EFFECT OF HOLD TIME ONLOW CYCLE FATIGUE CRACK GROWTH BEHAVIOR AT HIGH TEMPERATURE IN TWO TURBINE DISK ALLOYS

Shen Zhumin;Xie Jizhou

Journal of Aeronautical Materials ›› 1995, Vol. 15 ›› Issue (4) : 54-61.

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PDF(483 KB)
Journal of Aeronautical Materials ›› 1995, Vol. 15 ›› Issue (4) : 54-61.

EFFECT OF HOLD TIME ONLOW CYCLE FATIGUE CRACK GROWTH BEHAVIOR AT HIGH TEMPERATURE IN TWO TURBINE DISK ALLOYS

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Abstract

The low cycle fatigue crack growth behaviors with and without hold time on upon peak load and itspropagation life prediction model were investigated for two turbine disk superalloys used extensively.

Key words

hold time / low cycle fatigue / creep / crack growth rate

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Shen Zhumin, Xie Jizhou. EFFECT OF HOLD TIME ONLOW CYCLE FATIGUE CRACK GROWTH BEHAVIOR AT HIGH TEMPERATURE IN TWO TURBINE DISK ALLOYS[J]. Journal of Aeronautical Materials, 1995, 15(4): 54-61

References

[2] Baudin G,Policella H. A Pulsed D C P D Technique-Application to Three-Dimensional Crack Fronts,ONERA,France,Dec,1988
诸武扬等.断裂韧性测试.北京:科学出版社,1979,78
[3] Hoffelner W. Effect of Enviroment on Crack Growth Behavior of Superalloys Under Various Loading Conditions,Materials Science & Technology.1987,3(3):765
[4] Shahinlan P. Creep-Fatigue-Enviorment Interactions on Crack Propagation in Alloy 718. Conf on Engng Aspects of Creep,1980,2:1
[5] Keh-Minna Chang. Time Dependent Fatigne Crack Propagation in IN718 Superalloy,Mechanical Behavior of Materials,1987,2:1139
[6] Saxena A,Shih T T. Characterizing and Predicting Crack Growth Behavior in Alloys at Elevated Temperature.5th Interconf.of Fracture.France,1980:2403
[7] Pedron J P,Pin,4. Effect of Hold Time on The Elevated Temperature Fatigue Crack Growth Behavfor of IN718 Alloy. Advances in Fracture Research,Sth.Int on Fracture,1981,5:2385.
[8] Saxena A.et aI..AModel for Represating and predicting The Influence of Hold Time on Fatigne Crack Growth Behavior at Elevated Temperature,ASTM STP 743,1981:86.
[9] Sayda J. Fatigue Crack Propagation of Ni-base Superalloys at 650-C ,ASTM STP 942,1988:293.
[10] Sadananda K.et al. Met Trans,1972,8A:439.
[11] Riedel H.Rice J R. Tensile Crack in Creeping Solids.Fracture Mechanics 12th Conf.,1979
[12] Shahani V,et al,Evaluation of Cycle Behavior of Aircraft Turbine Disk Alloys,NASA-CR-159433. 1978.
[13] ENSIP参考资料(5),发动机关键件上应用的损伤容限概念.606研究所,1988
[14] 哈宽富.金属力学性质的微观理论.1980;648
[15] 吴四发,孔庆平.GH901合金的蠕变裂纹扩展.金属学报,1988,24(6):51
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