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  • 1  Research progress on total temperature measurement and calibration technology of gas flow
    ZHAO Jian
    2026, 46(2):1-9. DOI: 10.11823/j.issn.1674-5795.2026.02.01
    [Abstract](83) [HTML](100) [PDF 8.42 M](73)
    Abstract:
    A systematic review is conducted on the research progress of total temperature measurement and calibration technology for gas flow. High-precision, high-temperature, and high-frequency gas flow total temperature measurement methods, as well as steady-state and dynamic calibration techniques for temperature sensors based on calibration wind tunnels are summarized. The principles and applicable scenarios of various techniques are elaborated. The sources of errors in airflow total temperature measurement and the technical challenges in typical scenarios such as engines are analyzed. The development trend of total temperature measurement and calibration of gas flow under multi field coupling and extreme working conditions is explored. Constructive suggestions are proposed, including the integration of non-contact and contact measurement technologies and the enhancement of calibration capabilities under extreme conditions, which can provide reference and ideas for improving the accuracy of total temperature measurement in complex and extreme environments and supporting the high-quality development of aerospace and power systems.
    2  Application progress of turbine blade temperature radiation thermometry technology
    MA Hongwei GAO Ruolin
    2025, 45(1). DOI: 10.11823/j.issn.1674-5795.2025.01.02
    [Abstract](604) [HTML](167) [PDF 12.28 M](665)
    Abstract:
    Compared with the traditional temperature measurement technology, radiation thermometry technology offers the advantages of non-contact measurement, fast response and excellent high-temperature adaptability. It enables real-time measurement of the surface temperature distribution of key components such as turbine rotor blades. It introduces the basic principles, technical characteristics and application scope of various radiation temperature measurement methods including brightness thermometry, colorimetric thermometry, charge-coupled device (CCD) thermometry, and multi-wavelength radiation thermometry. The application and development status of radiation thermometry technology in turbine blade temperature measurement are described, and the future development direction of this technology is discussed. It is pointed out that the accuracy and reliability of radiation thermometry technology can be further improved by optimizing the design of optical probe, using more advanced algorithms, and applying new type of high-temperature-resistant materials; and that the radiation thermometry technology can be combined with thermocouple thermometry technology to build a more precise and stable turbine blade temperature monitoring system.
    3  Research on turbine blade surface temperature field measurement system based on multi-spectrum
    ZHANG Xuecong DONG Lei HU Weichen CAI Jing LI Yuan
    2025, 45(1). DOI: 10.11823/j.issn.1674-5795.2025.01.06
    [Abstract](596) [HTML](154) [PDF 2.49 M](651)
    Abstract:
    Due to the strong background radiation inside the aero engine, there is a large deviation between the temperature value obtained by measuring the surface of the turbine blade using the conventional radiation temperature measurement system and the actual temperature value. To address this issue, a new generation of turbine blade surface temperature measurement system was developed based on the principle of multispectral temperature measurement. The system uses movable mirror probes and fixed mirror probes to achieve high-reliability scanning, realizes efficient signal acquisition and precise control of equipment through high-speed multi-channel synchronous signal acquisition and control system, and realizes online measurement and reconstruction of three-dimensional temperature field on the blade surface by using multispectral temperature measurement modeling in complex thermal environment, multi-view three-dimensional temperature field reconstruction and other technologies. The performance indexes of the multispectral turbine blade surface temperature field measurement system were tested by using a blackbody radiation source and a dynamic calibration device, and the results showed that the system could achieve real-time online measurement of the surface temperature of turbine blades at 550 ~ 1 500 ℃, and the maximum allowable error did not exceed ± 7.5 ℃, which met the temperature measurement requirements of turbine blades. The research results provide strong support for promoting the development of thermal parameter testing technology for aeroengine turbine blades in high-temperature and complex environments.
