机构地区:[1]安徽工业大学机械工程学院,安徽马鞍山243032 [2]中国机械科学研究总院集团有限公司,北京100044 [3]北京机科国创轻量化科学研究院有限公司先进成形技术与装备国家重点实验室,北京100083 [4]北京科技大学机械工程学院,北京100083
出 处:《稀有金属材料与工程》2023年第12期4099-4116,共18页Rare Metal Materials and Engineering
基 金:Major Natural Science Research Project of Anhui Provincial Department of Education(KJ2021A036);Top Talent Project of China Mechanical Science Research Institute Group Co.,Ltd。
摘 要:Al-Cu-Li合金是航天航空工业中重要的轻质结构材料,已成为国产大飞机结构件的关键材料之一。飞行器在海洋等潮湿环境服役时,易受到具有腐蚀性的卤化物阴离子的侵蚀,尤其是在Cl离子侵蚀作用下,Al-Cu-Li合金构件表面易出现点蚀、晶间腐蚀和剥落腐蚀现象。Al-Cu-Li合金的局部腐蚀主要归因于合金相与合金基体间存在电势差,进而导致在腐蚀介质中形成微型腐蚀原电池。综述了Al-Cu-Li合金在NaCl溶液中的腐蚀行为以及热处理工艺对合金耐腐蚀性能的影响,重点分析了粗大第二相颗粒和时效析出相对Al-CuLi合金腐蚀性能的影响,研究了典型第3代Al-Cu-Li(2A97-T3、2A97-T6、2060-T8和2099-T83)合金以及航空用常规高强铝合金2024-T4在3种不同浓度NaCl溶液中的侵蚀行为以及在质量分数3.5%NaCl溶液中的电化学行为。综合分析各试样的微观腐蚀形貌、腐蚀电化学参数以及腐蚀程度,最终得出各试样的耐腐蚀性能由强至弱为:2A97-T3>2A97-T6>2024-T4>2060-T8>2099-T83。最后揭示了Al-Cu-Li合金在腐蚀介质中的腐蚀机理,总结了在海洋环境下铝合金的防腐措施。本文为后续Al-Cu-Li合金防腐性能的发展和飞机耐腐蚀性能的提升提供了参考。Al-Cu-Li alloy is a critical lightweight structural material in aviation and aerospace industry,which has become one of the key materials to manufacture the large aircraft structures in China.When the aircraft is in service in humid environments such as the ocean,it is vulnerable to be eroded by corrosive halide anions,and especially under the Cl-ion erosion,its surface of Al-Cu-Li alloy components is prone to pitting corrosion,intergranular corrosion and exfoliation corrosion.The local corrosion of Al-Cu-Li alloy is mainly attributed to the potential difference between the alloy phase and the alloy matrix,which leads to the formation of microcorrosion battery in the corrosive medium.The corrosion behavior of Al-Cu-Li alloy in NaCl solution and the effect of heat treatment on the corrosion resistance of the alloy were reviewed.The effects of coarse second phase particles and aging precipitates on the corrosion properties of Al-Cu-Li alloy were analyzed.In addition,the corrosion behavior in NaCl solution of different contents and electrochemical behavior in 3.5wt%NaCl solution of typical third generation Al-Cu-Li(2A97-T3,2A97-T6,2060-T8 and 2099-T83)alloys and conventional high strength aluminum alloy 2024-T4 used in aviation were studied in NaCl solution.The micro-corrosion morphology,corrosion electrochemical parameters and corrosion degree of each sample were analyzed.Finally,the corrosion resistance of each sample was obtained,from strong to weak in an order of:2A97-T3>2A97-T6>2024-T4>2060-T8>2099-T83.Finally,the corrosion mechanism of Al-Cu-Li alloy in a corrosive medium was revealed,and the anti-corrosion measures of aluminum alloys in marine environments were summarized.This reseach progress provides reference for the subsequent development of the AlCu-Li alloy corrosion protection process and the enhancement in the corrosion resistance of aircraft in humid environments.
关 键 词:AL-CU-LI合金 合金相 局部腐蚀 腐蚀机理 腐蚀防护
分 类 号:TG172[金属学及工艺—金属表面处理]
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