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电弧离子镀Cr-CrN-Cr-CrAlN多层膜热冲击性能研究
作者:
作者单位:

1.海军装备部驻长沙地区军事代表室,湖南 株洲412000;2.广东省科学院新材料研究所/现代材料表面工程技术国家工程实验室/广东省现代表面工程技术重点实验室0;3.中国航发南方工业有限公司,湖南 株洲412000

作者简介:

何志良(1986-),男,湖南益阳人,硕士,工程师,主要研究方向为发动机设计与制造,E-mail:85058687@qq.com。

通讯作者:

林松盛(1973-),男,广东潮州人,博士,教授级高工,主要研究方向为气相沉积,E-mail:linsongsheng@gdinm.com。

中图分类号:

TG174

基金项目:

广东省特支计划团队项目(2019BT02C629);广东省科学院发展专项资金项目(2022GDASZH-2022010103)


Study on Thermal Shock Properties of Cr-CrN-Cr-CrAlN Multilayers Prepared by Arc Ion Plating
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Affiliation:

1.Military Representative Office of Naval Equipment Department in Changsha, Zhuzhou 412000, China;2.Institute of New Materials, Guangdong Academy of Sciences/National Engineering Laboratory of Modern Materials Surface Engineering Technology/Guangdong Provincial Key Laboratory of Modern Surface Engineering Technology, Guang-zhou 510651, China;3.Aecc South Industry Company Limited, Zhuzhou 412000, China

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    摘要:

    为进一步提升航空发动机压气机钛合金部件的服役性能,采用电弧离子镀技术在TC4钛合金表面制备抗砂粒冲蚀Cr-CrN-Cr-CrAlN多层膜。经不同温度热冲击试验后,利用扫描电镜(SEM)、X射线衍射仪(XRD)、显微硬度计、洛氏硬度计及砂粒冲蚀试验仪分析检测了多层膜的表截面形貌、硬度、结合强度和抗砂粒冲蚀性能等。结果表明:随热冲击温度的升高,多层膜的氧化程度逐级增加,当热冲击温度升至900 ℃后,多层膜已明显氧化和出现分层剥落;同样地,多层膜的显微硬度和结合强也随着热冲击温度的升高而降低,硬度由热冲击前的3658 HV降低至经900 ℃冲击后的1930 HV,结合强度则由热冲击前的HF1级降低至经900 ℃热冲击后的HF4级;在700 ℃以内,随着热冲击温度的升高多层膜的冲蚀速率上升缓慢,表明膜层的防护作用显著;而经900 ℃热冲击后,多层膜样品30和90 °攻角下的冲蚀速率由冲击前的0.28、0.65 μm?g-1分别增大至4.05、5.00 μm?g-1,表明膜层已失去防护作用。因此,Cr-CrN-Cr-CrAlN多层膜在700 ℃以内具有冲蚀防护效果,而900 ℃热冲击后已无抗冲蚀防护性能。

    Abstract:

    In order to further improve the service performance of titanium alloy components for aero-engine compressor. The sand erosion resistant Cr-CrN-Cr-CrAlN multilayers were prepared on TC4 titanium alloy by arc ion plating. After thermal shock test at different temperatures, surface cross-sectional morphology, hardness, bonding strength and sand erosion resistance of the multilayer films were analyzed by scanning electron microscopy (SEM), X-ray diffraction (XRD), microhardness tester, Rockwell hardness tester and sand erosion tester. The results showed that the oxidation of the multilayer films increased with the increase of thermal shock temperature. When the temperature increased to 900 ℃, the multilayer films were obviously oxidized and delaminated spalling. Similarly, the microhardness and bonding strength of the multilayer films also decreased with the increase of the thermal shock temperature. The hardness decreased from 3658 HV before thermal shock to 1930 HV after thermal shock at 900 ℃, and the bonding strength decreased from grade HF1 before thermal shock to grade HF4 after thermal shock at 900 ℃. Within 700 ℃, with the increase of thermal shock temperature, the erosion rate of multilayer films increased slowly, and the protective effect of multilayer films was significant. After thermal shock at 900 ℃, the erosion rate of multilayer films under impact at 30°and 90 ° increased from 0.28 and 0.65 μm?g-1 to 4.05 and 5.00 μm?g-1, which has lost its protective effect. Thus, the Cr-CrN-Cr-CrAlN multilayer films exhibit significant protect effect from sand erosion under 700 ℃, which lost its protective effect above 900 ℃.

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引用本文

何志良,林松盛,王迪,石倩,苏一凡,汪云程,吕亮,刘若愚.电弧离子镀Cr-CrN-Cr-CrAlN多层膜热冲击性能研究[J].材料研究与应用,2022,(5):663-668.

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  • 收稿日期:2022-08-31
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  • 在线发布日期: 2022-11-04
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