金属材料腐蚀疲劳研究进展
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摘要
首先归纳了金属材料的腐蚀疲劳裂纹萌生机理和扩展机制,从材料自身因素、外界力学因素和环境因素三方面分析了腐蚀疲劳影响因素,简要介绍了环境腐蚀-疲劳载荷交互试验和环境腐蚀-疲劳载荷协同试验研究现状及重要性,并展望了金属材料腐蚀疲劳今后研究的重要方向,为金属材料腐蚀疲劳的试验开展、机理探索和工程应用奠定基础。
The crack initiation mechanism and extension mechanism of corrosion fatigue were summarized in this paper.The influence factors of corrosion fatigue were analyzed from material itself, external mechanical factors and environmental factors. The research status and importance of environmental corrosion-fatigue load interactive test and environmental corrosion-fatigue load cooperative test were briefly introduced. And the research direction of corrosion fatigue of metal materials was prospected. It lays a foundation for corrosion fatigue test, mechanism exploration and engineering application of metal materials in future.
The crack initiation mechanism and extension mechanism of corrosion fatigue were summarized in this paper.The influence factors of corrosion fatigue were analyzed from material itself, external mechanical factors and environmental factors. The research status and importance of environmental corrosion-fatigue load interactive test and environmental corrosion-fatigue load cooperative test were briefly introduced. And the research direction of corrosion fatigue of metal materials was prospected. It lays a foundation for corrosion fatigue test, mechanism exploration and engineering application of metal materials in future.
引文
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[8]常红,韩恩厚,王俭秋,等.飞机蒙皮涂层对LY12CZ铝合金腐蚀疲劳寿命的影响[J].中国腐蚀与防护学报,2006,26(1):34-42.
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[12]FU Y,XIONG J,SHENOI R A.New Models for Depicting Corrosion Fatigue Behavior and Calendar Life of Metallic Structural Component[J].Archive Proceedings of the Institution of Mechanical Engineers Part C:Journal of Mechanical Engineering Science,2016,231(2):207-222.
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[18]陈亚军,张长田,张汛涛,等.固溶+时效对GH4169合金交替腐蚀疲劳性能的影响[J].热加工工艺,2018,47(8):158-162.
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[20]JONES K,HOEPPNER D W.The Interaction between Pitting Corrosion,Grain Boundaries,and Constituent Particles during Corrosion Fatigue of 7050-T6 Aluminum Alloy[J].International Journal of Fatigue,2009,31(4):686-692.
[21]王浦全,崔广椿.加载频率对腐蚀疲劳裂纹扩展速率影响的研究[J].机械强度,1992,11(1):74-76.
[22]DANIEL K.Enhanced Model of Partial Crack Closure for Correlation of R-ratio Effects in Aluminum Alloys[J].International Journal of Fatigue,2001,23:95-102.
[23]韩恩厚,韩玉梅,郑宇礼,等.应力比和频率对低合金钢腐蚀疲劳裂纹扩展机理的影响[J].金属学报,1993,29(5):223-228.
[24]AGAR S,GRUM J.Evaluation of the Residual Stresses and Corrosion Resistance of Shot-peened 7075 Aluminum Alloy under Different States[J].International Journal of Materials&Product Technology,2016,53(3/4):335.
[25]李鹏,吴仁涛,徐晓龙,等.腐蚀介质对7N01铝合金焊接接头腐蚀疲劳性能的影响[J].中国铁路,2014(10):38-41.
[26]臧启山,刘慷,马敏雅,等.频率、pH值和温度对A537海洋用钢腐蚀疲劳性能的影响[J].腐蚀科学与防护技术,1989,1(2):10-14.
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[28]SU X Y,CAO D G.Corrosion Fatigue Crack Growth of Aluminum Alloy LY12-CZ and LC4-CS in Various Environments[J].Material Engineering,1991,12(1):48-51.
[29]HUI L,ZHOU S,XU L,et al,Influence of Corrosion Environment on Corrosion Fatigue Property of Pre-corroded Aluminum Alloy[J].Material Engineering,2015,43(2):73-78.
