Turbine blade fatigue life evaluating method
View Patent ↗In order to provide a turbine blade fatigue life evaluating method for quantitively evaluating the fatigue life of a turbine blade, the turbine blade is determined to be within its fatigue life if the creep elongation strain in the longitudinal direction of the turbine blade is less than 0.5% of an initial length, and is determined to exceed its fatigue life if the creep elongation strain is 0.5% or more than the initial length. A turbine blade creep elongation strain measuring apparatus 20 comprises a first fixed end 21 , a second fixed end 22 , and a dial gauge 24 . A dimension in the longitudinal direction is stamped on the surface of a turbine blade.
1. A turbine blade fatigue life evaluating method, comprising:
measuring an initial length of a turbine blade in an initial state in which a creep elongation strain is zero;
marking the initial length on the turbine blade;
marking wall temperature of the turbine blade which is measured when the initial-dimension is measured, onto the turbine blade;
measuring a post-operation length of the turbine blade after being operated for a predetermined time;
estimating a creep elongation strain in a longitudinal direction of the turbine blade based on the initial length and the post-operation length; and
evaluating that the turbine blade is within its fatigue life if the creep elongation strain is less than 0.5% of the initial length, or evaluating that the turbine blade exceeds its fatigue life if the creep elongation strain is equal to or more than 0.5% of the initial length.
2. The turbine blade fatigue life evaluating method according to claim 1 , further comprising correcting the post-operation length considering a thermal expansion amount of the turbine blade when the creep elongation strain is evaluated.
3. The turbine blade fatigue life evaluating method according to claim 1 , further comprising setting wall temperature of the turbine blade when the post-operation length is measured, equal to wall temperature of the turbine blade when the initial length is measured.
4. The turbine blade fatigue life evaluating method according to claim 1 , further comprising estimating how many operable hours are remained until the end of a fatigue life of the turbine blade.