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刘彬, 董世运. 基于临界折射纵波无损评价激光熔覆层应力[J]. 焊接学报, 2014, 35(9): 53-56.
引用本文: 刘彬, 董世运. 基于临界折射纵波无损评价激光熔覆层应力[J]. 焊接学报, 2014, 35(9): 53-56.
LIU Bin, DONG Shiyun. Stress measurement of laser cladding coating with critically refracted longitudinal wave method[J]. TRANSACTIONS OF THE CHINA WELDING INSTITUTION, 2014, 35(9): 53-56.
Citation: LIU Bin, DONG Shiyun. Stress measurement of laser cladding coating with critically refracted longitudinal wave method[J]. TRANSACTIONS OF THE CHINA WELDING INSTITUTION, 2014, 35(9): 53-56.

基于临界折射纵波无损评价激光熔覆层应力

Stress measurement of laser cladding coating with critically refracted longitudinal wave method

  • 摘要: 基于临界折射纵波声弹性理论对激光熔覆层应力的评价方法进行研究.结果表明,激光熔覆层各向异性组织及层间界面是导致其临界折射纵波信号信噪比低、波形畸变程度大的主要因素,弹性极限内随应力的增大,临界折射纵波信号间时间差基本呈线性规律增大,当应力达到658 MPa时,再随应力的增大,时间差呈跳跃趋势变化,激光熔覆层各向异性组织引起的熔覆层不均匀塑性变形是导致上述结果的主要因素,且随应力的增大该影响程度亦逐渐增大.应力验证结果最大相对误差为4.5%,因而认为采用临界折射纵波法可实现激光熔覆层应力的无损评价.

     

    Abstract: Based on ultrasonic acoustoelastic theory, stress measurement of laser cladding coating with critically refracted longitudinal wave was introduced. The results show that anisotropic microstructure in laser cladding coating and its interface were main reasons for lower SNR and waveform distortion of critically refracted longitudinal signal. Within elastic limit, the difference in time of flight between critically refracted longitudinal signals increased linearly as the stress increased. When the stress reached 658 MPa, the relationship between difference in time of flight and stress was not obvious as stress increased further. Uneven plastic deformation of laser cladding coating due to anisotropic microstructure caused the above results, and influence degree of uneven plastic deformation on the results increased with the increase of stress. The maximum relative error in stress measurement was about 4.5%. The method in this study can be used to nondestructively measure the stress in laser cladding coating.

     

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