Radiation-Hardened and Flexible Pb(Zr0.53Ti0.47)O3 Piezoelectric Sensor for Structural Health Monitoring

被引:9
|
作者
Liu, Yajing [1 ]
Yun, Chao [1 ]
Wang, Yu [2 ]
Xu, Longjie [1 ]
Wang, Chongqi [2 ]
Li, Zhongxu [3 ]
Meng, Miao [4 ]
Song, Sijia [1 ]
Li, Kaifeng [1 ]
Li, Dong [1 ]
Chen, Feng [1 ]
Liu, Yang [1 ]
Ji, Yanda [1 ]
You, Tiangui [3 ]
Ning, Shuai [4 ]
Qiu, Lei [2 ]
Yang, Hao [1 ]
Li, Weiwei [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Phys, MIIT Key Lab Aerosp Informat Mat & Phys, State Key Lab Mech & Control Mech Struct, Nanjing 211106, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Res Ctr Struct Hlth Monitoring & Prognosis, State Key Lab Mech & Control Aerosp Struct, Nanjing, Peoples R China
[3] Chinese Acad Sci, Shanghai Inst Microsyst & Informat Technol, Natl Key Lab Mat Integrated Circuits, Shanghai 200050, Peoples R China
[4] Nankai Univ, Ctr Rare Earth & Inorgan Funct Mat, Sch Mat Sci & Engn, Tianjin Key Lab Rare Earth Mat & Applicat, Tianjin 300350, Peoples R China
基金
中国国家自然科学基金;
关键词
piezoelectric sensor; flexible devices; PZT; structural health monitoring; low energy proton radiation; LOW-ENERGY PROTONS; THIN-FILMS; DISPLACEMENT DAMAGE; TEMPERATURE; DEFECTS;
D O I
10.1021/acsami.3c10885
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Piezoelectric sensors are excellent damage detectors that can be applied to structural health monitoring (SHM). SHM for complex structures of aerospace vehicles working in harsh conditions is frequently required, posing challenging requirements for a sensor's flexibility, radiation hardness, and high-temperature tolerance. Here, we fabricate a flexible and lightweight Pb(Zr0.53Ti0.47)O-3 piezoelectric film on flexible KMg3(AlSi3O10)F-2 substrate via van der Waals (vdW) heteroepitaxy, endowing it with robust ferroelectric and piezoelectric properties under low energy-high flux protons (LE-HFPs) radiation (10(15) p/cm(2)). More importantly, the Pb(Zr0.53Ti0.47)O-3 film sensor maintains highly stable damage monitoring sensitivity on an aluminum plate under harsh conditions of LE-HFPs radiation (10(15) p/cm(2), flat structure), high temperature (175 degrees C, flat structure), and mechanical fatigue (bending 10(5) cycles under a radius of 5 mm, curved structure). All these superior qualities are suggested to result from the outstanding film crystal quality due to vdW epitaxy. The flexible and lightweight Pb(Zr0.53Ti0.47)O-3 film sensor demonstrated in this work provides an ideal candidate for real-time SHM of aerospace vehicles with flat and complex curve-like structures working in harsh aerospace environments.
引用
收藏
页码:49362 / 49369
页数:8
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