    4  Calibration device for thermocouple response time constant based on gas temperature step method
    JIN Ran HUANG Yuqi ZHU Liang
    2025, 45(6):86-94. DOI: 10.11823/j.issn.1674-5795.2025.06.07
    [Abstract](228) [HTML](122) [PDF 5.66 M](308)
    Abstract:
    To address the calibration demand for the response time constant of fast-response K-type thermocouples under gas medium conditions, a calibration device based on the gas temperature step method was developed. Key para-meters including heater power, orifice area, and nozzle flow rate were determined via theoretical calculations, and Ansys Fluent software was utilized for simulation to optimize the structure of the step temperature generation module. A calibration method based on synchronous dynamic pressure monitoring was proposed, which takes the pressure step moment as the reference to eliminate non-ideal excitation interference and ensure the calculation accuracy of the response time constant. Experimental tests were conducted using the developed device, and the results indicate that the gas temperature step amplitude generated by the device exceeds 200 ℃ with a temperature step excitation time of approximately 2.2 ms. The device can effectively calibrate the response time constant of K-type thermocouples with different wire diameters, demonstrating a significant engineering application value.
    5  Calibration of convective heat flux using a dual-plate transient method
    ZHENG Jianhua ZHAO Jian WANG Xiaolu HU Lintao KONG Xiangxue ZHAO Yijun
    2025, 45(6):141-152. DOI: 10.11823/j.issn.1674-5795.2025.06.12
    [Abstract](191) [HTML](126) [PDF 6.98 M](273)
    Abstract:
    Accurate heat flux measurement is essential for developing hypersonic vehicles and their thermal protection systems. The intense aerodynamic heating generated during high-speed flight of aerospace vehicles is primarily dominated by convective heat transfer. However, existing heat flux gauges struggle to accurately measure surface thermal loads under extreme high-temperature and high-speed conditions, resulting in low measurement accuracy and significantly constraining the performance evaluation of thermal protection systems and material development. To address the lack of reliable calibration methods for heat flux sensors under high-temperature and high-speed conditions, this study introduces a dual-plate transient calibration method. This method adopts a highly accurate thin-film platinum resistance sensor as a reference, installs a Gardon gauge to be calibrated with the sensor together on a displacement ejection mechanism, and simulates the high-speed flight scenario of the aircraft in the wind tunnel to achieve the calibration to the Gardon heat flux gauge under airflow conditions. Calibration experiments were conducted at a flight Mach number of 0.3 and temperatures from 100 °C to 300 °C for the developed convective heat flux measurement device. The results demonstrate that the relative expanded uncertainty is 4.2% (k = 2), and this method can effectively obtain the convective heat flux sensitivity coefficient of the Gardon heat flux meter. The dual plate transient calibration method proposed in this paper provides new ideas and approaches for high-temperature and high-speed convective heat flux calibration, significantly improving the reliability of convective heat flux measurement data and providing strong technical support for the development of hypersonic aircraft and accurate measurement of thermal loads in thermal protection systems.
    6  Design and application of chamber furnace for solving thin-film thermocouple static temperature testing challenges
    WANG Yida TIAN Qingyun CHEN Yong KONG Xiangxue MANG Kexin WANG Sujie SHI Jiyuan
    2025, 45(6):153-160. DOI: 10.11823/j.issn.1674-5795.2025.06.13
    [Abstract](172) [HTML](93) [PDF 2.83 M](243)
    Abstract:
    Traditional test equipment struggles to meet the high-precision and efficient static temperature testing requirements of thin-film thermocouples in high-temperature environments. To address this issue, a chamber furnace with large-space and precise temperature control functions has been developed. The furnace body adopts a split-type multi-layer structure design. Its side thermal insulation components can be flexibly disassembled to eliminate installation obstructions, satisfying the testing needs of thin-film thermocouples with different shapes. High-efficiency heating is achieved using three-section molybdenum disilicide heating elements, combined with a water-cooling system to realize precise temperature control and generate a stable and reliable temperature field. A three-dimensional thermodynamic model was established and simulated using ANSYS Workbench 2019R3 software. The simulation results show that the temperature field at the measuring end and the temperature at the reference end of the sample meet the design expectations. Practical tests conducted with the developed box-type furnace indicate that the temperature fluctuation in the furnace's test coordinate system is 0.47 ℃ / 6 min, and the temperature field uniformity is better than 3 ℃ / 50 mm, which complies with the testing requirements for thin-film thermocouples. Tests on Au-Pt thin-film thermocouples were conducted using this box-type furnace, further verifying its application effectiveness. It provides important technical support for the static temperature characteristic detection of thin-film thermocouples.
