Feasibility Study on PVD Thin Film Sensor for Vibration Fatigue Crack Monitoring

doi:10.7652/xjtuxb201911022

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Feasibility Study on PVD Thin Film Sensor for Vibration Fatigue Crack Monitoring

更新时间：2025-07-09

- Feasibility Study on PVD Thin Film Sensor for Vibration Fatigue Crack Monitoring
- Vol. 53, Issue 11, Pages: 156(2019)
- 作者机构：
  
  空军工程大学航空工程学院,西安,710038
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb201911022
  CLC： V215.6;TP212.1
- Online First：10 November 2019，
  
  Published：2019
- 稿件说明：
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Feasibility Study on PVD Thin Film Sensor for Vibration Fatigue Crack Monitoring[J]. 2019, 53(11): 156.
DOI：

Feasibility Study on PVD Thin Film Sensor for Vibration Fatigue Crack Monitoring[J]. 2019, 53(11): 156. DOI： 10.7652/xjtuxb201911022.

摘要

为确定将离子镀膜技术制备的物理气相沉积(PVD)薄膜传感器用于监测振动疲劳裂纹的可行性

开展了以PVD薄膜传感器和2A12-T4铝合金试验件为对象的研究。通过有限元仿真分析确定了试验件易产生裂纹的位置

并通过离子镀膜技术完成了PVD薄膜传感器的制备。对比了不同表面处理状态试验件的共振频率与振动幅值的变化和疲劳强度

应用显著性分析方法分析了制备PVD薄膜传感器的过程对基体振动响应特性的影响。使用逐步加载法对不同表面处理状态的试验件进行了振动疲劳试验

并对其疲劳强度进行了对比。进行了2A12-T4铝合金试验件的振动疲劳裂纹初步监测试验

对制备有PVD薄膜的试验件的指定点电位差进行了测量。研究结果表明:PVD薄膜传感器的制备过程不会对基体振动响应特性和振动疲劳性能产生不利影响; PVD薄膜传感器与基体具有良好的损伤一致性; PVD薄膜传感器适用于普通基体的振动疲劳裂纹监测。

Abstract

The physical vapor deposition(PVD)thin film sensor prepared by ion plating technology and the 2A12-T4 aluminum alloy test piece are investigated. The feasibility of PVD thin film sensor for vibration fatigue crack monitoring of common substrate is verified. Finite element simulation analysis is carried out to determine the location of cracks in the test piece

and the preparation of the PVD film sensor is completed by ion plating technology. Then

the resonance frequency

vibration amplitude and fatigue strength of the test pieces with different surface treatment states are compared. In the significance analysis

it is verified that the process of preparing the PVD film sensor does not exert an obvious impact on the vibration fatigue performance of the common substrate. The preliminary monitoring test of vibration fatigue crack in 2A12-T4 aluminum alloy test piece demonstrates that the monitoring results of the PVD film sensor coincide well with the actual observation results

and the

关键词

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references

沈海军. 疲劳破坏: 飞机安全的“杀手” [J]. 百科知识, 2007(24): 13-14.

邓增杰, 周敬恩. 工程材料的断裂与疲劳 [M]. 北京: 机械工业出版社, 1995: 1-5.

张勇, 孙强, 卞贵学, 等. 飞机结构的腐蚀防护与腐蚀疲劳研究的发展趋势 [J]. 新技术新工艺, 2014(5): 128-131.

ZHANG Yong, SUN Qiang, BIAN Guixue, et al. Research on development trend of corrosion protection and corrosion fatigue of aircraft structures [J]. New Technology New Process, 2014(5): 128-131.

戴婷. 应力和加载频率对疲劳寿命的影响 [J]. 广州化学, 2017, 42(2): 64-67.

DAI Ting. Effect of loading frequency on fatigue life [J]. Guangzhou Chemistry, 2017, 42(2): 64-67.

陈传尧. 疲劳与断裂 [M]. 武汉: 华中科技大学出版社, 2002: 2-5.

刘文光, 陈国平, 贺红林, 等. 结构振动疲劳研究综述 [J]. 工程设计学报, 2012, 19(1): 1-8, 24.

LIU Wenguang, CHEN Guoping, HE Honglin, et al. Review of studying on vibration fatigue [J]. Journal of Engineering Design, 2012, 19(1): 1-8, 24.

刘文光. 结构共振疲劳试验及裂纹构件的振动疲劳耦合分析 [D]. 南京: 南京航空航天大学, 2010: 1-2.

张金亮. 飞机蓄压油箱的振动疲劳寿命分析 [D]. 沈阳: 沈阳航空航天大学, 2016: 1-2.

樊程广, 潘孟春, 罗飞路, 等. 基于PVDF压电薄膜传感器的超声检测试验 [J]. 无损检测, 2012, 34(1): 27-30.

