材料科学技术(英文版)2022,Vol.104Issue(9) :269-284.

Thermal cycling creep properties of a directionally solidified superalloy DZ125

Wenrui An Satoshi Utada Xiaotong Guo Stoichko Antonov Weiwei Zheng Jonathan Cormier Qiang Feng
材料科学技术(英文版)2022,Vol.104Issue(9) :269-284.

Thermal cycling creep properties of a directionally solidified superalloy DZ125

Wenrui An 1Satoshi Utada 2Xiaotong Guo 3Stoichko Antonov 4Weiwei Zheng 1Jonathan Cormier 2Qiang Feng1
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作者信息

  • 1. Beijing Advanced Innovation Center for Materials Genome Engineering,State Key Laboratory for Advanced Metals and Materials,University of Science and Technology Beijing,Beijing 100083,China
  • 2. Institut Pprime,UPR CNRS 3346,Department of Physics and Mechanics of Materials,ISAE-ENSMA,BP40109,86961 Futuroscope Chasseneuil Cedex,France
  • 3. China Electronic Product Reliability and Environmental Testing Research Institute,Guangzhou 510610,China
  • 4. Department of Microstructure Physics and Alloy Design,Max-Planck-Institut für Eisenforschung GmbH,Düsseldorf 40237,Germany
  • 折叠

Abstract

Aero-engine turbine blades may suffer overheating during service,which can result in severe microstruc-tural and mechanical degradation within tens of seconds.In this study,the thermal cycling creep under(950℃/15 min+1100℃/1 min)-100 MPa was performed on a directionally solidified superalloy,DZ125.The effects of overheating and thermal cycling on the creep properties were evaluated in terms of creep behavior and microstructural evolution against isothermally crept specimens under 950℃/100 MPa,950℃/270 MPa,and 1100℃/100 MPa.The results indicated that the thermal cycling creep life was reduced dramatically compared to the isothermal creep under 950℃/100 MPa.The plastic creep deformation mainly occurred during the overheating stage during the thermal cycling creep.The thermal cycling creep curve exhibited three stages,similar to the 1100℃isothermal creep,but its minimum creep rate oc-curred at a lower creep strain.The overheating events caused severe microstructural degradation,such as substantial dissolution of y'phase,earlier formation of rafted y'microstructure,widening of the y chan-nels,and instability of the interfacial dislocation networks.This microstructural degradation was the main reason for the dramatic decrease in thermal cycling creep life,as the thermal cycling promoted more dis-locations to cut into y'phase and more cracks to initiate at grain boundaries,carbides,and residual eutectic pools.This study underlines the importance of evaluating the thermal cycling creep properties of superalloys to be used as turbine blades and provides insights into the effect of thermal cycling on directionally solidified superalloys for component design.

Key words

Directional solidified superalloy/Thermal cycling creep/Overheating/Creep properties/Microstructural degradation

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基金项目

National Key Research and Development Program of China(2016YFB0701403")

theNational Natural Science Foundation of China(51631008)

theNational Natural Science Foundation of China(91860201)

as well as the111 Project(B170003)

Institut Pprime gratefully acknowledgesContrat de Plan Etat-Région Nouvelle-Aquitaine CPER)as well as theFonds Européen de Dével()

Alexander von Humboldt Foundation()

出版年

2022
材料科学技术(英文版)
中国金属学会 中国材料研究学会 中国科学院金属研究所

材料科学技术(英文版)

CSTPCDCSCDSCI
影响因子:0.657
ISSN:1005-0302
被引量1
参考文献量61
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