A topologized resolved shear stress method for the life prediction of nickel-base single crystal superalloys

被引:18
作者
Li, Piao [1 ]
Yao, Weixing [1 ,2 ]
Shi, Huiji [3 ]
Luo, Peng [1 ]
Hua, Yichang [1 ]
机构
[1] Key Lab Fundamental Sci Natl Def Adv Design Techn, Nanjing 210016, Peoples R China
[2] State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
[3] Tsinghua Univ, Sch Aerosp, AML, Beijing 100084, Peoples R China
关键词
Nickel-base single crystal superalloy; Fatigue life evaluation; Multiaxial damage parameter; Topologized resolved shear stress; LOW-CYCLE FATIGUE; CRACK-GROWTH-BEHAVIOR; CRITICAL PLANE; CRYSTALLOGRAPHIC ORIENTATION; TEMPERATURE-DEPENDENCE; MECHANICAL-PROPERTIES; WOHLER CURVE; DAMAGE; FRACTURE; EVOLUTION;
D O I
10.1016/j.tafmec.2020.102624
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Fifteen multiaxial critical-plane fatigue damage parameters of isotropic metal materials are applied to the life evaluation of nickel-base single crystal superalloys. These parameters are classified into stress-, strain- and strain-energy parameters, and their predictive abilities are evaluated by 12 groups of single crystal fatigue data obtained from mainly an intermediate temperature range (500-760 degrees C) where the slip deformation is the main damage mode. The results show that the strain energy group exhibits the best fitting characteristics with correlation coefficients. A topologized resolved shear stress method (TRSS) considering the interaction of main slip systems is further proposed. The dispersion degree of resolved shear stress among the main slip systems is quantified by a dispersion factor, and the real driving capacity of resolved shear stress is amended according to the topology of driving force. The obtained results show that the proposed method has achieved an improvement of correlation ability.
引用
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页数:20
相关论文
共 87 条
[1]  
[Anonymous], 2013, THESIS LINKOPING U
[2]   High-temperature fatigue properties of single crystal superalloys in air and hydrogen [J].
Arakere, NK .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2004, 126 (03) :590-603
[3]   Effect of crystal orientation on fatigue failure of single crystal nickel base turbine blade superalloys [J].
Arakere, NK ;
Swanson, G .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2002, 124 (01) :161-176
[4]   Evolution of Ni-based superalloys for single crystal gas turbine blade applications [J].
Caron, P ;
Khan, T .
AEROSPACE SCIENCE AND TECHNOLOGY, 1999, 3 (08) :513-523
[5]   Expected principal stress directions under multiaxial random loading. Part I: theoretical aspects of the weight function method [J].
Carpinteri, A ;
Macha, E ;
Brighenti, R ;
Spagnoli, A .
INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (01) :83-88
[6]   Expected principal stress directions under multiaxial random loading. Part II: numerical simulation and experimental assessment through the weight function method [J].
Carpinteri, A ;
Brighenti, R ;
Macha, E ;
Spagnoli, A .
INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (01) :89-96
[7]   ELEVATED-TEMPERATURE FATIGUE CRACK-GROWTH BEHAVIOR OF MAR-M200 SINGLE-CRYSTALS [J].
CHAN, KS ;
LEVERANT, GR .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1987, 18 (04) :593-602
[8]   INFLUENCE OF ORIENTATION ON THE LOW-CYCLE FATIGUE OF MAR-M200 SINGLE-CRYSTALS AT 650-DEGREES-C .1. FATIGUE LIFE BEHAVIOR [J].
CHIERAGATTI, R ;
REMY, L .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1991, 141 (01) :1-9
[9]   INFLUENCE OF ORIENTATION ON THE LOW-CYCLE FATIGUE OF MAR-M200 SINGLE-CRYSTALS AT 650-DEGREE-C .2. CYCLIC STRESS-STRAIN BEHAVIOR [J].
CHIERAGATTI, R ;
REMY, L .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1991, 141 (01) :11-22
[10]  
Chu C.C., 1993, ADV MULTIAXIAL FATIG, P37