Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy
Co-Cr-W alloy was prepared by powder metallurgy technology. The effect of heat treatment temperature on the microstructure and mechanical properties of the prepared alloy was investigated by SEM and EPMA, etc. The results show that the phases in Co-Cr-W alloy under the heat treatment condition of 11...
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Journal of Aeronautical Materials
2018-12-01
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Series: | Journal of Aeronautical Materials |
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Online Access: | http://jam.biam.ac.cn/CN/Y2018/V38/I6/29 |
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author | CUI Yu SUN Yuan HOU Xingyu ZHANG Hongyu XUN Shuling HOU Guichen LIU Wenqiang ZHOU Yizhou |
author_facet | CUI Yu SUN Yuan HOU Xingyu ZHANG Hongyu XUN Shuling HOU Guichen LIU Wenqiang ZHOU Yizhou |
author_sort | CUI Yu |
collection | DOAJ |
description | Co-Cr-W alloy was prepared by powder metallurgy technology. The effect of heat treatment temperature on the microstructure and mechanical properties of the prepared alloy was investigated by SEM and EPMA, etc. The results show that the phases in Co-Cr-W alloy under the heat treatment condition of 1100 ℃ with holding time of 4 h and cooling without power is the same as before heat treatment. The matrix of alloy is composed of γ-Co with FCC structure, ε-Co with HCP structure, and the reinforced phases include M<sub>6</sub>C and M<sub>23</sub>C<sub>6</sub> carbides. The matrix of Co-Cr-W alloy under the heat treatment condition of 1150-1250 ℃ × 4 h is composed of single γ-Co in FCC structure and reinforced phases include M<sub>6</sub>C carbides and M<sub>23</sub>C<sub>6</sub> carbides. When the heat treatment temperature is increased from 1100 ℃ to 1200 ℃, the blocky M<sub>6</sub>C carbides and granular M<sub>23</sub>C<sub>6</sub> carbides grow up, meanwhile ε-Co phases are reduced and then disappeared, alloy density is improved, and tensile strength is increased. However, when the heat treatment temperature is above 1200 ℃, the performance of Co-Cr-W alloy has no obvious change, and the prepared alloy under the heat treatment condition of 1200 ℃ × 4 h achieves the optimal property with the average hardness of 63.5HRC and tensile strength of 408 MPa. |
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issn | 1005-5053 1005-5053 |
language | zho |
last_indexed | 2024-04-13T12:34:59Z |
publishDate | 2018-12-01 |
publisher | Journal of Aeronautical Materials |
record_format | Article |
series | Journal of Aeronautical Materials |
spelling | doaj.art-f2d2d5be99fd4447b2fd63ffa7b8b44c2022-12-22T02:46:41ZzhoJournal of Aeronautical MaterialsJournal of Aeronautical Materials1005-50531005-50532018-12-01386293510.11868/j.issn.1005-5053.2017.000187201806000187Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W AlloyCUI Yu0SUN Yuan1HOU Xingyu2ZHANG Hongyu3XUN Shuling4HOU Guichen5LIU Wenqiang6ZHOU Yizhou7AVIC Xi’an Aerospace Propulsion Control Technology Co., Ltd., Xi’an 710077, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaInstitute of Metal Research, Chinese Academy of Science, Shenyang 110016, ChinaCo-Cr-W alloy was prepared by powder metallurgy technology. The effect of heat treatment temperature on the microstructure and mechanical properties of the prepared alloy was investigated by SEM and EPMA, etc. The results show that the phases in Co-Cr-W alloy under the heat treatment condition of 1100 ℃ with holding time of 4 h and cooling without power is the same as before heat treatment. The matrix of alloy is composed of γ-Co with FCC structure, ε-Co with HCP structure, and the reinforced phases include M<sub>6</sub>C and M<sub>23</sub>C<sub>6</sub> carbides. The matrix of Co-Cr-W alloy under the heat treatment condition of 1150-1250 ℃ × 4 h is composed of single γ-Co in FCC structure and reinforced phases include M<sub>6</sub>C carbides and M<sub>23</sub>C<sub>6</sub> carbides. When the heat treatment temperature is increased from 1100 ℃ to 1200 ℃, the blocky M<sub>6</sub>C carbides and granular M<sub>23</sub>C<sub>6</sub> carbides grow up, meanwhile ε-Co phases are reduced and then disappeared, alloy density is improved, and tensile strength is increased. However, when the heat treatment temperature is above 1200 ℃, the performance of Co-Cr-W alloy has no obvious change, and the prepared alloy under the heat treatment condition of 1200 ℃ × 4 h achieves the optimal property with the average hardness of 63.5HRC and tensile strength of 408 MPa.http://jam.biam.ac.cn/CN/Y2018/V38/I6/29Co-Cr-W alloyheat treatment temperaturemicrostructuremechanical property |
spellingShingle | CUI Yu SUN Yuan HOU Xingyu ZHANG Hongyu XUN Shuling HOU Guichen LIU Wenqiang ZHOU Yizhou Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy Journal of Aeronautical Materials Co-Cr-W alloy heat treatment temperature microstructure mechanical property |
title | Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy |
title_full | Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy |
title_fullStr | Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy |
title_full_unstemmed | Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy |
title_short | Effect of Heat Treatment Temperature on Microstructure and Mechanical Properties of Co-Cr-W Alloy |
title_sort | effect of heat treatment temperature on microstructure and mechanical properties of co cr w alloy |
topic | Co-Cr-W alloy heat treatment temperature microstructure mechanical property |
url | http://jam.biam.ac.cn/CN/Y2018/V38/I6/29 |
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