Supersonic airflow micro-channel array generating device

By employing a chuck and rotating rod switching mechanism in the supersonic airflow microchannel array generator, the problem of the inability to adjust the critical cross-sectional area in conventional equipment is solved, enabling flexible airflow parameter control and rapid experimental adjustment.

CN122409129APending Publication Date: 2026-07-17CHANGZHOU UNIV HUAIDE COLLEGE

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
CHANGZHOU UNIV HUAIDE COLLEGE
Filing Date
2026-05-11
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Conventional supersonic airflow generators cannot adjust the critical cross-sectional area, resulting in limited experimental conditions and requiring the replacement of the entire Laval tube to adjust parameters, which is time-consuming and costly.

Method used

A switching mechanism is adopted, including multiple chucks and rotating rods. The switching of throat channels with different diameters is realized by the rotation of the chucks and the positioning mechanism. Combined with the contraction transition channel and the diffusion transition channel, the critical cross-sectional area is adjusted to control the airflow parameters.

Benefits of technology

It enables rapid adjustment of supersonic airflow rate and Mach number to meet different experimental needs and reduces equipment maintenance costs and time.

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Abstract

本申请涉及超声速气流微流道设备技术领域,尤其是涉及一种超声速气流微流道阵列发生设备,包括拉瓦尔管以及连接板,所述连接板上设置有切换不同直径喉部通道的切换机构,所述切换机构包括多个卡盘,多个所述卡盘上开设有不同直径大小的喉部通道,所述喉部通道两端分别连通收缩过渡通道和扩散过渡通道,所述收缩过渡通道和扩散过渡通道分别连通收缩管道和扩散管道。目标卡盘的弧形过渡面与拉瓦尔管的弧形槽对齐时,喉部通道通过收缩过渡通道和扩散过渡通道与收缩段和扩散段形成流线型衔接,通过更换不同直径的喉部通道,可调节临界截面积,从而控制超声速气流的流量和马赫数,满足不同实验需求。
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