    7  Broadband temperature measurement method for microcavities based on mode spacing matching
    CHEN Yincong CAI Jing YE Xi CHANG Haitao FEI Fan
    2026, 46(2):120-129. DOI: 10.11823/j.issn.1674-5795.2026.02.10
    [Abstract](69) [HTML](73) [PDF 4.40 M](60)
    Abstract:
    To address the limitation of traditional micro-ring resonator thermometry, which relies on tracking a single resonance peak, thereby restricting the measurement range to within the free spectral range, we propose a wide-spectrum microcavity temperature measurement method based on the matching of transverse electric (TE) and transverse magnetic (TM) mode spacing. A temperature measurement system was constructed, comprising a widely tunable laser, a silicon nitride micro-ring resonator, a Fabry-Pérot interferometer, and a water vapor absorption reference unit. Employing a two-stage calibration strategy that combines relative wavelength scale calibration with absolute wavelength anchoring, the system extracts the center wavelengths of resonance peaks and establishes a standard library of mode spacing values, thereby enabling temperature retrieval. Experimental results demonstrate that within the temperature range of -10℃ to 40℃, the mode spacing exhibits a strong linear correlation with temperature, yielding a coefficient of determination of 0.998. The measured temperature sensitivity for the TE single mode is 18.356 pm / K, while that for the TM single mode is 17.283 pm / K. The temperature measurement error of the traditional single resonance peak tracking method is ± 0.05 K, while the error of the microcavity broadband temperature measurement method based on mode spacing matching is ± 0.035 K. This approach not only improves measurement accuracy but also expands the measurement range, enhances system robustness and response efficiency, and provides important references for the engineering applications of microcavity photonic temperature measurement.
    8  Research on the optimization of data processing algorithms for measuring temperature field on turbine blade surface in complex thermal environments
    LI Yuan CAI Jing ZHANG Xuecong DONG Lei HU Weichen
    2026, 46(3):99-108. DOI: 10.11823/j.issn.1674-5795.2026.03.11
    [Abstract](40) [HTML](74) [PDF 5.81 M](50)
    Abstract:
    The traditional multispectral algorithm used for temperature field measurement on the surface of aeroengine turbine blades has high computational complexity, requiring singular value decomposition of spectral data for temperature field data calculation. In addition, the accuracy of turbine blade positioning signals is affected by simulated speed signals, resulting in deviations in temperature data. If no speed offset correction is performed, the calculated temperature data cannot accurately reflect the uneven combustion temperature and design defects of the blade discs and blades. To address the above issues, this paper optimizes the data processing algorithm for temperature field measurement on the surface of turbine blades in complex thermal environments, analyzes and constructs a multispectral temperature measurement model, and performs monochromatic temperature auxiliary calculation. Compared with the existing traditional multispectral optimization algorithm, the "multispectral + monochromatic temperature auxiliary correction" method improves the calculation efficiency by more than 30% without loss of temperature measurement accuracy. In addition, this paper proposes an adaptive speed offset correction algorithm that dynamically and adaptively adjusts the filter parameters. Compared with the existing adaptive correction algorithm, this method reduces the offset correction error by 15%. The optimized data processing algorithm for temperature field measurement on the surface of turbine blades can adapt to complex working conditions with multiple speeds, making up for the shortcomings of existing temperature measurement algorithms in engineering applications.
