一种模拟整机环境的联合压缩系统试验器设计方法

By using a combined compression system tester design method that simulates the overall machine environment, the problem of lack of systematic planning in compressor tester design is solved, achieving efficient and stable tester design and improving design and development efficiency.

CN121936056BActive 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
2026-03-30
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

The existing compressor test equipment design and development process lacks a systematic project development plan, resulting in limited testing capabilities, high design difficulty, long cycle time, and low efficiency.

Method used

The design method of a combined compression system tester that simulates the whole machine environment is adopted. By determining functional requirements, key performance indicators, structural design and material selection, the intake, exhaust and transmission systems are optimized, a clear process route is provided, the design difficulty is reduced and the cycle is shortened.

Benefits of technology

It improved the design and development efficiency of compressor testers, reduced the difficulty of structural design, shortened the demonstration and design cycle of technical solutions, and realized a tester design that is fully functional, structurally sound, and stable in operation.

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Abstract

本申请提供了一种模拟整机环境的联合压缩系统试验器设计方法,属于航空发动机试验技术领域,其包括:确定用于压缩系统试验的试验器的功能需求;基于所述试验器的功能需求确定所述试验器的关键性能指标;根据所述试验器的功能需求进行试验器的结构设计,确定试验器中进气系统、排气系统、传动系统、动力系统的结构形式;根据试验器的关键性能指标确定试验器中进气系统、排气系统的材料及加工工艺;对所述试验器中的进气系统、排气系统以及传动系统、动力系统进行优化。本申请的模拟整机环境的联合压缩系统试验器设计方法可以降低试验器结构设计难度,缩短技术路线、方案的论证、设计周期,提高设计、开发效率。
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