Surface Integrity and Oxidation of a Powder Metallurgy Ni-Based Superalloy Treated by Laser Shock Peening
Abstract
Laser shock peening is a mechanical surface treatment which can induce large compressive residual stresses and microstructural changes in the material by using repetitive shocks from laser pulses. In this work, the surface integrity (surface microstructure, topography, hardness and residual stress) of a laser shock peening treated powder metallurgy Ni-based superalloy was investigated. Laser shock peening treatment introduces large plastic deformation especially at a depth of about 100 μm from the surface, which increases the local hardness. The residual stress from the surface to the interior of the sample was investigated by synchrotron X-ray diffraction. The maximum compressive stress reaches 400 MPa at the surface, while the depth of the compressive stress is about 0.7 mm. Lastly, the oxidation behavior of the treated and untreated samples was evaluated by thermal exposure at 700°C for 312 h. The LSP treatment decreased the thickness of oxide layer, thereby showing improved oxidation resistance.
- Authors:
-
- Univ. of Science and Technology, Beijing (China)
- Beijing Inst. of Aeornautical Materials (China)
- Air Force Engineering Univ., Xi'an (China)
- Argonne National Lab. (ANL), Argonne, IL (United States)
- Publication Date:
- Research Org.:
- Argonne National Laboratory (ANL), Argonne, IL (United States)
- Sponsoring Org.:
- National Key Research and Development Program of China; National Natural Science Foundation of China (NSFC); Fundamental Research Funds for the Central Universities; USDOE Office of Science (SC), Basic Energy Sciences (BES). Scientific User Facilities Division
- OSTI Identifier:
- 1668069
- Grant/Contract Number:
- AC02-06CH11357
- Resource Type:
- Accepted Manuscript
- Journal Name:
- JOM. Journal of the Minerals, Metals & Materials Society
- Additional Journal Information:
- Journal Volume: 72; Journal Issue: 5; Journal ID: ISSN 1047-4838
- Publisher:
- Springer
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 36 MATERIALS SCIENCE
Citation Formats
Tan, Qing, Yan, Zhiran, Huang, Hua, Li, Shilei, Wang, Yandong, Feng, Yefei, Zhou, Xin, Li, Yinghong, Ren, Yang, and Antonov, Stoichko. Surface Integrity and Oxidation of a Powder Metallurgy Ni-Based Superalloy Treated by Laser Shock Peening. United States: N. p., 2020.
Web. doi:10.1007/s11837-020-04054-2.
Tan, Qing, Yan, Zhiran, Huang, Hua, Li, Shilei, Wang, Yandong, Feng, Yefei, Zhou, Xin, Li, Yinghong, Ren, Yang, & Antonov, Stoichko. Surface Integrity and Oxidation of a Powder Metallurgy Ni-Based Superalloy Treated by Laser Shock Peening. United States. https://doi.org/10.1007/s11837-020-04054-2
Tan, Qing, Yan, Zhiran, Huang, Hua, Li, Shilei, Wang, Yandong, Feng, Yefei, Zhou, Xin, Li, Yinghong, Ren, Yang, and Antonov, Stoichko. Wed .
"Surface Integrity and Oxidation of a Powder Metallurgy Ni-Based Superalloy Treated by Laser Shock Peening". United States. https://doi.org/10.1007/s11837-020-04054-2. https://www.osti.gov/servlets/purl/1668069.
@article{osti_1668069,
title = {Surface Integrity and Oxidation of a Powder Metallurgy Ni-Based Superalloy Treated by Laser Shock Peening},
author = {Tan, Qing and Yan, Zhiran and Huang, Hua and Li, Shilei and Wang, Yandong and Feng, Yefei and Zhou, Xin and Li, Yinghong and Ren, Yang and Antonov, Stoichko},
abstractNote = {Laser shock peening is a mechanical surface treatment which can induce large compressive residual stresses and microstructural changes in the material by using repetitive shocks from laser pulses. In this work, the surface integrity (surface microstructure, topography, hardness and residual stress) of a laser shock peening treated powder metallurgy Ni-based superalloy was investigated. Laser shock peening treatment introduces large plastic deformation especially at a depth of about 100 μm from the surface, which increases the local hardness. The residual stress from the surface to the interior of the sample was investigated by synchrotron X-ray diffraction. The maximum compressive stress reaches 400 MPa at the surface, while the depth of the compressive stress is about 0.7 mm. Lastly, the oxidation behavior of the treated and untreated samples was evaluated by thermal exposure at 700°C for 312 h. The LSP treatment decreased the thickness of oxide layer, thereby showing improved oxidation resistance.},
doi = {10.1007/s11837-020-04054-2},
journal = {JOM. Journal of the Minerals, Metals & Materials Society},
number = 5,
volume = 72,
place = {United States},
year = {Wed Feb 12 00:00:00 EST 2020},
month = {Wed Feb 12 00:00:00 EST 2020}
}
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