Study on the effect mechanism of aluminizing on fatigue performance of K403 nickel-based superalloy

被引:6
|
作者
Liu, J. C. [1 ]
Wang, C. [1 ]
Sotware, L. J. Tong [1 ]
Zhang, P. Y. [2 ]
Li, Q. L. [1 ]
Investigation, M. Y. Xie [3 ]
机构
[1] Air Force Engn Univ, Dept Basic Sci, Xian 710038, Peoples R China
[2] Air Force Engn Univ, Aeronaut Engn, Xian 710038, Peoples R China
[3] Peoples Liberat Army, Unit 95655, Chengdu 611530, Peoples R China
关键词
Aluminizing; K403; alloy; Fatigue life; Phase structure; First principles; ELECTRONIC-STRUCTURES; AL; MICROSTRUCTURE; 1ST-PRINCIPLES; STABILITY; BEHAVIOR; NI; OXIDATION; PROPERTY; HARDNESS;
D O I
10.1016/j.jallcom.2020.155277
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Aluminizing is widely used in the surface protection of high-temperature components in the aeroengines, but the effect mechanism of aluminizing on the fatigue properties of matrix alloys is unclear. Based on the analysis of microstructure and element distribution in an aluminized layer of K403 nickel-based superalloy, the effect of the thickness of the aluminized layer on the fatigue life is investigated in this study. By analyzing the phase composition on the surface of the aluminized layer with different thicknesses and combined with first-principles calculations, the effect mechanism of the surface phase structure on the fatigue performance of aluminized alloys is proposed. Results show that the aluminized layer presents an obvious layered structure along the depth direction, and the aluminum content gradually decreases from the outside to the inside. The fatigue life of the aluminized samples is the highest when the surface of the aluminized layer is of the NiAl phase, with the strongest metallic bond characteristics. However, when the surface is of the Ni2Al3 phase with high hardness and brittleness, the fatigue life is the lowest. (C) 2020 Elsevier B.V. All rights reserved.
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页数:8
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