    9  A hierarchical physically constrained annular temperature field reconstruction method fusing RBF interpolation and CNN-LSTM
    LI Shuyuan ZHAO Jian
    2026, 46(3):109-120. DOI: 10.11823/j.issn.1674-5795.2026.03.12
    [Abstract](40) [HTML](272) [PDF 13.35 M](73)
    Abstract:
    Aiming at the complex distribution characteristics of annular temperature fields, including radial gradient heterogeneity, circumferential periodic fluctuation, and local temperature inversion, as well as the deficiencies of traditional reconstruction methods in annular structure adaptability and physical consistency, this paper proposes an annular temperature field reconstruction method combining adaptive Radial Basis Function (RBF) interpolation, a Convolutional Neural Network (CNN)-Long Short-Term Memory (LSTM) hybrid network, and hierarchical physical constraints. Firstly, a hybrid-kernel RBF interpolation with radially adaptive kernel parameters is adopted to construct the initial temperature field through sparse measurement data. Then, the CNN-LSTM hybrid network is utilized to extract spatial local features and circumferential periodic features to correct the residual error of the initial temperature field. Finally, according to the heat conduction law, differentiated hierarchical physical constraints are applied to different regions of the temperature field to improve the physical rationality and credibility of the reconstruction results. Multi-condition experimental results show that the reconstruction errors of the proposed method under typical working conditions of 500 K, 1 000 K, and 1 750 K all meet the engineering error threshold of 5%. The spatial resolution reaches 0.5 mm, which is better than the engineering index of 2 mm. Ablation experiments verify that the LSTM module ensures the circumferential continuity of the temperature field, and the hierarchical physical constraints significantly enhance the physical credibility of the reconstruction results. The proposed method can provide a reliable technical support for high-precision annular temperature field reconstruction, condition monitoring, and performance optimization of aero-engines.
    10  Novel in-situ automatic calibration approach for multi-channel temperature scanning valves
    CONG Yutao WANG Peng KONG Xiangxue JIN Zhentao
    2026, 46(3):121-131. DOI: 10.11823/j.issn.1674-5795.2026.03.13
    [Abstract](55) [HTML](29) [PDF 5.07 M](55)
    Abstract:
    Aiming at the problems of low efficiency, high cost, equipment disassembly requirement and potential equipment damage in traditional calibration methods for temperature scanning valves, this paper proposes a fully automatic in-situ calibration method based on a "four-layer architecture". A fully automatic in-situ calibration system for temperature scanning valves was constructed, adopting a four-layer architecture design consisting of standard signal layer, signal switching layer, data acquisition layer, and control and analysis layer. By using dedicated metering aviation plugs, on-site calibration was realized, eliminating the equipment disassembly and assembly steps required in traditional methods. Systematic parameter optimization experiments were performed, in which four key parameters including measurement time, data acquisition interval, two-point calibration standard value combination, and channel switching stabilization time were comparatively analyzed, and the optimal parameter configuration balancing accuracy and efficiency was determined. A fully automated calibration workflow was developed, enabling complete automatic execution from equipment connection, data acquisition to coefficient calculation and writing, which simplifies the operation process and reduces errors. The results show that under the optimal configuration (measurement time of 8 s, data acquisition interval of 250 ms, calibration standard values of (10 mV, 40 mV), and channel switching stabilization time of 3 750 ms), the measurement repeatability (standard deviation) of the system is 0.003 3 mV, corresponding to an equivalent temperature error of 0.083 ℃, which meets the requirement of an error not exceeding ± 0.5 ℃. The proposed calibration method provides a reliable metrology support for the engineering application of temperature scanning valves.
    11  Review of the development trends of dew point temperature sensors
    NIE Jing LIU Xi
    2024(1). DOI: 10.11823/j.issn.1674-5795.2024.01.04
    [Abstract](1036) [HTML](271) [PDF 1.45 M](2668)
    Abstract:
    Introducing the current research status in the field of dew-point temperature sensors, and expounding the principles and structures of optical, resonant, electrical, thermal, weight and chemical dew-point temperature sensors. It is pointed out that the optical dew point temperature sensor has high measurement accuracy, and the cold mirror dew point sensor can be used as the humidity measurement standard. The resonant dew point temperature sensor has the characteristics of small size, low cost, short response time, high sensitivity and good reliability. The electrical dew point temperature sensor has high sensitivity and low power consumption, which is convenient for miniaturization and integration. Gravimetric method is the most accurate absolute humidity measurement method and the basis for establishing humidity benchmark. Chemical methods are often used to measure organic gas mixtures in low humidity. The application of dew point temperature sensor in environmental monitoring, industrial manufacturing, medical diagnosis and other fields is discussed. It is pointed out that dew point temperature sensors will develop towards high precision, high stability and high response in the future, and their application range will be further expanded to meet the measurement needs in extreme environments.