[30]CHEN Y L,BIAN G X,YI L,et al,Research on Fatigue Characteristic and Fracture Mechanics of Aluminum Alloy under Alternate action of Corrosion and Fatigue[J].Journal of Mechanical Engineering,2012,48(20):70-76.
[31]张有宏,吕国志,李仲,等.铝合金结构腐蚀疲劳裂纹扩展与剩余强度研究[J].航空学报,2007,28(2):332-335.
[32]王晴晴,上官晓峰.海洋大气腐蚀对7475铝合金疲劳性能的影响[J].科学技术与工程,2013,13(4):859-866.
[33]上官晓峰,姜松,王晴晴.海洋大气中30Cr Mn Si Ni2A钢接触腐蚀疲劳性能研究[J].西安工业大学学报,2014,34(2):152-159.
[34]沈海军,郭万林,吕国志.飞机谱载下铝合金锪窝孔结构腐蚀疲劳研究[J].力学学报,2003,35(1):21-25.
[35]张伦武,郑林,朱蕾,等.7A52铝合金及20Cr Mn Si A钢焊接件海洋大气应力腐蚀试验研究[J].装备环境工程,2017,14(6):109-115.
[36]罗来正,王晓辉,未来,等.一种高寒气候环境-拉、压、弯载荷耦合试验装置:中国,CN 106370532A[P].
[2]罗来正,肖勇,王晓辉,等.海洋气候环境-拉、压、弯载荷耦合试验设备及试验方法:中国,CN109115593A[P].
[3]罗来正,肖勇,王晓辉,等.一种海洋气候环境-扭转载荷耦合试验装置及试验方法:中国,CN 109163986A[P].
[4]文邦伟,胥泽奇.外军装备环境适应性典型案例[J].装备环境工程,2006,2(3):83-87.
[5]刘思宏.舰载机典型机构腐蚀疲劳可靠性分析[D].西安:西北工业大学,2013.
[6]WEI R P,LI C,HARLOW D G,et al,Probability Modeling of Corrosion Fatigue Crack Growth and Pitting Corrosion[J].Fatigue in New and Aging Aircraft,1998(1):197-214.
[7]WANG Q Y,PIDAPARTI R M,PALAKAL M J.Comparative Study of Corrosion-fatigue in Aircraft Materials[J].American Institute of Aeronautics and Astronautics,2001,39(2):325-330.
[8]常红,韩恩厚,王俭秋,等.飞机蒙皮涂层对LY12CZ铝合金腐蚀疲劳寿命的影响[J].中国腐蚀与防护学报,2006,26(1):34-42.
[9]张正贵,周兆元,刘长勇.高强度铝合金构件腐蚀疲劳失效分析[J].中国腐蚀与防护学报,2008,28(1):48-52.
[10]PIDAPARTI R M,JAYANTI S,SOWERS C A,et al,Classification,Distribution,and Fatigue Life of Pitting Corrosion for Aircraft Materials[J].Journal of Aircraft,2002,39(3):486-492.
[11]ZAMBER J E,HILLBERRY B M.Probabilistic Approach to Predict Fatigue Lives of Corroded 2024-T3[J].American Institute of Aeronautics and Astronautics,1999,37(10):1131-1137.
[12]FU Y,XIONG J,SHENOI R A.New Models for Depicting Corrosion Fatigue Behavior and Calendar Life of Metallic Structural Component[J].Archive Proceedings of the Institution of Mechanical Engineers Part C:Journal of Mechanical Engineering Science,2016,231(2):207-222.
[13]WANG L,HUI L,ZHOU S,et al,Effect of Corrosive Environment on Fatigue Property and Crack Propagation Behavior of Al 2024 Friction Stir Weld[J].Transactions of Nonferrous Metals Society of China,2016,26(11):2830-2837.
[14]路民旭,郑修麟,秦熊浦.腐蚀疲劳力学-化学模型研究进展[J].中国腐蚀与防护学报,1991,11(3):197-208.
[15]WEI R P,SIMMONS G W.Recent Progress in Understanding Environment Assisted Fatigue Crack Growth[J].International Journal of Fracture,1981,17:235-247.
