一种航空发动机空气系统引气管与孔板匹配设计方法

By establishing the correspondence between pressure ratio and converted flow rate and conducting orifice plate flow characteristic tests, the problem of inaccurate pressure distribution in the matching design of air intake pipe and orifice plate was solved, realizing efficient and accurate design of aero-engine air system and reducing costs.

CN117287303BActive 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
2023-09-25
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the existing technology, the matching design of the air duct and orifice plate of the air system of aero-engine lacks a clear technical route, which leads to the reliance on experience for pressure distribution, which may result in design results that do not meet requirements and increase costs.

Method used

By obtaining the flow characteristic test results of existing air intake pipes, the correspondence between pressure ratio and converted flow rate is established. Flow characteristic tests of orifice plates under different orifice diameters are conducted to obtain the fitting relationship. Combined with input parameters and deviation allowance pressure ratio, the pressure ratio and size of air intake pipes and orifice plates are determined to ensure that the design results meet the requirements.

Benefits of technology

This significantly improved the accuracy of pressure distribution between the air intake tube and the orifice plate, reduced design costs and repetitive work, and ensured the accuracy and efficiency of the design results.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN117287303B_ABST
    Figure CN117287303B_ABST
Patent Text Reader

Abstract

本申请属于航空发动机空气系统领域,为一种航空发动机空气系统引气管与孔板匹配设计方法,通过先根据现有数据建立压比与换算流量之间的对应关系,而后分别进行孔板在不同的孔径下的引气管流量特性试验,获得压比与换算流量之间的拟合关系,再通过定义输入参数、总压比和引气参数偏差预留压比的分配比例,确定引气管的流量需求G1、引气管流量特性为下限的最大流量G2与拟合系数之间的对应关系,而后定义G2≥G1,得到当引气管压比在G2与G1相等时的数值,并进一步得到孔板压比;最后根据孔板压比和引气管压比完成孔板孔径和引气管管径的计算。根据设计输入获得满足条件的最优管路尺寸,提升工作效率,降低了成本。
Need to check novelty before this filing date? Find Prior Art