高超声速飞行器碳基结构高温应变测量

doi:10.7527/S1000-6893.2022.27733

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

高超声速飞行器碳基结构高温应变测量

吴东, 杨鸿(), 赵文峰, 罗跃

中国空气动力研究与发展中心超高速空气动力研究所，绵阳 621000

收稿日期:2022-06-30 修回日期:2022-07-27 接受日期:2022-08-27 出版日期:2022-12-25 发布日期:2022-09-13
通讯作者: 杨鸿 E-mail:yanghong@cardc.cn
基金资助:
国家级项目

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

Dong WU, Hong YANG(), Wenfeng ZHAO, Yue LUO

Hypervelocity Aerodynamics Institute，China Aerodynamics Research and Development Center，Mianyang 　621000，China

Received:2022-06-30 Revised:2022-07-27 Accepted:2022-08-27 Online:2022-12-25 Published:2022-09-13
Contact: Hong YANG E-mail:yanghong@cardc.cn
Supported by:
National Level Project

摘要/Abstract

摘要：

高超声速飞行器结构热应力影响巨大，同时高超声速飞行器高温结构使用碳基材料较多，在碳基材料结构上开展高温应变测量分析就变得非常重要。针对碳基材料上应变计的可靠安装和应变计的热特性差异，开展了碳基材料上高温应变测量研究和碳基端头模型高温应变测量应用试验。碳基材料上高温应变测量研究针对粘贴和喷涂等4种不同安装工艺开展了研究，并针对高温流场环境开展了碳基平板高温应变测量验证试验，应变测量最高温度达900 ℃。应用试验在电弧风洞模拟的高温流场中对碳基端头模型进行了高温应变测量，应变测量温度最高为850 ℃，并开展了有限元计算结果对比，验证了高温应变测量结果。碳基端头模型内腔最大压应力值为220 MPa，应变测量结果显示端头模型的应力状态正常。

关键词: 高超声速, 热应力, 碳基材料, 风洞, 喷流

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

中图分类号:

V411.4

吴东, 杨鸿, 赵文峰, 罗跃. 高超声速飞行器碳基结构高温应变测量[J]. 航空学报, 2022, 43(S2): 160-169.

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.

图/表 16

图 1

图 2

图 3

图 4

图 5

图 6

表 1

表 2

表 3

图 7

图 8

图 9

图 10

图11

图 12

图 13

参考文献 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.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

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]	孙朋朋, 刘平安, 樊枫, 曾伟. 悬停状态共轴刚性旋翼机身气动干扰特性[J]. 航空学报, 2024, 45(9): 529284-529284.
[2]	王畅, 何龙, 徐栋霞, 唐敏, 马率, 吴希明. 共轴刚性旋翼桨毂流动控制减阻研究[J]. 航空学报, 2024, 45(9): 529084-529084.
[3]	张卫国, 唐敏, 武杰, 彭先敏, 章贵川, 聂博文, 王亮权, 李超群. 倾转旋翼机风洞试验综述[J]. 航空学报, 2024, 45(9): 530114-530114.
[4]	聂博文, 王亮权, 黄志银, 何龙, 杨仕鹏, 颜鸿涛, 章贵川. 复合式高速无人直升机飞行动力学建模与控制策略设计[J]. 航空学报, 2024, 45(9): 529848-529848.
[5]	郑建成, 曲智国, 谭贤四, 李志淮, 朱刚, 李陆军, 刘伟. 基于责任区划分的雷达网探测高超声速目标资源管理[J]. 航空学报, 2024, 45(8): 329022-329022.
[6]	戴今钊, 陈海昕. 流场波系引导的三维消波翼优化设计方法[J]. 航空学报, 2024, 45(6): 628942-628942.
[7]	陈其昌, 史志伟, 张维源, 姚灵珑, 童晟翔. 展开式变体垂直起降飞行器气动布局与控制策略设计及飞行验证[J]. 航空学报, 2024, 45(6): 629583-629583.
[8]	刘柳, 向先宏, 张宇飞, 陈海昕, 魏闯, 朱剑, 杨普. 一种高升阻比非常规翼身融合燕尾气动布局[J]. 航空学报, 2024, 45(6): 629630-629630.
[9]	刘小勇, 王明福, 刘建文, 任鑫, 张轩. 超燃冲压发动机研究回顾与展望[J]. 航空学报, 2024, 45(5): 529878-529878.
[10]	杨博, 于贺, 樊子辰. 微观能量分析气动光学效应时变误差的方法[J]. 航空学报, 2024, 45(4): 128703-128703.
[11]	李海星, 周峰, 颜巍, 白峰, 赵克良. 砂纸冰对民机平尾气动特性的影响[J]. 航空学报, 2024, 45(2): 128657-128657.
[12]	李学良, 李创创, 苏伟, 吴杰. 分布式粗糙元对高超声速边界层不稳定性的影响试验[J]. 航空学报, 2024, 45(2): 128627-128627.
[13]	赖江, 范召林, 王乾, 董思卫, 童福林, 袁先旭. 高超声速有攻角锥裙直接数值模拟[J]. 航空学报, 2024, 45(2): 128610-128610.
[14]	熊有德, 李创创, 张振辉, 吴杰. 高超声速风洞自由来流扰动热线测量技术[J]. 航空学报, 2024, 45(10): 129042-129042.
[15]	刘宇, 秦梦婕, 王强, 易贤. 含盐海水飞沫的结冰风洞试验相似准则[J]. 航空学报, 2023, 44(S2): 729297-729297.

高超声速飞行器碳基结构高温应变测量

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

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

图/表 16

参考文献 23

相关文章 15

编辑推荐

Metrics

本文评价