[16]AUSTEN I M,MCLNTYRE P.Corrosion Fatigue of High Strength Steel in Low Pressure Hydrogen Gas[J].Metal Science,1979,13(7):420-428.
[17]WEI R P,SOEIDEL M O.Phenomenological Aspects of Corrosion Fatigue,Critical Introduction;Corrosion Fatigue:Chemistry[J].Mechanics and Microstructure,1972,9(2):379-380.
[18]陈亚军,张长田,张汛涛,等.固溶+时效对GH4169合金交替腐蚀疲劳性能的影响[J].热加工工艺,2018,47(8):158-162.
[19]王正.临界区热处理对腐蚀疲劳抗力的影响[J].郑州工学院学报,1984(2):21-25.
[20]JONES K,HOEPPNER D W.The Interaction between Pitting Corrosion,Grain Boundaries,and Constituent Particles during Corrosion Fatigue of 7050-T6 Aluminum Alloy[J].International Journal of Fatigue,2009,31(4):686-692.
[21]王浦全,崔广椿.加载频率对腐蚀疲劳裂纹扩展速率影响的研究[J].机械强度,1992,11(1):74-76.
[22]DANIEL K.Enhanced Model of Partial Crack Closure for Correlation of R-ratio Effects in Aluminum Alloys[J].International Journal of Fatigue,2001,23:95-102.
[23]韩恩厚,韩玉梅,郑宇礼,等.应力比和频率对低合金钢腐蚀疲劳裂纹扩展机理的影响[J].金属学报,1993,29(5):223-228.
[24]AGAR S,GRUM J.Evaluation of the Residual Stresses and Corrosion Resistance of Shot-peened 7075 Aluminum Alloy under Different States[J].International Journal of Materials&Product Technology,2016,53(3/4):335.
[25]李鹏,吴仁涛,徐晓龙,等.腐蚀介质对7N01铝合金焊接接头腐蚀疲劳性能的影响[J].中国铁路,2014(10):38-41.
[26]臧启山,刘慷,马敏雅,等.频率、pH值和温度对A537海洋用钢腐蚀疲劳性能的影响[J].腐蚀科学与防护技术,1989,1(2):10-14.
[27]AGAR S,GRUM J.Evaluation of the Residual Stresses and Corrosion Resistance of Shot-peened 7050 Aluminum Alloy under Different States[J].International Journal of Material technology,2016,53(3/4):335.
[28]SU X Y,CAO D G.Corrosion Fatigue Crack Growth of Aluminum Alloy LY12-CZ and LC4-CS in Various Environments[J].Material Engineering,1991,12(1):48-51.
[29]HUI L,ZHOU S,XU L,et al,Influence of Corrosion Environment on Corrosion Fatigue Property of Pre-corroded Aluminum Alloy[J].Material Engineering,2015,43(2):73-78.
[30]CHEN Y L,BIAN G X,YI L,et al,Research on Fatigue Characteristic and Fracture Mechanics of Aluminum Alloy under Alternate action of Corrosion and Fatigue[J].Journal of Mechanical Engineering,2012,48(20):70-76.
[31]张有宏,吕国志,李仲,等.铝合金结构腐蚀疲劳裂纹扩展与剩余强度研究[J].航空学报,2007,28(2):332-335.
[32]王晴晴,上官晓峰.海洋大气腐蚀对7475铝合金疲劳性能的影响[J].科学技术与工程,2013,13(4):859-866.
[33]上官晓峰,姜松,王晴晴.海洋大气中30Cr Mn Si Ni2A钢接触腐蚀疲劳性能研究[J].西安工业大学学报,2014,34(2):152-159.
[34]沈海军,郭万林,吕国志.飞机谱载下铝合金锪窝孔结构腐蚀疲劳研究[J].力学学报,2003,35(1):21-25.
[35]张伦武,郑林,朱蕾,等.7A52铝合金及20Cr Mn Si A钢焊接件海洋大气应力腐蚀试验研究[J].装备环境工程,2017,14(6):109-115.
[36]罗来正,王晓辉,未来,等.一种高寒气候环境-拉、压、弯载荷耦合试验装置:中国,CN 106370532A[P].