潘峤,张骐,葛玉麟,高蒙,孙志华,杨丽媛,闫巍.TC21钛合金表面涂层体系在多因素综合加速试验条件下的老化规律研究[J].装备环境工程,2020,17(10):26-31. PAN Qiao,ZHANG Qi,GE Yu-lin,GAO Meng,SUN Zhi-hua,YANG Li-yuan,YAN Wei.Evolution Laws of Coated TC21 Titanium Alloy during the Indoor Multi-factor Comprehensive Accelerated Aging Test[J].Equipment Environmental Engineering,2020,17(10):26-31.
TC21钛合金表面涂层体系在多因素综合加速试验条件下的老化规律研究
Evolution Laws of Coated TC21 Titanium Alloy during the Indoor Multi-factor Comprehensive Accelerated Aging Test
投稿时间:2020-03-06  修订日期:2020-04-04
DOI:10.7643/issn.1672-9242.2020.10.005
中文关键词:  钛合金  涂层  多因素  加速试验  岛礁大气环境  电化学阻抗
英文关键词:titanium alloy  coatings  multi-factor  accelerated test  island atmospheric environment  electrochemical impedance
基金项目:“十三五”技术基础科研项目(JSHS2016207A002-2)
作者单位
潘峤 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
张骐 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
葛玉麟 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
高蒙 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
孙志华 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
杨丽媛 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
闫巍 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
AuthorInstitution
PAN Qiao Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
ZHANG Qi Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
GE Yu-lin Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
GAO Meng Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
SUN Zhi-hua Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
YANG Li-yuan Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
YAN Wei Aero Engine Corporation of China Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
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中文摘要:
      目的 研究TC21钛合金表面防护体系(酸洗+环氧底漆+聚氨酯面漆)在多因素协同加速试验条件下的表面性能变化规律。方法 利用一台海洋大气综合模拟试验装置,在户内模拟热带岛礁海洋大气环境,对经历各个加速试验周期后的试样进行外观拍照、光泽度测试、色差测试、光学显微拍照、以及电化学阻抗测试(EIS),并描述相关变化过程。结果 5个周期的加速试验后,试样表面涂层的失光率和色差分别达到45.6%和4.36。涂层在0.01 Hz处的阻抗模值由初始的2.74×1010 Ω下降为6.21×107 Ω。结论 经历5个周期的户内多因素综合加速试验的过程中,TC21钛合金表面涂层体系的防护效果呈持续下降趋势,但5周期后尚未完全失效。
英文摘要:
      The work aims to study the surface property evolution laws of coated TC21 titanium alloy specimens (acid pickling+ epoxy primer +polyurethane top-coat) during the indoor multi-factor comprehensive accelerated aging test. The marine atmosphere environment of tropical island reef was simulated indoors by a marine atmosphere comprehensive simulation test device. The samples after each accelerated test cycle were subject to appearance photo, gloss test, color difference test, optical micrograph and electrochemical impedance test (EIS), and the related change process was described. The glossiness loss rate and the chromatic aberration of the specimens after 5 cycles of accelerated test increased to 45.6% and 4.36, respectively. Additionally, the impedance magnitude of the coating at 0.01 Hz was changed from 2.74×1010 Ω to 6.21×107 Ω.The anti-corrosion ability of the TC21 titanium coating system is continuously decreasing during 5 cycles of indoor multi-factor comprehensive accelerated aging test, but does not completely fail after total 5 cycles of aging test.
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