一种展向压力可控的高速三维内流示踪粒子注入方法

CN119756759BActive Publication Date: 2026-07-17CHINA ACAD OF AEROSPACE AERODYNAMICS

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHINA ACAD OF AEROSPACE AERODYNAMICS
Filing Date
2024-12-24
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Under high-speed inflow conditions, tracer particles are difficult to uniformly enter the inflow model, especially when the angle of attack and sideslip angle are variable, the tracer particles in the leeward area are sparse, which leads to inaccurate measurement of the inflow velocity field.

Method used

A three-dimensional internal flow tracer particle injection device with controllable spanwise pressure is adopted. Through N pressure regulating valves, opening valves and power devices, the pressure inside the particle container is controlled to achieve uniform seeding of tracer particles in the internal flow model. The flow field pressure distribution is calculated by numerical simulation, and the pressure valves are adjusted to ensure uniform particle injection.

Benefits of technology

This method achieves three-dimensional uniform seeding of tracer particles in the internal flow model, improving the accuracy and precision of internal flow velocity field measurement and avoiding interference from particle injection on the flow field.

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Abstract

本发明涉及一种展向压力可控的高速三维内流示踪粒子注入装置,该装置包括N个压力调节阀、开度阀、粒子容器、动力装置,N大于等于3;动力装置连接粒子容器,粒子容器连接开度阀,开度阀并联连接N个压力调节阀,N个压力调节阀沿展向均匀布置在内流模型底部,分别通过内流模型上的连接接口,将示踪粒子均匀播撒进模型内部;其中动力装置通过抽真空降低粒子容器内的压力,使得粒子容器内的真空度符合预设要求;粒子存储在粒子容器内,在粒子容器内的真空度符合预设要求后,开启开度阀和调压阀,使得粒子从粒子注入位置中进入到内流模型的流动空间内实现飞行器内流示踪粒子的三维均匀播撒。
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