알루미늄 합금 용접재의 피로파괴에 미치는 잔유응력의 영향에 관한 연구

A Study on the Influence of Residual Stresses on Fatigue Fracture of Aluminum Alloy Weldments

  • 차용훈 (조선대학교 기계공학과(수송기계부품 공장자동화 연구센터))
  • 발행 : 1995.12.01

초록

This study is to inspect the influence of the initial residual stress on fatigue crack growth behavior after the distribution of the initial residual stress is measured when the crack is growing from the compressive residual stress field. Also, the tensile residual stress field. Also, the influence of the variation of residual stress distribution on fatigue crack growth behavior at the crack tip is studied when the initial crack occurs on weld metal, bead interface and HAZ (Heat Affected Zone), respectively. For this purpose, CT-type specimen that crack parallel to the welding bead were manufactured by butt welding on the Al. Alloy 1100-O plate.

키워드

참고문헌

  1. Third Edition Metallury of Welding J.F.Lancaster
  2. 改訂最新鏞接工學 詠本春義
  3. International Sries on Materials Science and Technology v.33 Analysys of Welded Structrres K.Masubuchi
  4. 大宇造船工業株式會社 技術紙(大宇造船 技術) v.3 no.10 疲勞强度에 미치는 鎔接缺陷의 影響 이광주
  5. Thans. of JWS 2-2 Analysis of Theramal Elastic-Plastic Stress and Strain during Welding by Finite Element Method Y.Ueda;T.Yamakawa
  6. ASTM STP776 Effect of Residual Stress on Fatigue Crack Propagantion D.V.Nelson
  7. Trans. ASME. J. Appl. Mech. v.6 Bearing Pressures and Cracks H.M.Westerrgaad
  8. ASTM STP 776 Effect of Residual Stresses on Fatigue Crack Growth Rate in Weldment of Aluminum Alloy 5456 Plate G.E.Nordmark;L.N.Muller;R.A.Kelsey
  9. ASTM STP 743 Effectof Residual Stresses on Fatige Crack Growth Rate Measurement R.J.Buci
  10. ASTM STP 776 Residual Stress and Stress Interaction in Fatigue Testing of Welded Joint S.Berge;O.I.Eide
  11. ASTM STP 776 Effect of Residual Stresses on Fatigue Crack Growth Rate in Weldment of Aluminum Alloy 5456 Plate G.E.Nordmtk;L.N.Muller;R.A.Kelsey
  12. ASTM STP 648 Influence of Residual Seresses on Fatigue Crack Propagation in Electroslag Wels B.M.Kapadia
  13. ASTM E647-83 Standard Test Method for Constant-Load Amplitue Fatigue Crack Growth Rate Above 10-8mm/Cycle
  14. SFA-5.10 Material Specifications. Part C-Welding Rods. Electrodes. and Filler Metals. ASME