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 1-7.
[5]	Yifeng HUANG, Shuhua ZENG, Zhongzheng JIANG, Weifang CHEN. Numerical study on high-altitude lateral jet based on nonlinear coupled constitutive relation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 8-22.
[6]	Kai LUO, Yonghai WANG, Qiu WANG, Jiwei LI, Zheng LI, Chunsheng NIE, Zheng LI. Plasma-actuated flow control test in high enthalpy shock tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 89-96.
[7]	Xudong ZHANG, Zheng LI, Hao DONG, Siyuan GAO, Zubi JI, Kaixin LI, Guanghui BAI. Drag reduction characteristics of opposing plasma synthetic jet in hypersonic flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 115-123.
[8]	Shouchao HU, Yu ZHUANG, Xian LI, Tao JIANG. Hypersonic aero-heating environment research model HyHERM-I: Experiment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 233-248.
[9]	Haoge LI, Hua YANG, Yuxin YANG, Weifang CHEN. Refinement optimization design for heat reduction on windward surface of hypersonic lifting body [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 124-137.
[10]	Chunsheng NIE, Ye YUAN, Wei MA, Zhanwei CAO, Mingxing YU. Effect of active ejection gas parameters on thermal environment of plate and air rudder [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 170-179.
[11]	Zhengxue MA, Zhenbing LUO, Aihong ZHAO, Yan ZHOU, Wei XIE, Qiang LIU, Yinxin ZHU, Wenqiang PENG. Reverse jet characteristics of plasma synthetic jet in hypersonic flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 192-203.
[12]	Zhikun SUN, Zhiwei SHI, Weilin ZHANG, Zheng LI, Qijie SUN. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 23-39.
[13]	Hai DU, Lejie YANG, Zheng LI, Yue XU, Jingyang SUN, Yuhang WANG. Lifting mechanism and energy efficiency analysis of multistage circulation control technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 54-66.
[14]	LI Jun, WANG Junfeng, ZHAO Yatian, LUO Shibin. Research on combinational configuration of spike and multi-jets in off-design regimes [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 125949-125949.
[15]	LIU Chuanzhen, MENG Xufei, LIU Rongjian, BAI Peng. Experimental and numerical investigation of hypersonic performance of double swept waverider [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 126015-126015.

High temperature strain measurement of hypersonic aircraft carbon-based composite material structures

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 16

References 23

Related Articles 15

Recommended Articles

Metrics

Comments