航空发动机控制软件仿真系统及其生成方法

By constructing an aero-engine control software simulation system and utilizing shared memory to achieve data interaction between modules, the challenges of interface changes and timing matching in closed-loop testing were solved, improving development efficiency and reducing costs, and achieving closed-loop control.

CN115202799BActive Publication Date: 2026-07-17AECC COMML AIRCRAFT ENGINE CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AECC COMML AIRCRAFT ENGINE CO LTD
Filing Date
2021-04-09
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing aero-engine control software simulation systems face challenges in closed-loop testing due to the enormous amount of manual modifications caused by interface changes and difficulties in timing matching, resulting in low development and verification efficiency.

Method used

An aero-engine control software simulation system was designed, including a test case module, an adjustable parameter module, a test model module, a data shared memory, a test case parsing module, a data conversion module, and an engine model module. Data interaction between modules is realized through data shared memory to build a closed-loop test environment.

Benefits of technology

It improves the efficiency of model development and simulation, reduces research and development costs and software maintenance costs, and realizes the automation and closed-loop control of interface configuration.

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Abstract

本发明涉及一种航空发动机控制软件仿真系统及其生成方法。该航空发动机控制软件仿真系统包括测试用例模块、可调参数模块、被测模型模块、数据共享内存、用例解析模块、数据转换模块和发动机模型模块;其中,测试用例模块包含测试用例;可调参数模块包含可调参数;用例解析模块接收测试用例模块发送的测试用例,解析测试用例形成解析结果,配置测试用例生成测试用例配置文件;数据共享内存完成可调参数模块、被测模型模块和数据转换模块之间的数据交互;数据转换模块用于完成发动机模型模块和数据共享内存之间的数据传递。通过本发明提供的方案极大的提高了模型的开发和仿真效率。
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