Preparation and Thermal Shock Performance of ZrO2/NiCrAlY Thermal Barrier Coating

Lingshuang Wang; Guojian Cao; Guangze Tang; Wanjiao Xu; Xinxin Ma

doi:10.11868/j.issn.1005-5053.2016.000081

Preparation and Thermal Shock Performance of ZrO₂/NiCrAlY Thermal Barrier Coating

Lingshuang Wang
, Guojian Cao^*
, Guangze Tang
, Wanjiao Xu
, Xinxin Ma

^*Corresponding author for this work

School of Materials Science and Engineering

Harbin University of Science and Technology

Research output: Contribution to journal › Article › peer-review

5 Scopus citations

Abstract

Electric spark deposition (ESD) combining with micro-arc oxidation (MAO) were employed to fabricate ZrO₂/NiCrAlY thermal barrier coating (TBC) on GH4169 substrate. Firstly, a NiCrAlY coating with thickness of 250 μm was deposited on GH4169 substrate by ESD. Secondly, a Zr coating with thickness of 150 μm was deposited on NiCrAlY coating followed by MAO of the Zr coating. The thermal shock performances of the coatings under different temperatures were investigated. The results indicate that the thermal cycle numbers of the coatings at 750℃, 850 ℃ and 950℃ are 51, 32, and 19 respectively.

Original language	English
Pages (from-to)	44-48
Number of pages	5
Journal	Journal of Aeronautical Materials
Volume	37
Issue number	2
DOIs	https://doi.org/10.11868/j.issn.1005-5053.2016.000081
State	Published - 1 Apr 2017

Keywords

Coating
Electric spark deposition(ESD)
Micro-arc oxidation
Thermal shock performance

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10.11868/j.issn.1005-5053.2016.000081

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title = "Preparation and Thermal Shock Performance of ZrO2/NiCrAlY Thermal Barrier Coating",

abstract = "Electric spark deposition (ESD) combining with micro-arc oxidation (MAO) were employed to fabricate ZrO2/NiCrAlY thermal barrier coating (TBC) on GH4169 substrate. Firstly, a NiCrAlY coating with thickness of 250 μm was deposited on GH4169 substrate by ESD. Secondly, a Zr coating with thickness of 150 μm was deposited on NiCrAlY coating followed by MAO of the Zr coating. The thermal shock performances of the coatings under different temperatures were investigated. The results indicate that the thermal cycle numbers of the coatings at 750℃, 850 ℃ and 950℃ are 51, 32, and 19 respectively.",

keywords = "Coating, Electric spark deposition(ESD), Micro-arc oxidation, Thermal shock performance",

author = "Lingshuang Wang and Guojian Cao and Guangze Tang and Wanjiao Xu and Xinxin Ma",

year = "2017",

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doi = "10.11868/j.issn.1005-5053.2016.000081",

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pages = "44--48",

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TY - JOUR

T1 - Preparation and Thermal Shock Performance of ZrO2/NiCrAlY Thermal Barrier Coating

AU - Wang, Lingshuang

AU - Cao, Guojian

AU - Tang, Guangze

AU - Xu, Wanjiao

AU - Ma, Xinxin

PY - 2017/4/1

Y1 - 2017/4/1

N2 - Electric spark deposition (ESD) combining with micro-arc oxidation (MAO) were employed to fabricate ZrO2/NiCrAlY thermal barrier coating (TBC) on GH4169 substrate. Firstly, a NiCrAlY coating with thickness of 250 μm was deposited on GH4169 substrate by ESD. Secondly, a Zr coating with thickness of 150 μm was deposited on NiCrAlY coating followed by MAO of the Zr coating. The thermal shock performances of the coatings under different temperatures were investigated. The results indicate that the thermal cycle numbers of the coatings at 750℃, 850 ℃ and 950℃ are 51, 32, and 19 respectively.

AB - Electric spark deposition (ESD) combining with micro-arc oxidation (MAO) were employed to fabricate ZrO2/NiCrAlY thermal barrier coating (TBC) on GH4169 substrate. Firstly, a NiCrAlY coating with thickness of 250 μm was deposited on GH4169 substrate by ESD. Secondly, a Zr coating with thickness of 150 μm was deposited on NiCrAlY coating followed by MAO of the Zr coating. The thermal shock performances of the coatings under different temperatures were investigated. The results indicate that the thermal cycle numbers of the coatings at 750℃, 850 ℃ and 950℃ are 51, 32, and 19 respectively.

KW - Coating

KW - Electric spark deposition(ESD)

KW - Micro-arc oxidation

KW - Thermal shock performance

UR - https://www.scopus.com/pages/publications/85020736797

U2 - 10.11868/j.issn.1005-5053.2016.000081

DO - 10.11868/j.issn.1005-5053.2016.000081

M3 - 文章

AN - SCOPUS:85020736797

SN - 1005-5053

VL - 37

SP - 44

EP - 48

JO - Journal of Aeronautical Materials

JF - Journal of Aeronautical Materials

IS - 2

ER -

Preparation and Thermal Shock Performance of ZrO₂/NiCrAlY Thermal Barrier Coating

Abstract

Keywords

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