一种飞行器风洞试验半模型姿态角调平装置及应用

By using a positioning base plate and a distance measuring device, the problem of difficulty in measuring the attitude angle of a half-model was solved, and rapid and high-precision attitude angle adjustment and measurement were achieved. This method is suitable for half-models of the upper wall panel of a wind tunnel test section and has good prospects for engineering applications.

CN122149799BActive Publication Date: 2026-07-17INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
Filing Date
2026-05-09
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In wind tunnel testing, when the half-model is mounted on the upper wall, it is difficult to measure the attitude angle. Existing inclinometers and optical methods cannot meet the high-precision requirements, and the calibration cycle is long and the operation is complicated.

Method used

The system employs a positioning base plate and a distance measuring device, including a first connecting plate, a second connecting plate, and a distance measuring device. By measuring the distance between the second connecting plate and the leveling plane of the half-model, the attitude angle can be quickly adjusted and measured with high precision.

Benefits of technology

It achieves a wide range of measurement of attitude angles of half-models with high accuracy and simple operation, meeting the high efficiency and high precision requirements of the test site and has good engineering application value.

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Abstract

本发明公开了一种飞行器风洞试验半模型姿态角调平装置及应用,属于实验空气动力学测量领域,目的在于解决在对风洞试验段上壁板的半模型姿态角调节过程中,现有技术通常采用激光或陀螺仪进行测量,测量过程繁琐,校准周期长,检查和调整费时费力的问题。该调平装置包括定位基板、距离测定装置、用于安装在风洞的试验段上壁板上的半模型,所述定位基板包括第一连接板、第二连接板,所述第一连接板用于与试验段上壁板相连,所述第二连接板沿竖直方向布置,所述第一连接板与第二连接板垂直相连。本申请能够适用于飞行器风洞试验中安装于风洞试验段上壁板的半模型姿态角测量及快速调平,操作简单,速度快、效率高,具有极高的工业应用价值。
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