    12  Review of measurement error and uncertainty analysis of luminescence thermometry
    FU Tairan WU Yusong ZHANG Changxian
    2024, 44(3). DOI: 10.11823/j.issn.1674-5795.2024.03.02
    [Abstract](1015) [HTML](263) [PDF 12.80 M](689)
    Abstract:
    In this paper, the basic principle of luminescence thermometry and the composition of typical systems are introduced, with discussion on the measurement errors and uncertainty evaluation models of luminescence thermometry. The importance of measurement error analysis and measurement uncertainty evaluation in the research and application of luminescence thermometer is pointed out. In the analysis of measurement errors, it is crucial to comprehensively consider the influence of internal device parameters and the measurement environment on luminescence thermometry parameters, such as luminescence lifetime and intensity ratio. It can significantly minimize systematic errors and enhance the accuracy of temperature measurement to optimize the excitation light source, phosphors, detectors, data acquisition, and data processing schemes, along with to conduct thorough environmental factor analysis and calibration. Furthermore, to investigate the physical mechanisms that cause variations in the emission characteristics of phosphor due to factors other than temperature can lay a theoretical foundation for developing more adaptable luminescence thermometry materials. In the evaluation of measurement uncertainty, the uncertainty in temperature measurement based on luminescence lifetime and intensity ratio can be described using mathematical models. This quantified temperature measurement uncertainty serves as a basis for guiding the optimization and application of high-precision luminescence thermometry systems.
    13  Overview of temperature measurement methods for engine turbine blades based on infrared radiation
    GAO Shan XIONG Xinmeng LIU Hailong
    2024(4). DOI: 10.11823/j.issn.1674-5795.2024.04.01
    [Abstract](983) [HTML](190) [PDF 9.61 M](1396)
    Abstract:
    This paper introduces the basic principles of radiation temperature measurement technology and key issues in research. The current application status of temperature measurement methods for engine turbine blades based on infrared radiation at home and abroad is summarized, the errors generated during measurement are analyzed, and the measures to reduce errors are proposed. It is pointed out that in terms of environmental radiation, it is necessary to fully consider the influence of combustion gases and environmental surface radiation, establish accurate reflection models, integrate algorithms, and correct radiation interference errors; In terms of emissivity modelling, emissivity model and non-emissivity model should be established in advance according to specific situations, and machine learning algorithms should be combined to improve measurement accuracy; In terms of optical system design, it is necessary to select appropriate optical materials and coatings to enhance the sensitivity of the system in different environments; In terms of data processing, methods such as neural networks, genetic algorithms, and constraint optimization can be used to minimize errors and improve computational accuracy to the greatest extent possible.
    14  Research progress of ultrasonic temperature measurement technology in ultra-high temperature extreme environments
    WANG Gao LIANG Haijian WEI Yanlong WANG Xinhui ZHAO Jian LI Xin
    2024, 44(5). DOI: 10.11823/j.issn.1674-5795.2024.05.01
    [Abstract](636) [HTML](247) [PDF 12.36 M](635)
    Abstract:
    This paper introduces the principles of contact ultrasonic guided wave temperature measurement technology, ultrasonic internal temperature gradient temperature measurement technology, and cross-beam ultrasonic temperature measurement technology. It describes the research status of ultrasonic temperature measurement technology, and the application cases and test results of ultrasonic temperature measurement technology in engine combustion chamber temperature measurement. This review analyzes the technical characteristics and potential problems of various ultrasonic temperature measurement techniques. It is pointed out that the study of high temperature oxidation resistant waveguide materials is the top priority in the development of ultrasonic guided wave temperature measurement technology. It is proposed that the temperature measurement range can be extended and the temperature measurement accuracy can be improved by developing new materials, new processes and new equipment, and constantly iterating the feature signal recognition algorithm model. This provides reference for further development of acoustic temperature measurement technology.
