Self-Powered Digital Angle Sensor Based on Triboelectric Signal for Variable Structure of Aircraft

被引:0
|
作者
Sheng, Hengrui [1 ,2 ]
Cao, Leo N. Y. [2 ,3 ]
Li, Chengyu [2 ,4 ]
Zhou, Zhuyu [2 ]
Jiang, Yang [2 ,3 ]
Sun, Yanshuo [2 ,4 ]
Chen, Baodong [2 ,3 ]
Xu, Zijie [2 ,3 ,4 ]
Wang, Zhong Lin [2 ,3 ,4 ,5 ]
机构
[1] Guangxi Univ, Ctr Nanoenergy Res, Sch Phys Sci & Technol, Nanning 530004, Peoples R China
[2] Chinese Acad Sci, Beijing Inst Nanoenergy & Nanosyst, Ctr High Entropy Energy & Syst, Beijing Key Lab Micronano Energy & Sensor, Beijing 101400, Peoples R China
[3] Guangzhou Inst Blue Energy, Guangzhou 510555, Peoples R China
[4] Univ Chinese Acad Sci, Sch Nanosci & Technol, Beijing 100049, Peoples R China
[5] Georgia Inst Technol, Sch Mat Sci & Engn, Atlanta, GA 30332 USA
来源
ADVANCED MATERIALS TECHNOLOGIES | 2024年 / 9卷 / 14期
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
digital angle sensor; self-power; triboelectric nanogenerator; variable structure of aircraft;
D O I
10.1002/admt.202301708
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The rapid development of aircraft in recent years has attracted more attention, especially the issue of safe flight for aircraft. Some existing angle detection sensors are difficult to adapt to the development speed of the current aircraft due to the expensive price and large size, so there is an immediate need for new technology that can suit the current aircraft. Here, a self-powered digital angle sensor that is compact, simple, and lightweight is introduced. This sensor eliminates the need for an external power supply and demonstrates highly sensitive signal detection at the volt level when the variable structure of the aircraft is working. The sensor is designed with a thickness of 7.3 mm, a volume of 16.6 cm3, and a weight of 9.85 g. Its lightweight and compact structure allows for seamless integration into aircraft without causing significant impact. The sensor not only provides real-time monitoring the aircraft's variable structure deflection states, including deflection direction and angle but also alerts operators to any anomalies in deflection. Its small size and self-powered capability make it an ideal solution for aircraft applications, enhancing safety and efficiency during flight. The flight safety of aircraft is an important link in the development of aircraft. For angle sensing monitoring of variable components, it can ensure the correct flight attitude of the aircraft. In this work, a self-powered lightweight wireless angle sensor based on a triboelectric nanogenerator is used for monitoring flight safety parameters. image
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页数:8
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