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An acoustic emission evaluation of environmentally assisted cracking of 7039-T6 aluminum

机译:7039-T6铝的环境辅助裂纹的声发射评估

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Environmentally assisted cracking (EAC) is a significant problem in modern structures. The combination of a susceptible material, an adverse environment and mechanical stress can lead to unexpected failure of a structure by catasticophic crack growth. The mid-air failure of the aluminum alloy bulkhead and the subsequent loss of life on a Aloha Airlines flight on April 28, 1988 as shown in fighure 1, illustrates this fact. Additionally, the operating environment of the US Army contributes to premature failure of structures such as aluminum alloy armor, high strength steel armor and high strength steel control components on Army helicopters [1]. These failures not only endanger life but they also seriously hamper the fighting readiness of U.S.forces because of equipment down time for inspection and repair of faulty components. Work has been performed to better characterie EAC resistance in high strength aluminum armor alloys [2]. These high strength alloys are particularly prone to failure in a chloride environment, an environment encountered in most of the world. If we plan to aviod such failures, we must better understand the EAC phenomena and more diligently detect growing cracks before they become critical in iength. One characterization technique that promises to serve well both as a laboratory tool for understanding EAC and as a field device for detecting EAC is acoustic emission evaluation.
机译:在现代结构中,环境辅助开裂(EAC)是一个重大问题。易受影响的材料,不利的环境和机械应力的组合会导致结构由于意外裂纹的扩展而意外失效。如图1所示,铝合金隔板的半空中故障以及随后在1988年4月28日的Aloha航空公司航班上的人员伤亡证明了这一事实。此外,美国陆军的作战环境还导致陆军直升机上的铝合金装甲,高强度钢装甲和高强度钢制控制部件等结构过早失效[1]。这些故障不仅危及生命,而且由于检查和维修有故障组件的设备停机时间而严重妨碍了美国部队的战斗准备。已经进行了工作,以更好地表征高强度铝铠装合金的EAC耐性[2]。这些高强度合金特别容易在氯化物环境中失效,而氯化物环境是世界上大多数情况下所遇到的环境。如果我们计划避免此类故障,那么我们必须更好地了解EAC现象,并在它们逐渐成为关键之前,更加努力地检测出不断增长的裂缝。一种有望很好地用作了解EAC的实验室工具和检测EAC的现场设备的表征技术是声发射评估。

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