High-Temperature Corrosion Behavior of a Nickel-Based Superalloy in HCl-Containing Atmosphere
ZHOU Yiming1,2, HAN Yongjun3, XIE Guang2(), ZHENG Wei2, XIAO Yanbin3, PAN Yang3, ZHANG Jian2()
1 School of Materials Science and Engineering, University of Science and Technology of China, Shenyang 110016, China 2 Shi -changxu Innovation Center for Advanced Materials, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 3 The 705 Research Institute of China State Shipbuilding Corporation Limited, Xi'an 710077, China
Cite this article:
ZHOU Yiming, HAN Yongjun, XIE Guang, ZHENG Wei, XIAO Yanbin, PAN Yang, ZHANG Jian. High-Temperature Corrosion Behavior of a Nickel-Based Superalloy in HCl-Containing Atmosphere. Acta Metall Sin, 2025, 61(5): 770-782.
Superalloys are widely used in aviation, aerospace, energy, transportation, and petrochemical industries due to their excellent properties, such as high-temperature strength, plasticity, fracture toughness, oxidation resistance, and hot corrosion resistance. They are primarily employed in aircraft engines and gas turbines within aviation, marine, and power generation sectors. Furthermore, due to the unique properties of superalloys and continuous advancements of superalloy technology, their applications are expanding into increasingly extreme service environments. In order to simulate the harsh working conditions of materials under high temperature and high concentration HCl environment, the hot corrosion behavior of a nickel-based superalloy was investigated at 960 oC in a mixed atmosphere of 5%HCl + 0.5%O2 + Ar (volume fraction) using XRD, SEM, EDS, and EPMA techniques. Hot corrosion tests were conducted for 200 h. Analysis of corrosion kinetics, types and distribution of corrosion products, and cross-sectional elemental mapping revealed two distinct stages (0-75 h and 75-200 h), both showing an initial increase followed by a decrease in corrosion rate. Volatile chlorides containing Mo, Ti, and Cr formed extensively. The corrosion layer exhibited a poorly protective (Cr, Ti)-rich oxide layer, while no continuous Al2O3 layer was observed. The Ta-rich spinel layer inhibited outward diffusion of metal ions. The corrosion layer of the experimental alloy did not exhibit any significant chloride concentration on its cross-section. In addition to HCl and O2 in the atmosphere, Cl2 generated through chlorination and oxidation processes reacted with the alloy and played an important role in accelerating oxidation at 960 oC, without evidence of intermediate-temperature activated oxidation.
Fund: National Key Research and Development Program of China(2021YFA1600603);Science Center for Gas Turbine Project(P2022-C-IV-001-001);National Natural Science Foundation of China(52271042);National Natural Science Foundation of China(51911530154);National Natural Science Foundation of China(91860201);National Natural Science Foundation of China(U2141206);National Science and Technology Major Project(J2019-VI-0010-0124)
Corresponding Authors:
XIE Guang, professor, Tel: (024)23748882, E-mail: gxie@imr.ac.cn; ZHANG Jian, professor, Tel: (024)23911196, E-mail: jianzhang@imr.ac.cn
Fig.1 Schematic of hot corrosion test specimen (unit: mm)
Fig.2 Schematic of high-temperature HCl-containing corrosion test equipment
Fig.3 SEM images of the nickel-based superalloy after heat treatment (a) grain (b) carbides and eutectic (c) γ and γ' phases
Fig.4 Mass change vs time for nickel-based superalloy after corrosion in 5%HCl-containing atmosphere for 0-200 h at 960 oC and piecewise fitting results (t—corrosion time)
Fig.5 Surface macrostructures for nickel-based superalloy after corroded in 5%HCl-containing atmosphere for 25 h (a), 50 h (b), 75 h (c), 100 h (d), and 200 h (e) at 960 oC
Fig.6 Changes of spalling area on the surface of nickel-based superalloy with corrosion time
Fig.7 XRD spectra of the corrosion products on the surface of nickel-based superalloy (a) and macro morphology (b) and XRD spectra (c) of volatile corrosion products on the equipment condensing end after corrosion in 5%HCl-containing atmosphere for different time at 960 oC
Table 1 Phases identified by XRD of the corrosion products for nickel-based superalloy after corrosion in 5%HCl-containing atmosphere at 960 oC for different time
Fig.8 SEM backscattered electron (BSE) images of the surface of nickel-based superalloy after corroded in 5%HCl-containing atmosphere for 25 h (a), 50 h (b), 75 h (c), 100 h (d), and 200 h (e) at 960 oC
Fig.9 Cross sectional SEM-BSE images of nickel-based superalloy after corrosion in 5%HCl-containing atmosphere for 25 h (a), 50 h (b), 75 h (c), 100 h (d), and 200 h (e) at 960 oC (TCP—topologically close-packed)
Fig.10 Change of the thickness of corrosion products with corrosion time
Fig.11 Cross sectional SEM-BSE images showing the internal oxidation morphologies along grain boundaries for nickel-based superalloy after corroded for 75 h (a), 100 h (b), and 200 h (c)
Fig.12 Cross sectional SEM-BSE images and corresponding EPMA element maps of the nickel-based superalloy afte corroded in 5%HCl-containing atmosphere for 25 h (a), 50 h (b), 75 h (c), and 100 h (d) at 960 oC
Fig.13 Gibbs free energy differences (ΔG) for different elements M at different temperatures (2n is the valence state of metal ion) (a) M + HCl = MCl2n + H2 (b) M + nCl2 = MCl2n
Fig.14 ΔG for oxidation and chlorination of Al, Ti, and Cr at 960 oC
Type of chloride
Tm
Tb
AlCl3
466
454
CoCl2
1013
1326
CrCl2
1088
1573
CrCl3
1423
1218
MoCl3
1000
1700
MoCl4
590
680
MoCl5
467
541
NiCl2
1303
1243
TaCl2
1210
1650
TaCl3
1300
1620
TaCl4
570
1050
TaCl5
490
507
TiCl2
1308
-
TiCl3
-
1104
TiCl4
-
409
WCl6
555
561
Table 2 Melting points (Tm) and boiling points (Tb) of chlorides corresponding to the nickel-based superalloy[23]
Fig.15 ΔG for oxidation of different chlorides at 960 oC
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