一种发动机腔压测试位置高可靠性确定方法

By determining the location of the cavity pressure measurement point through three-dimensional numerical simulation and flow field analysis, the problem of large uncertainty in pressure measurement points in traditional methods is solved, and more accurate axial force calculation is achieved.

CN121595208BActive Publication Date: 2026-07-17AECC SHENYANG ENGINE RES INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AECC SHENYANG ENGINE RES INST
Filing Date
2025-11-18
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Traditional cavity pressure testing methods fail to effectively constrain the location of pressure measurement points, resulting in large uncertainties in pressure measurement and affecting the accuracy of axial force calculation.

Method used

The axial force on the rotor wall and the geometric dimensions of the rotating disk cavity are determined by three-dimensional numerical simulation. The axial projected area is calculated, the characteristic pressure value of the disk cavity is extracted, and the location of the cavity pressure measurement point is determined. CFX is used for flow field simulation and isosurface analysis, and a distance threshold is set to determine the location of the measurement point.

Benefits of technology

This improves the accuracy of the cavity pressure measurement point location and the reliability of axial force calculation, ensuring the accuracy of pressure measurement and enhancing the precision of axial force conversion.

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Abstract

本申请属于发动机测试领域,特别涉及一种发动机腔压测试位置高可靠性确定方法,提取三维仿真结果中的转子壁面轴向力和旋转盘腔的几何尺寸;根据转子壁面轴向力和旋转盘腔的几何尺寸计算转子壁面的轴向投影面积;根据转子壁面的轴向投影面积计算旋转盘腔的盘腔特征压力值;根据盘腔特征压力值进行盘腔压力数值仿真,提取特征压力值,根据特征压力值确定腔压测点位置。基于盘腔压力数值仿真,实现了发动机与轴向力相关腔压测点位置的确定。考虑了发动机盘腔的形貌结构不规则和发动机转子的高速旋转引起的旋转盘腔内的压力分布不均的情况,由此确定的测点位置更真实,更准确。通过提升盘腔压力测试的准确度,会使换算得到的轴向力更准确。
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