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Exfoliation Corrosion and Pitting Corrosion and Their Role in Fatigue Predictive Modeling: State-of-the-Art Review

机译:剥落腐蚀和点蚀及其在疲劳预测模型中的作用:最新研究

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摘要

Intergranular attack (IG) and exfoliation corrosion (EC) have a detrimental impact on the structural integrity of aircraft structures of all types. Understanding the mechanisms and methods for dealing with these processes and with corrosion in general has been and is critical to the safety of critical components of aircraft. Discussion of cases where IG attack and exfoliation caused issues in structural integrity in aircraft in operational fleets is presented herein along with a much more detailed presentation of the issues involved in dealing with corrosion of aircraft. Issues of corrosion and fatigue related to the structural integrity of aging aircraft are introduced herein. Mechanisms of pitting nucleation are discussed which include adsorption-induced, ion migration-penetration, and chemicomechanical film breakdown theories. In addition, pitting corrosion (PC) fatigue models are presented as well as a critical assessment of their application to aircraft structures and materials. Finally environmental effects on short crack behavior of materials are discussed, and a compilation of definitions related to corrosion and fatigue are presented.
机译:晶间腐蚀(IG)和剥落腐蚀(EC)对所有类型飞机结构的结构完整性都有不利影响。通常,了解用于处理这些过程以及腐蚀的机理和方法对于飞机关键部件的安全一直是至关重要的。本文讨论了IG攻击和剥落导致运营机队的飞机结构完整性出现问题的情况,并详细介绍了涉及飞机腐蚀的问题。本文介绍了与老化飞机的结构完整性有关的腐蚀和疲劳问题。讨论了点蚀成核的机理,包括吸附诱导,离子迁移渗透和化学机械膜击穿理论。此外,还介绍了点蚀(PC)疲劳模型,以及对其在飞机结构和材料中的应用进行了严格的评估。最后讨论了环境对材料短裂纹行为的影响,并提出了与腐蚀和疲劳有关的定义汇编。

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  • 来源
    《International journal of aerospace engineering》 |2012年第2012期|191879.1-191879.29|共29页
  • 作者单位

    Department of Mechanical Engineering, University of Utah, 50 South Central Campus Drive, Room 2010, Salt Lake City, UT 84112, USA;

    Department of Mechanical Engineering, University of Utah, 50 South Central Campus Drive, Room 2010, Salt Lake City, UT 84112, USA;

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