研究论文

一种镍基高温合金的高温HCl腐蚀行为

  • 周一鸣 ,
  • 韩勇军 ,
  • 谢光 ,
  • 郑伟 ,
  • 肖炎彬 ,
  • 潘阳 ,
  • 张健
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  • 1 中国科学技术大学 材料科学与工程学院 沈阳 110016
    2 中国科学院金属研究所 师昌绪先进材料创新中心 沈阳 110016
    3 中国船舶集团有限公司第七〇五研究所 西安 710077
周一鸣,男,1998年生,博士生
谢 光,gxie@imr.ac.cn,主要从事高温合金研发及同步辐射应用研究;
张 健,jianzhang@imr.ac.cn,主要从事高温合金研发

收稿日期: 2023-02-20

  修回日期: 2023-08-20

  网络出版日期: 2023-12-25

基金资助

国家重点研发计划项目(2021YFA1600603);航空发动机及燃气轮机基础科学中心项目(P2022-C-IV-001-001);国家自然科学基金项目(52271042);国家自然科学基金项目(51911530154);国家自然科学基金项目(91860201);国家自然科学基金项目(U2141206);两机基础研究项目(J2019-VI-0010-0124)

High-Temperature Corrosion Behavior of a Nickel-Based Superalloy in HCl-Containing Atmosphere

  • ZHOU Yiming ,
  • HAN Yongjun ,
  • XIE Guang ,
  • ZHENG Wei ,
  • XIAO Yanbin ,
  • PAN Yang ,
  • ZHANG Jian
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  • 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
XIE Guang, professor, Tel: (024)23748882, E-mail: gxie@imr.ac.cn;
ZHANG Jian, professor, Tel: (024)23911196, E-mail: jianzhang@imr.ac.cn

Received date: 2023-02-20

  Revised date: 2023-08-20

  Online published: 2023-12-25

Supported by

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)

摘要

针对极端环境中材料面临的高温、高浓度HCl的苛刻工况,采用XRD、SEM、EDS和EPMA等研究手段,研究了一种镍基高温合金在960 ℃、5%HCl + 0.5%O2 + Ar (体积分数)气氛条件下的热腐蚀行为,腐蚀时间长达200 h。通过对比不同时间的腐蚀动力学曲线、腐蚀产物种类及分布、截面腐蚀层结构及元素分布,在分析高温合金腐蚀规律的基础上,初步探讨了高温HCl腐蚀机理。结果表明,960 ℃高温下,合金动力学曲线可分为2段:0~75 h及75~200 h,随时间延长,2段曲线均呈先上升后下降的趋势,生成了大量含Mo、Ti、Cr的挥发性氯化物;腐蚀层中,外层富Cr和Ti的氧化物层保护性较差;没有形成连续的Al2O3层;富Ta尖晶石相层具有降低金属离子外扩散的作用;未在试片截面腐蚀层中观察到明显的氯化物富集。研究表明,960 ℃高温下,除了气氛中的HCl、O2以外,通过氯化-氧化过程,而非中温下的活化氧化过程,生成的Cl2同样参与了反应,并起到加速氧化的作用。

本文引用格式

周一鸣 , 韩勇军 , 谢光 , 郑伟 , 肖炎彬 , 潘阳 , 张健 . 一种镍基高温合金的高温HCl腐蚀行为[J]. 金属学报, 2025 , 61(5) : 770 -782 . DOI: 10.11900/0412.1961.2023.00070

Abstract

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.

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