Metrology & Measurement Technology, Volume. 45, Issue 1, 88(2025)

Research on turbine blade surface temperature field measurement system based on multi⁃spectrum

Xuecong ZHANG, Lei DONG, Weichen HU, Jing CAI, and Yuan LI
Author Affiliations
  • AVIC Changcheng Institute of Metrology & Measurement, Beijing100095, China
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    Figures & Tables(12)
    Schematic diagram of probe working principle
    Principle of software
    Physical pictures of fixed mirror scanning probe and movable mirror scanning probe
    Calibration process
    Diagram of relationship between engine and probe parameter settings
    Scanning mode test flowchart
    Basic process of data parsing
    Schematic diagram of uncertainty distribution evaluated using Monte Carlo method
    Interface diagram of 2D and 3D temperature field reconstruction effect
    Radial temperature analysis results
    Circumferential temperature analysis results
    • Table 1. Index of turbine blade surface temperature field measurement system

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      Table 1. Index of turbine blade surface temperature field measurement system

      温度测量范围 / ℃最大允许误差 / ℃频率响应采样率 / (MSa / s)靶点直径 / mm行程 / mm
      550 ~ 1 500± 7.5DC ~ 300 kHz(± 3 dB)52≥ 100
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    Xuecong ZHANG, Lei DONG, Weichen HU, Jing CAI, Yuan LI. Research on turbine blade surface temperature field measurement system based on multi⁃spectrum[J]. Metrology & Measurement Technology, 2025, 45(1): 88

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    Paper Information

    Category: Theory and Method

    Received: Dec. 28, 2024

    Accepted: --

    Published Online: Jul. 23, 2025

    The Author Email:

    DOI:10.11823/j.issn.1674-5795.2025.01.06

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