FAN Chengguang, PAN Mengchun, LUO Feilu, et al. Ultrasonic testing experiment based on the PVDF piezoelectric film sensor [J]. Nondestructive Testing, 2012, 34(1): 27-30.

KUANG K, CANTWELL W J. Use of conventional optical fibers and fiber Bragg gratings for damage detection in advanced composite structures: a review [J]. Applied Mechanics Reviews, 2003, 56(5): 493.

李炳乾. MEMS粗真空传感器研制 [J]. 传感器技术, 2005, 24(1): 87-88.

LI Bingqian. Development of MEMS vacuum sensor [J]. Journal of Transducer Technology, 2005, 24(1): 87-88.

陈祥林, 丁天怀, 黄毅平. 新型接近式柔性电涡流阵列传感器系统 [J]. 机械工程学报, 2006, 42(8): 150-153.

CHEN Xianglin, DING Tianhuai, HUANG Yiping. Novel flexible eddy current array sensor system for proximity sensing [J]. Chinese Journal of Mechanical Engineering, 2006, 42(8): 150-153.

RABIEI M, MODARRES M. Quantitative methods for structural health management using in situ acoustic emission monitoring [J]. International Journal of Fatigue, 2013, 49: 81-89.

WEI R P, BRAZILL R L. An AC potential system for crack length measurement [C]∥The Measurement of Crack Length and Shape during Fracture and Fatigue. Warley, UK: EMAS, 1980: 190-201.

杜金强, 何宇廷, 崔荣洪, 等. 基于电位法原理的金属结构裂纹监测传感器研究 [J]. 南京航空航天大学学报, 2010, 42(3): 387-391.

DU Jinqiang, HE Yuting, CUI Ronghong, et al. Crack monitoring sensor of metallic struc

崔荣洪, 刘凯, 侯波, 等. 耦合服役环境下高耐久性薄膜传感器裂纹监测 [J]. 航空学报, 2018, 39(3): 248-257.

CUI Ronghong, LIU Kai, HOU Bo, et al. Crack monitoring based on high durability film sensor in coupled environment [J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(3): 248-257.

刘凯, 崔荣洪, 侯波, 等. PVD薄膜传感器监测强化结构裂纹的可行性研究 [J]. 西安交通大学学报, 2018, 52(7): 139-145.

LIU Kai, CUI Ronghong, HOU Bo, et al. Feasibility of monitoring strengthened structure crack via PVD film sensor [J]. Journal of Xi'an Jiaotong University, 2018, 52(7): 139-145.

李明祥, 邹玉洁, 孙宝龙, 等. 铝合金阳极氧化技术发展 [J]. 电镀与精饰, 2014, 36(8): 41-46.

LI Mingxiang, ZOU Yujie, SUN Baolong, et al. The development of anodizing technology in aviation aluminum alloy [J]. Plating Finishing, 2014, 36(8): 41-46.

侯波, 何宇廷, 崔荣洪, 等. 基于涂层传感器的金属结构疲劳裂纹监测 [J]. 北京航空航天大学学报, 2013, 39(10): 1298-1302.

HOU Bo, HE Yuting, CUI Ronghong, et al. Fatigue crack monitoring of metallic structure based on coating sensor [J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(10): 1298-1302.

中华人民共和国航空工业部. 发动机叶片及材料振动疲劳试验方法: HB 5277—1984 [EB/OL]. [2019-04-10]. https: ∥wenku.baidu.com/view/8fb672d7b14e8 52458fb5762?ivk_sa=1023194j.

李思路. 航空发动机叶片掉角故障疲劳机理试验方法及强化处理研究 [D]. 西安: 空军工程大学, 2017: 21-33.

刘建华, 杨康, 于美, 等. 酒石酸钠体系中TC18钛合金阳极氧化膜的制备、表征与疲劳性能 [J]. 航空学报, 2014, 35(3): 902-910.

LIU Jianhua, YANG Kang, YU Mei, et al. Preparation, characterization and fatigue performance of anodic oxide film on titanium alloy TC18 in sodium tartrate electrolyte [J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3): 902-910.

NICHOLAS T. High cycle fatigue: a mechanics of materials perspective [M]. Amsterdam, Holland: Elsevier, 2006: 70-134.

XU W, YANG X F, ZHONG B, et al. Multiaxial fatigue investigation of titanium alloy annular discs by a vibration-based fatigue test [J]. International Journal of Fatigue, 2017, 95: 29-37.

崔荣洪. 基于微米传感元的飞机金属结构疲劳损伤监测关键技术研究 [D]. 西安: 空军工程大学, 2010: 61-94.tures based on electric potential method [J]. Journal of Nanjing University of Aeronautics Astronautics, 2010, 42(3): 387-391.

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