Effects of secondary orientation and temperature on the fretting fatigue behaviors of Ni-based single crystal superalloys

被引：36

作者：

Su, Yue ^{[1
]}

Han, Qi-Nan ^{[2
]}

Zhang, Cheng-Cheng ^{[3
]}

Shi, Hui-Ji ^{[1
]}

Niu, Li-Sha ^{[1
]}

Deng, Guo-Jian ^{[3
]}

Rui, Shao-Shi ^{[1
]}

机构：

[1] Tsinghua Univ, AML, Sch Aerosp Engn, Beijing 100084, Peoples R China

[2] Aircraft Strength Res Inst China, Xian 710065, Shaanxi, Peoples R China

[3] Aero Engine Grp Corp China, Shanghai Engn Res Ctr Commercial Aircraft Engine, Commercial Aircraft Engine Co Ltd, Shanghai 200241, Peoples R China

来源：

TRIBOLOGY INTERNATIONAL | 2019年 / 130卷

基金：

中国国家自然科学基金;

关键词：

Fretting fatigue; Ni-based single crystal superalloys; Secondary orientation; Temperature effect; PLASTICITY FINITE-ELEMENT; SITU SEM OBSERVATION; CRITICAL-PLANE; CYCLE FATIGUE; CRACK INITIATION; LIFE PREDICTION; DOVETAIL JOINT; NICKEL; SIMULATION; DEFORMATION;

D O I：

10.1016/j.triboint.2018.09.006

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

A dovetail fixture for fretting fatigue test was designed. Fretting fatigue experiments were performed for Nibased single crystal (NBSX) superalloys at 600 and 700 degrees C in two secondary orientations, [110] and [010]. The influence of secondary orientation and temperature on fretting fatigue behavior was investigated. The crystal plasticity finite element (CPFE) simulation was used to study the stress field at the contact region. The result indicates that the stress distribution is correlated to fretting damage, which is consistent with the crack initiation site. Fretting fatigue life is predicted based on critical plane method, which is in good agreement with the experimental result.

引用

页码：9 / 18

页数：10

共 54 条

[1] Fretting stresses in single crystal superalloy turbine blade attachments [J].

Arakere, NK ;

Swanson, G .

JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2001, 123 (02) :413-423

[2]

Arakere NK, 2000, EFFECT CRYSTAL ORIEN

[3] Failure analysis of a third stage gas turbine blade [J].

Barella, S. ;

Boniardi, M. ;

Cincera, S. ;

Pellin, P. ;

Degive, X. ;

Gijbels, S. .

ENGINEERING FAILURE ANALYSIS, 2011, 18 (01) :386-393

[4] Fatigue crack propagation simulation in an aircraft engine fan blade attachment [J].

Barlow, KW ;

Chandra, R .

INTERNATIONAL JOURNAL OF FATIGUE, 2005, 27 (10-12) :1661-1668

[5]

Celel A., 1988, Superalloys, V1988

[6] CONSTITUTIVE-EQUATIONS FOR CYCLIC PLASTICITY AND CYCLIC VISCOPLASTICITY [J].

CHABOCHE, JL .

INTERNATIONAL JOURNAL OF PLASTICITY, 1989, 5 (03) :247-302

[7]

Chu C.C., 1993, ADV MULTIAXIAL FATIG

[8] A CRITICAL PLANE APPROACH TO MULTIAXIAL FATIGUE DAMAGE INCLUDING OUT-OF-PHASE LOADING [J].

FATEMI, A ;

SOCIE, DF .

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 1988, 11 (03) :149-165

[9]

Findley W.N., 1958, A Theory for the Effect of Mean Stress on Fatigue of Metals Under Combined Torsion and Axial Load Or Bending

[10] The influence of contacting Ni-based single-crystal superalloys on fretting fatigue of Ni-based polycrystalline superalloys at high temperature [J].

Fleury, R. M. N. ;

Paynter, R. J. H. ;

Nowell, D. .

TRIBOLOGY INTERNATIONAL, 2014, 76 :63-72

← 1 2 3 4 5 6 →