書誌事項
- タイトル別名
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- Estimation of Fatigue Life of Al-Alloy Used for Compressor Disc of Jet Engine
- ジェット エンジンヨウ コンプレッサー ディスク ニ シヨウシテ イル アルミ
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抄録
Compressor discs of jet engines and turbine discs of gas turbine engines are usually subjected to a combined stress σcomb of centrifugal stress σt and thermal stress σth in the tangential direction during flight or start-stop time. However, there has been few studies on the life prediction for such components made of Al-alloy (2014-T6) at the condition of about 120°C and σcomb of 21 to 22 kg/mm2 during rotation. In this report, the life was estimated from the creep rupture data at 212, 400 and 600°F using the prediction method proposed by the authors.
収録刊行物
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- 材料
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材料 28 (307), 272-277, 1979
公益社団法人 日本材料学会
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詳細情報 詳細情報について
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- CRID
- 1390001205417342592
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- NII論文ID
- 110002298099
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- NII書誌ID
- AN00096175
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- ISSN
- 18807488
- 05145163
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- NDL書誌ID
- 2049121
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- データソース種別
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- JaLC
- NDL
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- 抄録ライセンスフラグ
- 使用不可