A mandrel-free hot-spinning was developed as a near-net-shape titanium alloy plate forming technique. In this work, a Ti–6Al–4V alloy conical product with a wall angle of 34 deg and 170 mm height was formed from a large size Ti–6Al–4V plate (890–920 mm diameter × 30 mm thick). The product was characterized metallurgically and mechanical properties were measured, and the shape of formed products was investigated. It was found that the mandrel-free hot-spinning is able to form a large size titanium alloy plate. Material properties including tensile strength and microstructure of the formed products satisfied the material specifications. Fatigue stress of the formed product was higher than that of the typical Ti–6Al–4V material. For a further improvement, a forming method using preformed material was proposed and which was successfully conducted with two types of preforms and found to be effective in the forming process.
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March 2019
Research-Article
An Experimental Study for the Development of Mandrel-Free Hot-Spinning for Large Size Titanium Alloy Plate Forming
Yoshihide Imamura,
Yoshihide Imamura
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: imamura_yoshihide@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: imamura_yoshihide@khi.co.jp
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Ken Ikawa,
Ken Ikawa
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: ikawa_ken@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: ikawa_ken@khi.co.jp
Search for other works by this author on:
Kojiro Motoyama,
Kojiro Motoyama
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: motoyama_kojiro@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: motoyama_kojiro@khi.co.jp
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Hayato Iwasaki,
Hayato Iwasaki
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: iwasaki_ha@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: iwasaki_ha@khi.co.jp
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Takeo Hirakawa,
Takeo Hirakawa
Engine Production Engineering Department,
Manufacturing Division,
Aerospace Systems Company,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: hirakawa_t@khi.co.jp
Manufacturing Division,
Aerospace Systems Company,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: hirakawa_t@khi.co.jp
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Hiroshi Utsunomiya
Hiroshi Utsunomiya
Professor
Division of Materials and
Manufacturing Science,
Graduate School of Engineering,
Osaka University,
2-1, Yamada-oka, Suita City,
Osaka 565-0871, Japan
e-mail: uts@mat.eng.osaka-u.ac.jp
Division of Materials and
Manufacturing Science,
Graduate School of Engineering,
Osaka University,
2-1, Yamada-oka, Suita City,
Osaka 565-0871, Japan
e-mail: uts@mat.eng.osaka-u.ac.jp
Search for other works by this author on:
Yoshihide Imamura
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: imamura_yoshihide@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: imamura_yoshihide@khi.co.jp
Ken Ikawa
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: ikawa_ken@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: ikawa_ken@khi.co.jp
Kojiro Motoyama
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: motoyama_kojiro@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: motoyama_kojiro@khi.co.jp
Hayato Iwasaki
Material Research Department,
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: iwasaki_ha@khi.co.jp
Technical Institute,
Corporate Technology Division,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: iwasaki_ha@khi.co.jp
Takeo Hirakawa
Engine Production Engineering Department,
Manufacturing Division,
Aerospace Systems Company,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: hirakawa_t@khi.co.jp
Manufacturing Division,
Aerospace Systems Company,
Kawasaki Heavy Industries, Ltd.,
1-1, Kawasaki-cho,
Akashi City 673-8666, Hyogo, Japan
e-mail: hirakawa_t@khi.co.jp
Hiroshi Utsunomiya
Professor
Division of Materials and
Manufacturing Science,
Graduate School of Engineering,
Osaka University,
2-1, Yamada-oka, Suita City,
Osaka 565-0871, Japan
e-mail: uts@mat.eng.osaka-u.ac.jp
Division of Materials and
Manufacturing Science,
Graduate School of Engineering,
Osaka University,
2-1, Yamada-oka, Suita City,
Osaka 565-0871, Japan
e-mail: uts@mat.eng.osaka-u.ac.jp
1Corresponding author.
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 9, 2018; final manuscript received July 24, 2018; published online October 4, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Mar 2019, 141(3): 032501 (8 pages)
Published Online: October 4, 2018
Article history
Received:
July 9, 2018
Revised:
July 24, 2018
Citation
Imamura, Y., Ikawa, K., Motoyama, K., Iwasaki, H., Hirakawa, T., and Utsunomiya, H. (October 4, 2018). "An Experimental Study for the Development of Mandrel-Free Hot-Spinning for Large Size Titanium Alloy Plate Forming." ASME. J. Eng. Gas Turbines Power. March 2019; 141(3): 032501. https://doi.org/10.1115/1.4041161
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