High Temperature Low Cycle Fatigue Behavior of GH4742 Alloy
High temperature low cycle fatigue tests on GH4742 superalloy were studied under the total strain-con- trolled conditions at 650 ℃. Combined with fatigue test data, fatigue properties of the alloy were analyzed. Fracture morphology and dislocation structure were observed by scanning electron microsc...
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Published in | Journal of iron and steel research, international Vol. 22; no. 6; pp. 551 - 556 |
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Main Authors | , , , , |
Format | Journal Article |
Language | English |
Published |
Singapore
Elsevier Ltd
01.06.2015
Springer Singapore |
Subjects | |
Online Access | Get full text |
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Summary: | High temperature low cycle fatigue tests on GH4742 superalloy were studied under the total strain-con- trolled conditions at 650 ℃. Combined with fatigue test data, fatigue properties of the alloy were analyzed. Fracture morphology and dislocation structure were observed by scanning electron microscopy and transmission electron mi- croscopy. The results showed that fatigue life and fatigue resistance of GH4742 alloy decreased significantly with in- creasing total strain amplitude. The cyclic hardening, cyclic softening and cyclic stability phenomena of the alloy oc- curred during the low cycle fatigue process. The increasing total strain amplitude is conducive to the formation of γ1 phase. Fatigue crack propagation is controlled jointly by ductile and brittle fracture. Inhomogeneous deformation and deformation restricted in slip bands are the main reasons for the reduction of fatigue life of GH4742 alloy. |
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Bibliography: | 11-3678/TF superalloy; low cycle fatigue; cyclic hardening; cyclic softening; fracture morphology; dislocation structure High temperature low cycle fatigue tests on GH4742 superalloy were studied under the total strain-con- trolled conditions at 650 ℃. Combined with fatigue test data, fatigue properties of the alloy were analyzed. Fracture morphology and dislocation structure were observed by scanning electron microscopy and transmission electron mi- croscopy. The results showed that fatigue life and fatigue resistance of GH4742 alloy decreased significantly with in- creasing total strain amplitude. The cyclic hardening, cyclic softening and cyclic stability phenomena of the alloy oc- curred during the low cycle fatigue process. The increasing total strain amplitude is conducive to the formation of γ1 phase. Fatigue crack propagation is controlled jointly by ductile and brittle fracture. Inhomogeneous deformation and deformation restricted in slip bands are the main reasons for the reduction of fatigue life of GH4742 alloy. |
ISSN: | 1006-706X 2210-3988 |
DOI: | 10.1016/S1006-706X(15)30039-X |