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首页> 外文期刊>Mathematical Problems in Engineering >The Reliability Life of 7B04 Aluminum Alloy under Alternate Action of Corrosion and Fatigue
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The Reliability Life of 7B04 Aluminum Alloy under Alternate Action of Corrosion and Fatigue

机译:腐蚀和疲劳交替作用下7B04铝合金的寿命

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摘要

Experiment of alternate action of corrosion and fatigue on 7B04 aluminum alloy was carried out in this paper and fatigue life was obtained. One of the characteristics about fatigue life is that it is not always decreasing with the increasing of corrosion time. The surface splits caused by the corrosion of intruding and extruding slip steps on the surface and decreasing of stress concentration around corrosion pits were the main reasons. Single side allowance factor.. was proposed to calculate reliability fatigue life with both reliability and confidence. Reliability, confidence, and specimen number had affection on the value of k. The reliability influences more greatly the reliability fatigue life compared to the confidence. The safe fatigue life is smaller than median life and it was safe to administrate aircraft life using safe fatigue life.
机译:本文对7B04铝合金进行腐蚀和疲劳交替作用实验,得出疲劳寿命。疲劳寿命的特征之一是,它并不总是随着腐蚀时间的增加而降低。主要原因是由于侵入式和挤出式滑动台阶在表面上的腐蚀以及腐蚀坑周围应力集中的降低而引起的表面裂开。提出了单侧允许系数,以可靠性和置信度来计算可靠性疲劳寿命。可靠性,置信度和样本数量对k值有影响。与置信度相比,可靠性对可靠性疲劳寿命的影响更大。安全疲劳寿命小于中值寿命,使用安全疲劳寿命来管理飞机寿命是安全的。

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  • 来源
    《Mathematical Problems in Engineering 》 |2016年第3期| 3907420.1-3907420.9| 共9页
  • 作者单位

    Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Dept Aircraft Engn, Xian 710038, Peoples R China;

    Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Dept Aircraft Engn, Xian 710038, Peoples R China;

    Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Dept Aircraft Engn, Xian 710038, Peoples R China;

    Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Dept Aircraft Engn, Xian 710038, Peoples R China;

    Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Dept Aircraft Engn, Xian 710038, Peoples R China;

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