首页> 外国专利> Method for estimating porosity of e.g. composite material part of aircraft, involves utilizing joint ultrasonic characterization process for estimating value of porosity degree and thickness of material part

Method for estimating porosity of e.g. composite material part of aircraft, involves utilizing joint ultrasonic characterization process for estimating value of porosity degree and thickness of material part

机译:估算孔隙度的方法飞机的复合材料零件,涉及利用联合超声表征工艺估算材料零件的孔隙度和厚度值

摘要

The method involves utilizing a joint ultrasonic characterization process for estimating value of porosity degree and thickness of a material part. Mean velocity of an ultrasonic wave generated by an ultrasonic generator is estimated (210) using the porosity degree and thickness of a material part, and new thickness is estimated (220) from the measured mean velocity. A new porosity degree is determined using the estimated (230) new thickness, and difference between the new thickness and the estimated thickness and the new degree of porosity and the estimated degree is calculated (240).
机译:该方法包括利用联合超声表征过程来估计孔隙率值和材料零件的厚度。使用材料部分的孔隙率和厚度来估计(210)由超声发生器产生的超声波的平均速度,并且根据所测量的平均速度来估计新厚度(220)。使用估计的(230)新厚度来确定新的孔隙度,并且计算新的厚度和估计的厚度以及新的孔隙度和估计的度之间的差(240)。

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