A method for managing lifespans of high temperature gas...

G - Physics – 06 – F

Patent

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G06F 17/40 (2006.01) F02C 7/00 (2006.01) F02C 9/00 (2006.01) G01M 13/00 (2006.01) G01M 15/00 (2006.01)

Patent

CA 2432746

It provides a method for managing the remaining life of a high temperature component used in a gas turbine that enables a state of fatigue of a high temperature component to be evaluated and controlled with a high level of accuracy, and a program medium for performing the method for managing the remaining life of a high temperature gas turbine component on a computer. In the method for managing the lifespan of a high temperature component used in a gas turbine, the lifespan of a high temperature component being evaluated is set within an operating area bounded by a component life limit line that is determined on the basis of field data giving the correlation between the operating time and operating cycles for the state of fatigue from past high temperature components. As the program medium, a medium is employed that is provided with a program in which this method is used for managing a lifespan of a high temperature component used in a gas turbine.

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