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Aircraft components structural health monitoring using flexible ultrasonic transducer arrays

机译:使用柔性超声换能器阵列的飞机部件结构健康监测

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摘要

A damage detection capability based on a flexible ultrasonic transducer (FUT) array bonded onto a planar and a curved surface is presented. The FUT array was fabricated on a 75 \u3bcm titanium substrate using sol-gel spray technique. Room temperature curable adhesive is used as the bonding agent and ultrasonic couplant between the transducer and the test article. The bonding agent was successfully tested for aircraft environmental temperatures between -80 \ub0C and 100 \ub0C. For a planar test article, selected FUT arrays were able to detect fasteners damage within a planar distance of 176 mm, when used in the pulse-echo mode. Such results illustrate the effectiveness of the developed FUT transducer as compared to commercial 10MHz ultrasonic transducer (UT). These FUT arrays were further demonstrated on a curved test article. Pulse-echo measurements confirmed the reflected echoes from the specimen. Such measurement was not possible with commercial UTs due to the curved nature of the test article and its accessibility, thus demonstrating the suitability and superiority of the developed flexible ultrasonic transducer capability.
机译:提出了基于柔性超声换能器(FUT)阵列的损伤检测功能,该阵列结合在平坦和弯曲的表面上。使用溶胶-凝胶喷涂技术将FUT阵列制作在75微米的钛基板上。室温可固化粘合剂用作换能器与测试物品之间的粘合剂和超声耦合剂。该粘合剂已成功测试了-80 \ ub0C和100 \ ub0C之间的飞机环境温度。对于平面测试制品,当以脉冲回波模式使用时,选定的FUT阵列能够在176毫米平面距离内检测紧固件损坏。这样的结果说明了与商用10MHz超声换能器(UT)相比,开发的FUT换能器的有效性。这些FUT阵列在弯曲的测试制品上得到了进一步证明。脉冲回波测量确认了样品反射的回波。由于测试物品的弯曲特性及其可及性,使用商用UT不可能进行这种测量,从而证明了开发的柔性超声换能器的适用性和优越性。

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