    15  Preparation of ITO-Pt flexible thin film thermocouples and optimization of their thermoelectric properties
    HUANG Mingjing LIU Zhaojun LI Yang GUO Zijun ZHANG Zhongkai TIAN Bian
    2024, 44(5). DOI: 10.11823/j.issn.1674-5795.2024.05.05
    [Abstract](692) [HTML](209) [PDF 8.00 M](886)
    Abstract:
    In order to solve the problems of deformation failure and low sensitivity of flexible thin-film thermocouples, a thermoelectric sensing model was established and thermal-electrical-force multi-field coupling simulations of flexible thin-film thermocouples were performed. Based on the results, the structural dimensions of the sensor were optimized, and a process method for optimizing the sensitivity by heat treatment was proposed, so as to prepare a thermoelectric Indium Tin Oxide-Platinum (ITO-Pt) thin-film temperature sensor based on polyimide substrate with high reliability and high sensitivity. The calibration test experiment proves that the sensor sensitivity reaches 40.10 μV / ℃, which can effectively meet the temperature testing requirements of human wearable devices and lithium battery health monitoring.
    16  Multi field synchronous testing of high-temperature gas for aircraft engines
    LIN Yin GUO Daoyong YIN Xiaoya HUANG Mingjing
    2024, 44(6). DOI: 10.11823/j.issn.1674-5795.2024.06.06
    [Abstract](634) [HTML](263) [PDF 11.11 M](909)
    Abstract:
    In order to solve the problem of high temperature gas flow field test in the whole process measurement of aero engine, a rotating multi-section and multi-parameter flow field scanning and measurement device was developed. The designed rotary scanning measurement section was used to replace the original hybrid diffuser section of a certain type of aero engine, the circumferential measurement point encryption was realized by controlling the rotation of the measurement section, and the temperature field, pressure field, velocity field, direction field and other parameters were measured at the turbine outlet and afterburner inlet of the aero engine at the same time. The feasibility of the design of the rotary scanning measurement device, the layout design of the temperature / pressure / velocity multi-field synchronous test, the reliability design of the probe, the accurate measurement of the temperature of high-temperature gas with a large declination angle, and the complex three-dimensional flow field measurement scheme with a large declination angle were verified by experiments. Then, tests were conducted under the test conditions of a certain type of aircraft engine to verify the practical application effect of the rotating multi-section and multi-parameter flow field scanning measurement device. This study provides important technical support for the performance evaluation and component matching research of aircraft engines.
    17  A temperature compensation model for QCM humidity sensor in high temperature environment based on deep learning
    FENG Junyi CUI Jianmin WEN Lianpeng WANG Guohua NIE Jing
    2023(5). DOI: 10.11823/j.issn.1674-5795.2023.05.04
    [Abstract](1005) [HTML](276) [PDF 2.88 M](1482)
    Abstract:
    To reduce the impact of temperature drift on sensor measurement results in high temperature and low humidity environments, a humidity sensor based on quartz crystal microbalance (QCM) was developed by using a quartz crystal with a fundamental frequency of 4 MHz as a substrate and depositing graphene oxide (GO) on the substrate using a drop-on-demand method. The temperature drift phenomenon of AT-cut quartz crystal wafers and graphene oxide materials in high temperature environments is significant, resulting in frequency output drift of the sensor. Therefore, a deep-learning method was used to correct the temperature drift. The adaptability of the back propagation (BP) neural network correction model to the QCM humidity sensor was tested under different absolute humidity conditions. The experimental results show that the correction model obtained through deep learning can effectively improve the sensitivity, stability, and response speed of the QCM humidity sensor. It is of great significance for studying the frequency correction technology of QCM humidity sensors under temperature and humidity coupling conditions.
