Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment

Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment

  • CN 103,459,996 A
  • Filed: 02/07/2012
  • Published: 12/18/2013
  • Est. Priority Date: 02/09/2011
  • Status: Active Application
First Claim
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1. the method for the heat radiation figure of the turbine components in the high-temp combustion environment of calibrating turbine, described method comprises:

  • By at least one spot material arrangements on the surface of turbine components;

    Imager is arranged in the visual field of described at least one spot in imager, to obtain the imaging data of described at least one spot;

    Increase the temperature of the burning situation of turbine;

    When the temperature of burning situation turbine increases, process imaging data to produce the image sequence of described at least one spot;

    When the temperature of burning situation turbine increases, the image sequence of monitoring described at least one spot is with the generation of the physical change of determining described at least one spot;

    AndWhen determining described at least one spot generation physical change, distribute the first temperature value to the surface of turbine components.

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