一种无机盐铝涂层涂覆镍基粉末高温合金的高温氧化组织分析
High temperature oxidation microstructure analysis of Ni-based P/M superalloy coated with an inorganic aluminum coating
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文摘
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使用TWL12+TWL20无机盐铝涂层喷涂于镍基粉末高温合金表面,采用XRD、SEM、EPMA和TEM研究无机盐铝涂层与粉末高温合金经700、750、800 ℃高温氧化后的组织变化。结果表明:高温氧化后涂层表层结构出现剥落,涂层中的铝与基体合金发生扩散,形成由氧化区、扩散区、互扩散区组成的过渡层,其中氧化区为最外层,该区域主要富集O、Al元素,形成Al_2O_3层;随之的扩散区主要含有Ni、Al元素,形成NiAl相及在其中弥散分布的 α-Cr相;最后是富集Ti、Cr、Co、Ta等元素的互扩散区,存在于扩散区与基体之间,主要由Ni2AlTi相基体及在其中弥散分布的σ相组成;分析表明过渡层厚度随着氧化温度升高而变化,主要表现为互扩散区宽度增加,扩散区中的 α-Cr相与互扩散区的σ相尺寸增大,且σ相沿垂直过渡区方向生长的趋势加剧;氧化增重曲线表明,涂层表层结构脱落后,过渡层在750、800 ℃高温氧化过程中表现出良好的抗氧化性能,说明TWL12+TWL20无机盐铝涂层具有为航空发动机用先进粉末高温合金提供高温氧化涂层保护的潜力。 |
其他语种文摘
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In this paper, TWL12 + TWL20 inorganic salt aluminum coating was sprayed on the surface of Ni-based P/M superalloy. The microstructure changes of inorganic salt aluminum coating and P/M superalloy after high temperature oxidation at 700, 750 ℃ and 800 ℃ were studied by XRD, SEM, EPMA and TEM. The results show that after high temperature oxidation, the surface structure of the coating peels off, and the aluminum in the coating diffuses with the substrate to form a transition layer composed of oxidation zone, diffusion layer and interdiffusion zone. The oxidation zone is the outermost layer, where is mainly enriched with O and Al elements to form Al_2O_3 layer. The diffusion layer mainly contains Ni and Al elements, forming NiAl phase and α-Cr phase dispersed in it. Finally, the interdiffusion zone rich in Ti, Cr, Co, Ta and other elements exists between the diffusion zone and the matrix, which is mainly composed of Ni2AlTi phase matrix and σ phase dispersed in it. The analysis shows that the thickness of transition layer changes with the increase of oxidation temperature, it is mainly manifested by the increase of the width of the interdiffusion zone, the increase of the size of α-Cr phase in the diffusion layer and σ phase in the interdiffusion zone, and the growth trend of σ phase along the vertical transition zone is intensified. The oxidation weight gain curve shows that the transition layer exhibits good oxidation resistance during high temperature oxidation at 750 ℃ and 800 ℃ after the surface structure of the coating falls off, it indicates that the TWL12 + TWL20 inorganic salt aluminum coating has the potential to provide high temperature oxidation coating protection for advanced P/M superalloy used in aeroengines. |
来源
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航空材料学报
,2023,43(5):67-75 【核心库】
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DOI
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10.11868/j.issn.1005-5053.2023.000003
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关键词
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TWL12+TWL20无机盐铝涂层
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镍基粉末高温合金
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高温氧化
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显微组织
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地址
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1.
中国航发北京航空材料研究院先进高温结构材料重点实验室, 北京, 100095
2.
中国航发北京航空材料研究院, 航空材料先进腐蚀与防护航空科技重点实验室, 北京, 100095
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语种
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中文 |
文献类型
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研究性论文 |
ISSN
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1005-5053 |
学科
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金属学与金属工艺 |
基金
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国防科技重点实验室基金
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文献收藏号
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CSCD:7575085
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参考文献 共
15
共1页
|
1.
张国庆. 航空发动机用粉末高温合金及制备技术研究进展.
金属学报,2019,55(9):1133-1144
|
CSCD被引
37
次
|
|
|
|
2.
Khanna A S. High-temperature oxidation.
Handbook of Environmental Degradation of Materials (Third Edition),2018:117-132
|
CSCD被引
1
次
|
|
|
|
3.
Bache M R. Environment and time dependent effects on the fatigue response of an advanced nickel based superalloy.
International Journal of Fatigue,2009,31(11):1719-1723
|
CSCD被引
5
次
|
|
|
|
4.
Xu C. Mechanism of hightemperature oxidation effects in fatigue crack propagation and fracture mode for FGH97 superalloy.
Rare Metals,2019,38(7):642-652
|
CSCD被引
6
次
|
|
|
|
5.
Misra A K. Aerospace propulsion and power materials and structures research at NASA Glenn Research Center.
Journal of Aerospace Engineering,2013,26(2):459-490
|
CSCD被引
4
次
|
|
|
|
6.
张光业. 航空用高温合金防护涂层的研制及其应用的新进展.
材料导报,2006,20(5):59-62
|
CSCD被引
10
次
|
|
|
|
7.
Texier D. Tensile properties of a non-line-of-sight processed β-γ-γ ' MCrAlY coating at high temperature.
Surface and Coatings Technology,2017,326:28-36
|
CSCD被引
2
次
|
|
|
|
8.
史学海. 无机磷酸盐耐高温涂料的防腐机理及研究进展.
电镀与涂饰,2021,40(14):1110-1118
|
CSCD被引
3
次
|
|
|
|
9.
杨宏波. 金属表面耐高温防腐涂料的研究进展.
表面技术,2017,46(3):216-222
|
CSCD被引
11
次
|
|
|
|
10.
王巍. 某型燃机中温部件防护涂层性能研究.
汽轮机技术,2014,56(6):475-477
|
CSCD被引
1
次
|
|
|
|
11.
费瑞梅. 高强度钢TEL-11涂层工艺的研究.
材料工程,1994(4):29-32
|
CSCD被引
1
次
|
|
|
|
12.
张鹏飞. 无机盐铝涂料及其性能研究.
涂料工业,2013,43(8):69-73
|
CSCD被引
5
次
|
|
|
|
13.
Pedraza F. Oxidation resistance of thermal barrier coatings based on hollow alumina particles.
Oxidation of Metals,2016,85(3):231-244
|
CSCD被引
2
次
|
|
|
|
14.
Goward G W. Current research on the surface protection of superalloys for gas turbine engines.
JOM,1970,22(10):31-39
|
CSCD被引
3
次
|
|
|
|
15.
Montero X. Low-activity aluminide coatings for superalloys using a slurry process free of halide activators and chromates.
Surface and Coatings Technology,2013,222:9-14
|
CSCD被引
5
次
|
|
|
|
|