基于ARM和LabVIEW的高頻電磁渦流檢測(cè)系統(tǒng)集成設(shè)計(jì)
[Abstract]:With the increasing demand of carbon fiber composites in the field of aerospace, it is urgent to detect the damage of carbon fiber composites in time to avoid the major safety risks caused by structural damage. There are many damage detection methods for carbon fiber composites, and eddy current testing is widely used as a common nondestructive testing method because of its simple structure, non-contact, no need of coupling agent and so on. Because the carbon fiber composite is composed of conductive carbon fiber and insulating matrix material, it is possible to detect the eddy current of carbon fiber composite. In this paper, Eddy current testing method is used to detect the damage of carbon fiber composites. In order to meet the different demands of excitation signal frequency in different situations, a high frequency electromagnetic eddy current detection system is designed and developed. The frequency can be adjusted arbitrarily, and the system is of high integration and small volume. Easy to use. The main contents of this paper are as follows: first, the hardware circuit of the high frequency electromagnetic eddy current detection system is designed according to the overall scheme, including power supply module, excitation signal processing module, automatic balance module, phase-locked amplifier module. STM32 core module, sinusoidal signal generation module, data acquisition module, automatic balance control module and USB communication module. Secondly, the software design of the high frequency electromagnetic eddy current detection system is carried out, which mainly includes the upper computer software and the lower computer software. The main function of the upper computer is to control the work of the lower computer and the process of detection. The main function of the lower computer is to receive the commands of the upper computer to perform different operations. Thirdly, the high frequency electromagnetic eddy current testing system is used to test the common damage of carbon fiber composites, including crack, impact and delamination. The feasibility and practicability of the system are proved.
【學(xué)位授予單位】:南京航空航天大學(xué)
【學(xué)位級(jí)別】:碩士
【學(xué)位授予年份】:2016
【分類號(hào)】:TB302.5;TP274
【參考文獻(xiàn)】
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