The invention provides a test
system and method for a
turbine blade integrated thin film temperature sensor, which solves the problem that the existing
turbine blade integrated thin film temperature sensor cannot adopt an industrial
thermocouple temperature measurement calibration mode. The
system comprises a heating box, an instantaneous heating unit, an imaging unit, a standard
thermocouple, a check meter and a
control unit, wherein the instantaneous heating unit comprises a
laser, a condensation unit and a rotary table; the condensation unit is located outside the observation opening in the side wall of the heating box and on an emergent light path of the
laser; the condensation unit is arranged on the rotary table; the imaging unit is arranged outside the observation opening of the heating box; the number of the standard thermocouples is equal to that of the thin film temperature sensors on the
turbine blade to be measured, and the positions are in one-to-one correspondence; the thin film temperature sensor and the standard
thermocouple are respectively connected with the check meter; the
control unit controls the emergent energy of the
laser and is connected with the rotary table; and the
control unit compares the temperatures obtained by the thin film temperature sensor and the standard thermocouple, and judges whether the performance of the thin film temperature sensor is qualified or not.