Effect of prior oxidation on high cycle fatigue performance of RR1000 and role of oxidation in fatigue crack initiation

被引:9
作者
Cruchley, S. [1 ]
Taylor, M. P. [1 ]
Li, H. Y. [1 ]
Evans, H. E. [1 ]
Bowen, P. [1 ]
Child, D. J. [2 ]
Hardy, M. C. [2 ]
机构
[1] Univ Birmingham, Sch Met & Mat, Birmingham B15 2TT, W Midlands, England
[2] Rolls Royce PLC, Derby DE24 8BJ, England
基金
英国工程与自然科学研究理事会;
关键词
Oxidation; Fatigue crack initiation; High cycle fatigue; GRAIN-BOUNDARY OXIDATION; NI-BASED SUPERALLOY; MECHANISM; ALLOY; BEHAVIOR; KINETICS; GROWTH; DAMAGE; TIP;
D O I
10.1179/0960340914Z.00000000064
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The effect of prior oxidation on the room temperature fatigue life of coarse grained Ni based superalloy, RR1000 has been performed at an R ratio of 0.1 with two pre-oxidation times: 100 and 2000 h at 700 degrees C. These pre-exposures produce extensive oxidation damage. The room temperature high cycle fatigue life of the pre-oxidised specimens has been compared to as received specimens. At a maximum applied stress of 800 MPa a significant fatigue life deficit is observed in the pre-oxidised testpieces. This is accompanied with the observations of significant cracking of the external chromia scale and the intergranular internal oxides within the area of maximum stress. Preferential cracking of oxides may lead to early crack initiation and consequently a reduction in total fatigue life.
引用
收藏
页码:68 / 73
页数:6
相关论文
共 22 条
[1]   Cyclic Oxidation Behavior of IN 718 Superalloy in Air at High Temperatures [J].
Al-hatab, Kh. A. ;
Al-bukhaiti, M. A. ;
Krupp, U. ;
Kantehm, M. .
OXIDATION OF METALS, 2011, 75 (3-4) :209-228
[2]   INTERGRANULAR CRACK TIP OXIDATION MECHANISM IN A NICKEL-BASED SUPERALLOY [J].
ANDRIEU, E ;
MOLINS, R ;
GHONEM, H ;
PINEAU, A .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1992, 154 (01) :21-28
[3]   LOW-CYCLE FATIGUE OF RENE-80 AS AFFECTED BY PRIOR EXPOSURE [J].
ANTOLOVICH, SD ;
DOMAS, P ;
STRUDEL, JL .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1979, 10 (12) :1859-1868
[4]   Oxidation behavior of several chromia-forming commercial nickel-base superalloys [J].
Chen, JH ;
Rogers, PM ;
Little, JA .
OXIDATION OF METALS, 1997, 47 (5-6) :381-410
[5]   Characterisation of subsurface oxidation damage in Ni based superalloy, RR1000 [J].
Cruchley, S. ;
Taylor, M. P. ;
Evans, H. E. ;
Hardy, M. C. ;
Child, D. J. .
MATERIALS SCIENCE AND TECHNOLOGY, 2014, 30 (15) :1884-1889
[6]  
Cruchley S, 2012, SUPERALLOYS 2012, P751
[7]   Chromia layer growth on a Ni-based superalloy: Sub-parabolic kinetics and the role of titanium [J].
Cruchley, S. ;
Evans, H. E. ;
Taylor, M. P. ;
Hardy, M. C. ;
Stekovic, S. .
CORROSION SCIENCE, 2013, 75 :58-66
[8]   Evaluation of oxidation related damage caused to a gas turbine disc alloy between 700 and 800°C [J].
Encinas-Oropesa, A. ;
Simms, N. J. ;
Nicholls, J. R. ;
Drew, G. L. ;
Leggett, J. ;
Hardy, M. C. .
MATERIALS AT HIGH TEMPERATURES, 2009, 26 (03) :241-249
[9]   A mechanism for stress-aided grain boundary oxidation ahead of cracks [J].
Evans, H. E. ;
Li, H. Y. ;
Bowen, P. .
SCRIPTA MATERIALIA, 2013, 69 (02) :179-182
[10]  
EVANS HE, 1995, INT MATER REV, V40, P1, DOI 10.1179/095066095790151124