High-Temperature and Flexible Piezoelectric Sensors for Lamb-Wave-Based Structural Health Monitoring

被引：37
作者：
Zhang, Xiyuan [1 ,2 ,3 ]
Wang, Yu [4 ]
Gao, Xingyao [5 ]
Ji, Yanda [1 ,2 ]
Qian, Fengjiao [1 ,2 ]
Fan, Jiyu [1 ,2 ]
Wang, Haiyan [5 ]
Qiu, Lei [4 ]
Li, Weiwei [1 ,2 ,6 ]
Yang, Hao [1 ,2 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Sci, Nanjing 211106, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, MIIT Key Lab Aerosp Informat Mat & Phys, Nanjing 211106, Peoples R China
[3] High Energy Phys Chinese Acad Sci, Ctr Expt Phys, Beijing 100049, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Res Ctr Struct Hlth Monitoring & Prognosis, Nanjing 210016, Peoples R China
[5] Purdue Univ, Sch Mat Engn, W Lafayette, IN 47907 USA
[6] Univ Cambridge, Dept Mat Sci & Met, Cambridge CB3 0FS, England
来源：
ACS APPLIED MATERIALS & INTERFACES | 2021年 / 13卷 / 40期
基金：
美国国家科学基金会; 中国国家自然科学基金;
关键词：
flexible sensor; piezoelectric sensor; BaTiO3; Lamb wave; structural health monitoring; ACTIVE SENSORS; COMPOSITE; FERROELECTRICITY;
D O I：
10.1021/acsami.1c13704
中图分类号：
TB3 [工程材料学];
学科分类号：
0805 ; 080502 ;
摘要：
Piezoelectric sensors can be utilized in Lamb-wave-based structural health monitoring (SHM), which is an effective method for aircraft structural damage detection. However, due to the inherent stiffness, brittleness, weight, and thickness of piezoelectric ceramics, their applications in aircraft structures with complex curved surfaces are seriously restricted. Herein, we report a flexible, light-weight, and high-performance BaTiO3:Sm2O3/SrRuO3/SrTiO3/mica film sensor that can be used in high-temperature SHM of aircraft. Enhanced ferroelectric Curie temperature (487 degrees C) and piezoelectric coefficient d(33) (120-130 pm/V) are achieved in BaTiO3, which can be attributed to the tensile strain developed by stiff Sm2O3 nanopillars. Stable ferroelectricity and piezoelectricity are retained up to 150 degrees C. The flexible BaTiO3:Sm2O3/ SrRuO3/SrTiO3/mica film is validated as an ultrasonic sensor with high sensitivity and stability for damage monitoring on aircraft structures with the curved surface ranging from 25 to 150 degrees C. Our work demonstrates that flexible and light-weight BaTiO3:Sm2O3/SrRuO3/SrTiO3/mica film sensors can be employed as high-temperature piezoelectric sensors for real-time SHM of aircraft structures with complex curved surfaces.
引用
收藏
页码：47764 / 47772
页数：9
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