一种适用S弯喷管的异形波瓣混合器及其设计方法

By designing a non-circular lobe mixer suitable for S-curve nozzles, the problems of narrow channels and airflow mismatch in traditional mixers were solved, achieving efficient mixing of inner and outer bypass airflows and improving aerodynamic performance.

CN122154105BActive Publication Date: 2026-07-17TAIHANG NATIONAL LABORATORY

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
TAIHANG NATIONAL LABORATORY
Filing Date
2026-05-07
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the prior art, the traditional axisymmetric lobe mixer of the S-bend nozzle forms a narrow channel between the flow channels, resulting in large flow losses, limited mixing effect, and mismatch between the airflow direction and the flow channel, causing additional aerodynamic performance losses.

Method used

A non-circular lobe mixer suitable for S-bend nozzles is designed. By ensuring that the center point of the mixer outlet is consistent with the flow direction of the S-bend nozzle, the peak and trough control curves are generated using the proportional scaling method. The profile is generated using the friction control curve and the sweeping method to ensure that the normal direction of the mixer outlet section is consistent with the nozzle section and that the lobe structure matches the flow channel.

Benefits of technology

It significantly enhances the mixing effect of the inner and outer bypass airflow, improves mixing efficiency, reduces aerodynamic losses caused by airflow deflection, and makes the flow more uniform, thus reducing flow losses.

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Abstract

本发明提供了一种适用S弯喷管的异形波瓣混合器及其设计方法,涉及航空发动机技术领域,所述异形波瓣混合器沿S弯喷管流道变化设置,其出口截面与对应位置S弯喷管截面的法向一致;根据混合器出口处对应的S弯喷管中间截面曲线,以混合器出口中心为中心进行等比缩放,得到限制波峰和波谷位置的两条控制曲线;各波瓣沿周向按相同角度布置,通过波峰引导线和波谷引导线对波瓣型面进行引导,并由进口圆形分段弧线扫掠至出口曲线形成异形波瓣混合器。本发明能够提高内外涵气流掺混效率,降低S弯喷管内气流大角度偏转引起的气动损失。
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