Title :
Thermo-elasto-plastic Stress and Strain Analysis and Life Prediction of Gas Turbine Blade
Author :
Zhu, Jiang-jiang ; Yang, Zi-chun
Author_Institution :
Coll. of ship & power, Naval Univ. of Eng., Wuhan, China
Abstract :
Finite element method was used to compute the thermo-elasto-plastic stress and strain fields of turbine blade according to typical loading spectrum. Controlled-strain test of turbine blade material was carried to get some necessary parameters used in life prediction formulas. On the basis of the above analysis, fatigue life of gas turbine blade was estimated.
Keywords :
blades; elastoplasticity; fatigue; finite element analysis; gas turbines; remaining life assessment; stress-strain relations; thermoelasticity; fatigue life; finite element method; gas turbine blade; life prediction; stress-strain analysis; thermoelastoplasticity; Blades; Capacitive sensors; Fatigue; Finite element methods; Plastics; Temperature; Thermal force; Thermal stresses; Transient analysis; Turbines; controlled-strain test; fatigue life; finite element method; gas turbine blade;
Conference_Titel :
Measuring Technology and Mechatronics Automation (ICMTMA), 2010 International Conference on
Conference_Location :
Changsha City
Print_ISBN :
978-1-4244-5001-5
Electronic_ISBN :
978-1-4244-5739-7
DOI :
10.1109/ICMTMA.2010.374
