オーステンパ処理球状黒鉛鋳鉄の長寿命域における疲労強度
スポンサーリンク
概要
- 論文の詳細を見る
This paper describes the effects of shot peening and artificial small defects on the fatigue strength of austempered ductile cast iron (ADI). The fatigue strength of smooth specimens was increased by shot peening in a short life regime and the increments reached about 33 and 29% at 10^5 and 10^6 cycles, respectively. The improvement of fatigue strength, however, almost disappeared in a long life regime of 10^8 cycles. Small drilling holes were used as artificial defects. The diameters of the holes were 0.1,0.2,0.3 and 0.4mm and their depths were almost the same as the diameter. The fatigue strength of the specimens with a 0.1mm drilling hole did not decrease when compared with that of the smooth specimens, but the fatigue strengths of the specimens with 0.2〜0.4mm drilling holes decreased. The experimental results of the specimens with 0.2〜0.4mm drilling holes were consistent with the predlction by Murakami's √<area> parameter model. The maximum size, (√<area>)_<max>, of the pre-existent defects in ADI was equivalent to the defect of the specimen with a 0.1mm drilling hole and was estimated to be about 90 μm by the above model.
- 一般社団法人日本機械学会の論文
- 1997-06-25
著者
関連論文
- 136 Ti-6Al-4V 合金切欠き材の高温疲労強度に及ぼすショットピーニングの影響
- Ti-6Al-4V合金の高温疲労強度に及ぼすショットピーニングの影響(疲労)
- 412 Ti-4Al-22V 合金の疲労強度に及ぼすショットピーニングの影響
- β型Ti-22V-4Al合金の疲労挙動に及ぼす冷間加工の影響
- 切欠き付Ti-6Al-4V合金ショット材の高温疲労特性
- 126 β型Ti-22V-4Al合金の疲労挙動に及ぼす冷間加工の影響(チタン,疲労の機構と強度信頼性,オーガナイスドセッション1,第53期学術講演会)
- 620 β型 Ti-22V-4Al 合金の疲労強度に及ぼす冷間加工の影響
- 105 表面組織改質したβ型 Ti-22V-4Al 合金の疲労挙動
- 炭素鋼の高温疲労限度に及ぼす微小人工欠陥の影響
- 122 鋳造アルミニウム合金 AC4CH 切欠き材の疲労挙動
- Ti-6Al-4V合金ショット材の高温疲労特性(疲労)
- オーステンパ処理球状黒鉛鋳鉄の長寿命域における疲労強度
- 高温におけるTi-6Al-4V合金の疲労強度に及ぼす人工微小欠陥の影響
- 二相ステンレス鋼における大き裂と微小き裂の疲労き裂進展特性
- Al-Li 合金の静的強度と回転曲げ疲労強度
- 純チタンの微小疲労き裂成長挙動とその確率特性
- 131 Al-Li合金の静的強度と回転曲げ疲労強度(疲労強度)