See the published version of this preprint at The International Journal of Advanced Manufacturing Technology.
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Research Article
Ilyas Kacar
Nigde Ömer Halisdemir Üniversitesi
Corresponding Author
ORCiD: https://orcid.org/0000-0002-5887-8807
License:
This work is licensed under a CC BY 4.0 License. Read Full License
6XXX series aluminum alloys are generally excellent alternatives to steels for many forged parts in aerospace and automotive industries. In this study, the forging performance of the 6082 aluminum alloy is investigated in order to replace the existing material for forged steel parts. The effect of artificial aging of the alloy on the microstructure and mechanical properties is studied. Optimum aging conditions are determined. Results reveal that AA6082 could be a good replacement for applications where shock and vibrational loads exist. The rod end part currently manufactured from AISI1045 can be replaced by AA6082 without any design changes. The major drawback is that the cold forging of the aged alloy is poor due to its brittle nature and crack initiations. Therefore, warm or hot forging is recommended to overcome the poor forgeability.
Keywords
Al-Si alloy, AA6082, artificial aging, hot forging, fatigue, automotive
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CURRENT STATUS: Published
View the published article at The International Journal of Advanced Manufacturing Technology.
Version 1
Posted 11 Mar, 2021
No community comments so far
Reviews received
Received 07 Mar, 2021
Reviewers invited
Invitations sent on 06 Mar, 2021
Editor assigned
On 28 Feb, 2021
First submitted
On 22 Feb, 2021
Metrics
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HTML Views: ...
Subject Areas
Biotechnology and Bioengineering
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A new preprint design is coming!
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See the published version of this preprint at The International Journal of Advanced Manufacturing Technology.
This is a preprint, a preliminary version of a manuscript that has not completed peer review at a journal. Research Square does not conduct peer review prior to posting preprints. The posting of a preprint on this server should not be interpreted as an endorsement of its validity or suitability for dissemination as established information or for guiding clinical practice.
Learn more about In Review
Research Article
Ilyas Kacar
Nigde Ömer Halisdemir Üniversitesi
Corresponding Author
ORCiD: https://orcid.org/0000-0002-5887-8807
Badges
Prescreen
This manuscript passed our Prescreen assessment
Complete author information
Appropriate declaration statements
Potential risks to human health
Prescreen
Peer Review Timeline
CURRENT STATUS: Published
View the published article at The International Journal of Advanced Manufacturing Technology.
Version 1
Posted 11 Mar, 2021
No community comments so far
Reviews received
Received 07 Mar, 2021
Reviewers invited
Invitations sent on 06 Mar, 2021
Editor assigned
On 28 Feb, 2021
First submitted
On 22 Feb, 2021
Metrics
Comments: 0
PDF Downloads: ...
HTML Views: ...
Subject Areas
Biotechnology and Bioengineering
License:
This work is licensed under a CC BY 4.0 License. Read Full License
View the published article at The International Journal of Advanced Manufacturing Technology.
6XXX series aluminum alloys are generally excellent alternatives to steels for many forged parts in aerospace and automotive industries. In this study, the forging performance of the 6082 aluminum alloy is investigated in order to replace the existing material for forged steel parts. The effect of artificial aging of the alloy on the microstructure and mechanical properties is studied. Optimum aging conditions are determined. Results reveal that AA6082 could be a good replacement for applications where shock and vibrational loads exist. The rod end part currently manufactured from AISI1045 can be replaced by AA6082 without any design changes. The major drawback is that the cold forging of the aged alloy is poor due to its brittle nature and crack initiations. Therefore, warm or hot forging is recommended to overcome the poor forgeability.
Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
Figure 6
Figure 7
Figure 8
Figure 9
Figure 10
Figure 11
Figure 12
Figure 13
Figure 14
Figure 15
Figure 16
Figure 17
Figure 18
Figure 19
This is a list of supplementary files associated with this preprint. Click to download.
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