等离子体激励器温度场数据获取方法、装置、应用及介质

By using fluorescence thermometry and solving linear equations, the problem of incomplete measurement data in existing technologies has been solved, enabling accurate measurement of the two-dimensional and three-dimensional temperature fields on the surface of the insulating medium of the plasma actuator and the air above it, thus improving the actuator control effect.

CN122192552BActive Publication Date: 2026-07-17LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
Filing Date
2026-05-14
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies struggle to accurately obtain the two-dimensional temperature field of the insulating medium surface of the plasma actuator and the air above the actuator using a single method, resulting in incomplete measurement data.

Method used

Fluorescent thermometry is used to acquire fluorescence images by applying a temperature-sensitive coating layer on the surface of the heat-conducting sheet. The two-dimensional surface temperature field is calculated by combining the calibration relationship between light intensity and temperature. The two-dimensional heat source temperature field is then reconstructed by solving a system of linear equations and the least squares method. Finally, the three-dimensional heat source temperature field is reconstructed.

Benefits of technology

It achieves complete temperature field data for the exciter plasma, the surface of the insulating medium, and the air above, and can accurately obtain the temperature field of the two-dimensional surface and the three-dimensional heat source, supporting the development of aircraft.

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Abstract

本申请涉及温度测量技术领域,尤其涉及一种等离子体激励器温度场数据获取方法、装置、应用及介质,包括以下步骤:基于荧光测温技术,获取处于激励器上方的导热片的荧光图像;基于所述荧光图像光强与温度之间的标定关系、以及所述荧光图像,确定导热片所在平面的二维表面温度场;基于所述导热片所在平面的二维表面温度场,确定其对应平面的二维热源温度场。本申请可以兼顾测量激励器等离子体、绝缘介质表面、上方空气这三者的温度场,保证了数据完整性,有效解决了本领域现有技术方案测量数据不完整的问题,重构出激励器等离子体及其上方空气的三维温度场,为推动飞行器的发展提供了重要技术支撑。
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