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柔性涡流阵列(FECA)传感器在恶劣服役环境中的耐久性。

The durability of flexible eddy current array (FECA) sensors in harsh service environments.

作者信息

Song Yujian, Chen Tao, Cui Ronghong, He Yuting, Fan Xianghong, Ma Binlin

机构信息

Aeronautic Engineering College, Air Force Engineering University, 1 Baling Road, Xi'an, 710038, China.

出版信息

Sci Rep. 2021 May 14;11(1):10341. doi: 10.1038/s41598-021-89750-y.

Abstract

Sensors for structural health monitoring (SHM) need to be permanently integrated on structures and withstand the harsh service environments, which has been a big challenge for the application of SHM in aircrafts. This paper focuses on the durability of flexible eddy current array (FECA) sensors in harsh service environments of aircrafts, including vibration environment and several typical exposed environments. First, a kind of FECA sensor is illustrated and its integration method is proposed. Moreover, in order to study the durability of the sensor in vibration environment, the modal analysis is performed by the finite element method. According to the simulation results, the durability experiment in vibration environment is carried out under the fourth order vibration mode, which makes the sensor suffer the harshest vibration loads. During the vibration experiment, output signals of the sensor keep stable and the sensor is well bonded to the structure, which shows the integrated sensor has high durability in vibration environment. Finally, the durability of integrated sensors is separately tested in three exposed environments, including salt fog corrosion environment, fluid immersion environment, as well as hygrothermal and ultraviolet-radiation environment. After these environmental exposure experiments, all sensors are well bonded to structures and can effectively monitor fatigue cracks, which shows great durability. Therefore, FECA sensors can survive in harsh service environments of aircrafts, which provides important support for the engineering applications of FECA sensors.

摘要

用于结构健康监测(SHM)的传感器需要永久集成在结构上,并承受恶劣的服役环境,这一直是SHM在飞机应用中的一大挑战。本文重点研究了柔性涡流阵列(FECA)传感器在飞机恶劣服役环境中的耐久性,包括振动环境和几种典型的暴露环境。首先,阐述了一种FECA传感器并提出了其集成方法。此外,为了研究传感器在振动环境中的耐久性,采用有限元方法进行模态分析。根据仿真结果,在四阶振动模式下进行振动环境中的耐久性试验,使传感器承受最恶劣的振动载荷。在振动试验过程中,传感器的输出信号保持稳定,且传感器与结构良好粘结,这表明集成后的传感器在振动环境中具有较高的耐久性。最后,在三种暴露环境下分别测试集成传感器的耐久性,包括盐雾腐蚀环境、流体浸泡环境以及湿热和紫外线辐射环境。经过这些环境暴露试验后,所有传感器均与结构良好粘结,且能有效监测疲劳裂纹,显示出良好的耐久性。因此,FECA传感器能够在飞机的恶劣服役环境中存活,这为FECA传感器的工程应用提供了重要支持。

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