DocumentCode :
2317697
Title :
On-line calculation model of thermal stress of steam turbine rotor based on integrated modular modeling software
Author :
Liu, Yanfeng ; Hao, Runtian ; Gao, Jianqiang ; Zhai, Rutao ; Fan, Xiaoying
Author_Institution :
Sch. of Energy & Power Eng., North China Electr. Power Univ., Baoding
fYear :
2008
fDate :
21-24 April 2008
Firstpage :
136
Lastpage :
139
Abstract :
The formula of two-dimensional temperature and thermal stress of steam turbine rotor is derived by using energy-balance method. The on-line calculation model of two dimensional temperature and thermal stress of steam turbine rotor is built based on integrated modular modeling software and engineering modularized method. A simulation experiment has been given to compare with the result computed by finite-element method on the same condition. The result shows this model has gained high accuracy and speed. The modularized structure of simulation model makes it very convenient that modification of physical dimension of the turbine rotor and the grids, so this model can be used for analyzing thermal state of other axis-symmetry object having similar boundary condition.
Keywords :
finite element analysis; power engineering computing; rotors; steam turbines; thermal stresses; energy- balance method; engineering modularized method; finite-element method; integrated modular modeling software; online calculation model; steam turbine rotor; thermal stress; two-dimensional temperature; Internal stresses; Mathematical model; Power engineering and energy; Rotors; Temperature; Thermal engineering; Thermal expansion; Thermal factors; Thermal stresses; Turbines; integrated modular modeling software; model; on-line; thermal stress; turbine rotor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Condition Monitoring and Diagnosis, 2008. CMD 2008. International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-1621-9
Electronic_ISBN :
978-1-4244-1622-6
Type :
conf
DOI :
10.1109/CMD.2008.4580248
Filename :
4580248
Link To Document :
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