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Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties
Astroloy is a Ni-based superalloy with high-volume fraction of γ′, which gives high temperature properties but reduces its forgeability. Therefore, powder metallurgy manufacturing processes such as Near Net Shape HIPping are the most suitable manufacturing technology for Astroloy. However, NNSHIP ha...
Autores principales: | , , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2022
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8874756/ https://www.ncbi.nlm.nih.gov/pubmed/35207974 http://dx.doi.org/10.3390/ma15041434 |
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author | Napal, Unai Galech Segarra, Miren Aristizabal Lazcano, Borja Elguezabal Sivo, Antonio Zubillaga, Iñigo Iturriza |
author_facet | Napal, Unai Galech Segarra, Miren Aristizabal Lazcano, Borja Elguezabal Sivo, Antonio Zubillaga, Iñigo Iturriza |
author_sort | Napal, Unai Galech |
collection | PubMed |
description | Astroloy is a Ni-based superalloy with high-volume fraction of γ′, which gives high temperature properties but reduces its forgeability. Therefore, powder metallurgy manufacturing processes such as Near Net Shape HIPping are the most suitable manufacturing technology for Astroloy. However, NNSHIP has its own drawbacks, such as the formation of prior particle boundaries (PPBs), which usually tend to decrease material mechanical properties. The detrimental effect of PPBs can be reduced by optimizing the entire HIP processing route. Conventional HIP cycles have very low cooling rates, especially in big components from industry, and thus a series of post-heat treatments must be applied in order to achieve desirable microstructures and improve the mechanical properties. Standard heat treatments for Astroloy are long and tedious with several steps of solutioning, stabilization and precipitation. In this work, two main studies have been performed. First, the effect of the cooling rate after the solutioning treatment, which is driven by the materials’ thermal mass, on the Astroloy microstructure and mechanical properties was studied. Experimental analyses and simulation techniques have been used in the present work and it has been found that higher cooling rates after solutioning increase the density of tertiary γ′ precipitates by 85%, and their size decreases by 22%, which leads to an increase in hardness from 356 to 372 HB30. This hardness difference tends to reduce after subsequent standard heat treatment (HT) that homogenizes the microstructure. The second study shows the effect of different heat treatments on the microstructure and hardness of samples with two different thermal masses (can and cube). More than double the density of γ′ precipitates was found in small cubes in comparison with cans with a higher thermal mass. Therefore, the hardness in cubes is between 4 and 20 HB 30 higher than in large cans, depending on the applied HT. |
format | Online Article Text |
id | pubmed-8874756 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2022 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-88747562022-02-26 Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties Napal, Unai Galech Segarra, Miren Aristizabal Lazcano, Borja Elguezabal Sivo, Antonio Zubillaga, Iñigo Iturriza Materials (Basel) Article Astroloy is a Ni-based superalloy with high-volume fraction of γ′, which gives high temperature properties but reduces its forgeability. Therefore, powder metallurgy manufacturing processes such as Near Net Shape HIPping are the most suitable manufacturing technology for Astroloy. However, NNSHIP has its own drawbacks, such as the formation of prior particle boundaries (PPBs), which usually tend to decrease material mechanical properties. The detrimental effect of PPBs can be reduced by optimizing the entire HIP processing route. Conventional HIP cycles have very low cooling rates, especially in big components from industry, and thus a series of post-heat treatments must be applied in order to achieve desirable microstructures and improve the mechanical properties. Standard heat treatments for Astroloy are long and tedious with several steps of solutioning, stabilization and precipitation. In this work, two main studies have been performed. First, the effect of the cooling rate after the solutioning treatment, which is driven by the materials’ thermal mass, on the Astroloy microstructure and mechanical properties was studied. Experimental analyses and simulation techniques have been used in the present work and it has been found that higher cooling rates after solutioning increase the density of tertiary γ′ precipitates by 85%, and their size decreases by 22%, which leads to an increase in hardness from 356 to 372 HB30. This hardness difference tends to reduce after subsequent standard heat treatment (HT) that homogenizes the microstructure. The second study shows the effect of different heat treatments on the microstructure and hardness of samples with two different thermal masses (can and cube). More than double the density of γ′ precipitates was found in small cubes in comparison with cans with a higher thermal mass. Therefore, the hardness in cubes is between 4 and 20 HB 30 higher than in large cans, depending on the applied HT. MDPI 2022-02-15 /pmc/articles/PMC8874756/ /pubmed/35207974 http://dx.doi.org/10.3390/ma15041434 Text en © 2022 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). |
spellingShingle | Article Napal, Unai Galech Segarra, Miren Aristizabal Lazcano, Borja Elguezabal Sivo, Antonio Zubillaga, Iñigo Iturriza Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title | Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title_full | Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title_fullStr | Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title_full_unstemmed | Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title_short | Thermal Mass Effect on the Solution Cooling Rate and on HIPped Astroloy Component Properties |
title_sort | thermal mass effect on the solution cooling rate and on hipped astroloy component properties |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8874756/ https://www.ncbi.nlm.nih.gov/pubmed/35207974 http://dx.doi.org/10.3390/ma15041434 |
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