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CONDITION BASED LIFING OF GAS TURBINE ENGINE COMPONENTS
CONDITION BASED LIFING OF GAS TURBINE ENGINE COMPONENTS
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机译:基于条件的燃气轮机发动机组件提升
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摘要
A system and methods for the condition based lifing of a gas turbine engine component is disclosed. The system and methods determine the stress and caused by fatigue and creep for each load cycle of the gas turbine engine, and use a ductility exhaustion method to combine the fatigue and creep strain rates determined from the fatigue and creep stresses to determine the remaining useful of the gas turbine engine component.
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