Fatigue Damage Research on Rod-Fastening Rotor of Gas Turbine Considering Start-Up Stage

Article Preview

Abstract:

Fatigue damage was analyzed of the rod-fastening rotor of gas turbine in the process of frequent start-up. The maximum stress of rotor was calculated, applying nonlinear damage mechanics model to analyze the fatigue damage of the rotor in the process of startup. Finally, we get the damage quantity in each process of start. It provides certain theoretical basis on slowing degradation velocity of the rotor.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

221-226

Citation:

Online since:

August 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Frank J. Brooks. GE gas turbine performance characteristics[R]. GE Power Systems. Schenectady, NY, (2000).

Google Scholar

[2] Meherwan P. Boyce. Gas turbine engineering handbook. paper[M]. Oxford UK : 2012: 841-842.

Google Scholar

[3] I.S. Diakunchak. Performance deterioration in industrial gas turbines [J]. Journal of Engineering for Gas Turbines and Power, 1992, 114(2): 161-168.

DOI: 10.1115/1.2906565

Google Scholar

[4] MacLeod, J. D., Taylor, V., and Laflamme, J. C. G., 1991, Implanted component faults and their effects on gas turbine engine performance, ASME Paper 91-GT-41, (1992).

Google Scholar

[5] Chaboche J L. Continuum damage mechanics: Part 2, Transaction of the ASME[J]. Journal of Applied Mechanics, 1988, 55(1): 65-72.

Google Scholar

[6] Chaboche J L. Continuum damage mechanics: present state and future trends[J]. Nuclear Engineer & Design, 1987, 105: 19-33.

DOI: 10.1016/0029-5493(87)90225-1

Google Scholar

[7] Wang Zhixing, Zhou Dian. Fine grain microstructure of hot die ring and the high cycle fatigue performance of GH4169.

Google Scholar

[8] Wang Weiguo, Zhen Wen. 12CrMoV steel low cycle fatigue damage research. Materials science and technology, 2005, 13(22):193-195.

Google Scholar

[9] Wang Weimin. Combination of heavy-duty gas turbine rotor structure of contact interface strength and the design method of system dynamics research[D]. XiAn. Xi 'an jiaotong university, (2012).

Google Scholar