    18  Performance evaluation of vacuum high-temperature blackbody radiation source
    DONG Lei REN Jia ZHANG Lan HU Weichen
    2023(6). DOI: 10.11823/j.issn.1674-5795.2023.06.13
    [Abstract](631) [HTML](244) [PDF 4.58 M](872)
    Abstract:
    In order to solve the calibration problem of radiation heat flux sensors in vacuum environments, a 50 mm large-diameter vacuum high-temperature blackbody radiation source device was developed by using pyrolytic graphite as the heating element, and measuring and controlling the temperature using a standard photoelectric pyrometer, and the performance indexes of the device were tested and evaluated. The temperature stability of the device within 10 min was not more than 0.5℃, and the radial temperature uniformity was not more than 0.1%t (t is the set temperature), which met the requirements of relevant regulations. Finally, the uncertainty components introduced by the performance indexes of the vacuum high-temperature blackbody radiation source in the process of heat flow calibration were calculated and analyzed. The research results provide strong support for promoting the application of the device in the calibrations of heat flow, radiation temperature and other fields.
    19  Optimization method for acoustic temperature measurement signal delay
    LI Shuyuan ZHAO Jian ZHAO Yijun
    2024(1). DOI: 10.11823/j.issn.1674-5795.2024.01.07
    [Abstract](740) [HTML](235) [PDF 1.39 M](901)
    Abstract:
    This research is dedicated to the optimization of time delay processing for acoustic temperature measurement signals within engine combustion chambers, aiming to significantly enhance the precision and reliability of temperature determinations. A novel signal processing methodology is introduced, integrating wavelet packet decomposition transformation recombination with the isolation forest algorithm. This approach promises to refine the quality of temperature data by effectively mitigating noise interference and extracting pivotal information. Firstly, the acoustic temperature probe was thermally calibrated in a wind tunnel to obtain the data in a high temperature airflow environment. Secondly, the wavelet packet decomposition transformation and reorganization method combined with the isolated forest algorithm was used to filter and reconstruct the temperature data to eliminate noise and extract effective information. At the same time, outliers in the reconstructed data was detected to improve data quality and accuracy. The results of thermal calibration wind tunnel experiments show that the data distribution after signal processing is smoother and more symmetrical, the standard deviation is significantly reduced, and the data is more concentrated on the mean, so as to improve the accuracy and stability of temperature measurement. The research provides an effective technical solution for acoustic temperature measurement.
    20  Dynamic characteristics measurement system of thermocouple based on LabVIEW
    KONG Xiangxue ZHAO Jian LI Yajin
    2023(2). DOI: 10.11823/j.issn.1674-5795.2023.02.16
    [Abstract](866) [HTML](350) [PDF 1.03 M](1048)
    Abstract:
    With the development of aviation technology, higher requirements are put forward for the dynamic characteristics of thermocouples. In view of the problem that the existing thermocouple acquisition scheme cannot continuously acquire and obtain the temperature value in real time, a set of thermocouple dynamic characteristics measurement system based on LabVIEW is designed. The working principle, hardware structure and software design of the system are described in detail, and the system is compared with the oscilloscope data collection scheme. The test results show that the system has high reliability and high automation, which effectively improves the working efficiency, and provides support for the performance evaluation of temperature sensors.
    21  Research on response time measuring method of radiant heat flux meter
    REN Jia DONG Lei
    2023(2). DOI: 10.11823/j.issn.1674-5795.2023.02.11
    [Abstract](974) [HTML](311) [PDF 2.63 M](1292)
    Abstract:
    In order to meet requirements of transient heat flux measurement and solve the problem that the response time of radiant heat flux meter cannot be accurately measured, we designed a response time measuring device of radiant heat flux meter, which uses the fast response characteristics of high-power laser to form a heat flux step system, uses a high-speed acquisition system to collect the output of the heat flux meter synchronously. The response curve of the heat flux meter is analyzed and calculated to obtain the response time. A variety of response time testing schemes are compared, and the fast response characteristics of the radiation heat flux meter response time measurement device is verified through experiments. The results show that the fastest response time of the device to measure the radiation heat flux meter is 4.4 ms, which can effectively meet the response time test requirements of large-range and fast response radiation heat flux meter, and promote the development of transient radiant heat flux measurement technology in China.