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基于非線性超聲調(diào)制頻譜識(shí)別2024-T351鋁合金板材的疲勞裂紋
發(fā)布人：上海艾荔艾金屬材料有限公司www.jshcn.cn
更新時(shí)間：2015-11-23
基于非線性超聲調(diào)制頻譜法，對(duì)航空鋁合金板材中的疲勞裂紋識(shí)別進(jìn)行研究；以?xún)蓚€(gè)不同頻率的超聲蘭姆波為激勵(lì)信號(hào)，依靠超聲換能器、波形發(fā)生器和激光測(cè)振儀等，對(duì)含有疲勞裂紋和無(wú)損傷的2024-T351鋁合金薄板試樣進(jìn)行對(duì)比實(shí)驗(yàn)；分別采用時(shí)域、頻域和時(shí)頻域聯(lián)合法分析非線性超聲波在鋁合金薄板試樣中傳播的響應(yīng)信號(hào)。
基于非線性超聲調(diào)制頻譜識(shí)別2024-T351鋁合金板材的疲勞裂紋Identification of fatigue cracks in 2024-T351 aluminum alloy plates based on nonlinear ultrasonic modulation spectrum
基于非線性超聲調(diào)制頻譜法，對(duì)航空鋁合金板材中的疲勞裂紋識(shí)別進(jìn)行研究；以?xún)蓚€(gè)不同頻率的超聲蘭姆波為激勵(lì)信號(hào)，依靠超聲換能器、波形發(fā)生器和激光測(cè)振儀等，對(duì)含有疲勞裂紋和無(wú)損傷的2024-T351鋁合金薄板試樣進(jìn)行對(duì)比實(shí)驗(yàn)；分別采用時(shí)域、頻域和時(shí)頻域聯(lián)合法分析非線性超聲波在鋁合金薄板試樣中傳播的響應(yīng)信號(hào)。結(jié)果表明：非線性聲學(xué)特征即調(diào)制頻譜及三階諧波可作為識(shí)別2024-T351鋁合金板材介質(zhì)中疲勞裂紋的判據(jù)，通過(guò)對(duì)試樣表面進(jìn)行掃描，建立調(diào)制頻譜的峰值幅度與位移的關(guān)系，據(jù)此可確定樣板中疲勞裂紋的位置和輪廓，這為航空鋁合金板材疲勞裂紋的識(shí)別提供更多技術(shù)支撐。
The identification of fatigue cracks in the aviation aluminum alloy plates based on nonlinear ultrasonic modulation spectrum method was studied. Taking two different frequencies nonlinear Lamb wave as actuators, comparative experiments on two types of 2024-T351 aluminum alloy plate samples, with and without fatigue crack, were performed by using ultrasonic transducer, waveform generator and non-contact laser vibration meter and so on. The ultrasonic response signals during propagation were analyzed by the time domain, frequency domain and time-frequency domain methods, respectively. The results show that the acoustic characteristic of the modulation frequency components and the third harmonics can be used to indicate the presence of fatigue cracks in 2024-T351 aluminum alloy plates. By scanning the cracked plate, a relationship between the modulation frequency peak magnitude and scanning displacement was established, and according to this relationship the fatigue cracks can be located approximately, the crack contour can be obtained, which will provide more technical support for identification fatigue cracks in aviation aluminum alloy plate.
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