The invention provides a
turbine blade
radiation temperature measurement error
correction method based on a reflected
radiation model, and the method comprises the steps: building a reflected
radiation model through considering the reflected radiation of a preceding-stage guide blade, an adjacent moving blade and a
combustion chamber wall surface at the same time; calculating a
radiation angle coefficient between
turbine blades and a
radiation angle coefficient between wall surfaces of a
combustion chamber by using a surrounding channel
integral method; temperature distribution of the surface of the
turbine blade and the wall surface of the
combustion chamber at different temperatures is obtained through comsol
simulation; and designing a multiple reflection radiation formula, accurately calculating the reflection radiation of the hot end part, and obtaining a corrected
radiation temperature measurement result through inversion. According to the method, reflection radiation of a front-stage guide vane, adjacent movable vanes and a
combustion chamber wall surface is considered, a surrounding channel
integral method is adopted,
surface element shielding between blade surfaces is considered, and a
turbine blade surface
radiation angle coefficient is calculated; the wall surface of the
combustion chamber is increased, the reflection radiation of the hot end component is considered, a multiple reflection radiation formula is designed, the accurate reflection radiation of the hot end component is obtained, the reflection radiation
calculation error is reduced, and the
turbine blade radiation temperature measurement precision is improved.