Damage Assessment in a Kevlar/Polyester Composite Component

P. Stumpff
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Abstract

The purpose of this investigation was to determine the cause of the ultrasonic signal attenuation noted during an inspection of a composite aircraft component. Although ultrasonics was able to identify the location of the defective areas, destructive analysis had to be utilized to determine the exact nature of the defect. The investigation describes how cross-sectioning, fractography, and chemical analysis were utilized to determine the type of defect responsible for the signal attenuation.
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凯夫拉/聚酯复合材料部件的损伤评估
本调查的目的是确定超声信号衰减的原因注意到在检查复合飞机部件。虽然超声波能够识别缺陷区域的位置,但必须利用破坏性分析来确定缺陷的确切性质。该研究描述了如何利用横截面、断口学和化学分析来确定导致信号衰减的缺陷类型。
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