一种叶片叶根变厚度的压气机叶轮及涡轮增压器

By designing the blade root thickness to be distributed in a "hump" shape along the blade root length, the problem of balancing mass, inertia, and frequency in blade thickness distribution was solved, achieving reduced blade mass, lower inertia, and increased stiffness, thus avoiding high-cycle fatigue failure.

CN120969248BActive Publication Date: 2026-07-17WUXI WEIFU HIGH TECH CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
WUXI WEIFU HIGH TECH CO LTD
Filing Date
2025-09-12
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

The thickness distribution of existing compressor impellers along the blade root length direction makes it difficult to simultaneously improve the blade's natural frequency, reduce mass, and decrease rotational inertia.

Method used

The design of the leaf root thickness shows a "hump" distribution along the length of the leaf root, with the front section of the leaf being the thickest and the rear section thinning rapidly and then slowly. Combined with linear interpolation extrapolation, it is calculated that the thickness of the front section is more than 1.2 times that of the rear section.

Benefits of technology

This reduces blade mass and moment of inertia, improves blade structural stiffness and natural frequency, avoids high-cycle fatigue failure, and reduces centrifugal load.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN120969248B_ABST
    Figure CN120969248B_ABST
Patent Text Reader

Abstract

本发明涉及一种叶片叶根变厚度的压气机叶轮及涡轮增压器。本发明压气机叶轮的主叶片的叶根厚度沿叶根长度坐标轴的变化曲线呈驼峰状,按变化曲线在100%叶根长度处的叶根后端厚度值,结合变化曲线在70%叶根长度处的叶根后部厚度值,进行线性插值外推算得在30%叶根长度处的基准厚度,变化曲线在30%叶根长度处的叶根前部厚度值,至少为基准厚度的1.2倍。使得自叶片侧面前竖边起,叶片前段的叶根厚度逐渐增加至最大值,接近叶片后段时急剧减薄,叶片后段的叶根厚度在叶片前段叶根厚度急剧减薄的基础上改呈缓慢减薄直至叶片侧面后竖边,该叶根厚度分布方式既能减轻叶片及叶轮质量、减小离心载荷和转动惯量,又能保证较高的叶片振动固有频率。
Need to check novelty before this filing date? Find Prior Art