Influence of temperature on hot corrosion behavior of GH4169 superalloy subjected to Na2SO4-NaCl salts attack

被引:5
作者
Yang, Baishun [1 ]
Li, Biao [1 ,2 ]
Chen, Xiaoxiao [1 ]
Zhang, Yaning [1 ]
Li, Yazhi [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[2] Natl Key Lab Strength & Struct Integr, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
GH4169; superalloy; Hot corrosion; Temperature; Pit depth and radius; Spallation; Models; Quantitative analysis; CYCLE FATIGUE BEHAVIOR; FAILURE ANALYSIS; DEGREES-C; NICKEL; MODEL; EVOLUTION; MIXTURE; PREDICT;
D O I
10.1016/j.matchemphys.2024.129731
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This work studies the hot corrosion behavior of GH4169 Ni-based superalloy, deposited with a mixture of salts comprising 95 wt% Na2SO4 and 5 wt% NaCl, across three distinct temperatures (i.e., 650 degrees C, 800 degrees C and 950 degrees C). Corrosion and non-corrosive exposure experiments were compared, yielding data on mass loss and gain, respectively. Material characterization results revealed that the corrosion layer was mainly comprised of Cr2O3, Fe2O3, NiO, Al2O3, TiO2, NbS2 and MoS2. Notably, as the temperature ascended from 650 degrees C to over 800 degrees C, the corrosion mechanisms underwent a transition from pitting to uniform corrosion, corresponding to lowtemperature hot corrosion and high-temperature hot corrosion, respectively. At 650 degrees C, a large number of semi-ellipsoidal corrosion pits manifested on the surface. Conversely, at 800 degrees C and 950 degrees C, the corrosion layer on the surface exhibited nearly uniform spallation. The pit growth model and spallation dynamics model were, respectively, developed based on the observed microstructure features. The models serve as tools for quantitative examination of the hot corrosion process of the superalloy at different temperatures.
引用
收藏
页数:19
相关论文
共 49 条
[1]   An analytical and numerical approach to multiscale ductility constraint based model to predict uniaxial/multiaxial creep rupture and cracking rates [J].
Alang, N. A. ;
Nikbin, K. .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2018, 135 :342-352
[2]   Measurement and Discussion of Low-Temperature Hot Corrosion Damage Accumulation upon Nickel-Based Superalloy Rene 104 [J].
Birbilis, N. ;
Buchheit, R. G. .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2008, 39A (13) :3224-3232
[3]   Progress in the Research and Manufacture of GH4169 Alloy [J].
Du, Jin-hui ;
Lu, Xu-dong ;
Deng, Qun ;
Bi, Zhong-ban .
JOURNAL OF IRON AND STEEL RESEARCH INTERNATIONAL, 2015, 22 (08) :657-663
[4]   Hot corrosion in gas turbine components [J].
Eliaz, N ;
Shemesh, G ;
Latanision, RM .
ENGINEERING FAILURE ANALYSIS, 2002, 9 (01) :31-43
[5]   On the Hot Corrosion of Nickel at 700 A°C [J].
Gheno, Thomas ;
Gleeson, Brian .
OXIDATION OF METALS, 2015, 84 (5-6) :567-584
[6]   MECHANISMS FOR HOT CORROSION OF NICKEL-BASE ALLOYS [J].
GOEBEL, JA ;
PETTIT, FS ;
GOWARD, GW .
METALLURGICAL TRANSACTIONS, 1973, 4 (01) :261-278
[7]   Sulfidation Characteristics of an Advanced Superalloy and Comparison with Other Superalloys Intended for Gas Turbine Use [J].
Gurrappa, I. ;
Yashwanth, I. V. S. ;
Burnell-Gray, J. S. .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2013, 44A (11) :5270-5280
[8]   Damage evolution and life modeling of hot corrosion environment on creep-fatigue of a directionally solidified nickel-based superalloy [J].
Hu, Jianhui ;
Zhao, Gaole ;
Li, Shaolin ;
Qi, Hongyu ;
Yang, Xiaoguang ;
Shi, Duoqi .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2023, 46 (04) :1512-1526
[9]   Effects of Hot Corrosion on Fatigue Performance of GH4169 Alloy [J].
Jiang, R. ;
Zhang, L. C. ;
Zhao, Y. ;
Chen, X. H. ;
Gan, B. ;
Hao, X. C. ;
Song, Y. D. .
JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, 2021, 30 (03) :2300-2308
[10]   High temperature cyclic oxidation and hot corrosion behaviours of superalloys at 900A°C [J].
Kamal, Subhash ;
Jayaganthan, R. ;
Prakash, S. .
BULLETIN OF MATERIALS SCIENCE, 2010, 33 (03) :299-306