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  1. B. 理工学域; 数物科学類・物質化学類・機械工学類・フロンティア工学類・電子情報通信学類・地球社会基盤学類・生命理工学類
  2. b 10. 学術雑誌掲載論文
  3. 1.査読済論文(工)

Thinning minimization for forming aluminum beverage can end shells

https://doi.org/10.24517/00008319
https://doi.org/10.24517/00008319
6a3968f7-f5ad-4d1d-9d35-9391aa440fa7
名前 / ファイル ライセンス アクション
TE-PR-YAMAZAKI-K-9045-478.pdf TE-PR-YAMAZAKI-K-9045-478.pdf (292.9 kB)
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Item type 学術雑誌論文 / Journal Article(1)
公開日 2017-10-03
タイトル
タイトル Thinning minimization for forming aluminum beverage can end shells
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ journal article
ID登録
ID登録 10.24517/00008319
ID登録タイプ JaLC
著者 Han, Jing

× Han, Jing

WEKO 11623

Han, Jing

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Yamazaki, Koetsu

× Yamazaki, Koetsu

WEKO 11624
e-Rad 70110608

Yamazaki, Koetsu

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Otsuka, Takayasu

× Otsuka, Takayasu

WEKO 11625

Otsuka, Takayasu

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Hasegawa, Takashi

× Hasegawa, Takashi

WEKO 11626
e-Rad 50272943

Hasegawa, Takashi

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Itoh, Ryoichi

× Itoh, Ryoichi

WEKO 11627

Itoh, Ryoichi

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ANishiyama, Sadao

× ANishiyama, Sadao

WEKO 11628

ANishiyama, Sadao

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著者別表示 山崎, 光悦

× 山崎, 光悦

山崎, 光悦

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長谷川, 卓

× 長谷川, 卓

長谷川, 卓

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書誌情報 13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 2010

号 2010, p. 9045, 発行日 2010-01-01
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 10.2514/6.2010-9045
出版者
出版者 American Institute of Aeronautics and Astronautics
抄録
内容記述タイプ Abstract
内容記述 Forming simulations of the can end shell have been implemented based on both of the axisymmetric model and three-dimensional models, for a better understanding of the forming process. The comparison shows that the simulation results agree reasonably well with the experimental observations of the actual forming process. The influence of the loads applied to tools, the clearance between tools, the shape of the tool profile and the position of tools have been investigated, based on the axisymmetric model to save computational time. The design optimization method based on the numerical simulations have been applied to search the optimum design points, in order to reduce the thinning subjected to the constraints of the geometric shape of the shell and the suppression of wrinkles. The optimization results show that the thinning can be improved up to 4% by optimizing the forming route, adjusting the clearance and the load, and modifying the tool shape. © 2010 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
著者版フラグ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
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