Analysis on Gas Turbine Rotor Life Based on Elastoplastic Theory

A compressor rotor crack accident occurred in 13E2 gas turbine used for combined cycle in Shenzhen Nantian Power Plant. To accurately predict the fatigue life of similar units, based on elastic-plastic theory, considering the influence of temperature field and centrifugal force on fatigue life of co...

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Bibliographic Details
Main Authors: Jiwei DING, Yan LI
Format: Article
Language:English
Published: Editorial Department of Power Generation Technology 2020-04-01
Series:发电技术
Subjects:
Online Access:https://www.pgtjournal.com/EN/10.12096/j.2096-4528.pgt.18183
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Summary:A compressor rotor crack accident occurred in 13E2 gas turbine used for combined cycle in Shenzhen Nantian Power Plant. To accurately predict the fatigue life of similar units, based on elastic-plastic theory, considering the influence of temperature field and centrifugal force on fatigue life of compressor compressor rotor, the finite element thermo-solid coupling numerical simulation model of the compressor rotor of the gas turbine was established. Based on the low cycle fatigue theory, it is calculated that the fatigue life of the gas turbine compressor rotor is 5333 times, and the actual fatigue life of the compressor rotor of the gas turbine in the power plant is 4435 times. The calculation error is within 20%. This method can be used to estimate the rotor life of gas turbine accurately.
ISSN:2096-4528