A nonlinear continuum damage mechanics model is proposed to assess the high temperature creep life of a steam turbine rotor, in which the effect of mean stress is taken into account and the damage is accumulated nonlinearly. The model is applied to a 300 MW steam turbine under hot start operation. The results are compared with those from the linear accumulation theory that is dominant in the creep life assessment of steam turbine rotors at present. The comparison results show that the nonlinear continuum damage mechanics model describes the accumulation and development of damage better than the linear accumulation theory.
Issue Section:
Gas Turbines: Structures and Dynamics
1.
Sedmak
, A.
, and Sedmak
, S.
, 1995, “Critical Crack Assessment Procedure for High Pressure Steam Turbine Rotors
,” Fatigue Fract. Eng. Mater. Struct.
8756-758X 18
, pp. 923
–934
.2.
Chaboche
, J. L.
, 1987, “Continuum Damage Mechanics: Present State and Future Trends
,” Nucl. Eng. Des.
0029-5493, 105
, pp. 19
–33
.3.
Lemaitre
, J.
, 1984, “How to Use Damage Mechanics
,” Nucl. Eng. Des.
0029-5493 80
, 233
–245
.4.
Lemaitre
, J.
, 1979, “Application of Damage Concepts to Predict Creep-Fatigue failures, Transaction of the ASME
,” J. Eng. Mater. Technol.
0094-4289 101
, 284
–292
.5.
Wang
X. J
, and Shi
K. Z.
, 1998, “Life Prediction of 300 MW Steam Turbine Under Cold Start
,” Turbine Technology
40
(5
), 269
–271
.6.
Zhang
B. H.
, 1988, “Life Management and Load-Peak Adjustment Running of Large Capacity Fossil Power Generator
,” Water Power and Electric Power Publishing Company
, Peking, China, pp. 19
–27
.7.
Li
J.
, and Zhou
J. L.
, 2000, “Investigation on Creep Performance of 30Cr1MolV Rotor Steel
,” Physical & Chemical Test-Physics Fascicule.
36
(1
), 10
–12
8.
Li.
Y. W
, and Li
C. B.
, 1998, “Investigation on Low-Cycle Performance of 30Cr1Mo1V Rotor Steel and Damage Evolution
,” Turbine Technology.
40
(4
), 248
–250
9.
Chaboche
J. L.
, 1988, “Continuum Damage Mechanics: Part II
,” Trans. ASME, J. Appl. Mech.
0021-8936 55
(1
), 65
–72
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