基于AMESim的涡扇发动机控制系统 综合仿真

任新宇; 王建礼; 赵小龙

基于AMESim的涡扇发动机控制系统综合仿真

1.
西北工业大学动力与能源学院,西安 71007
2.
中国航空工业集团公司西安航空动力控制公司,西安 710077

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出版历程
- 收稿日期: 2010-04-25
- 修回日期: 2010-08-16
- 刊出日期: 2010-12-28

Simulation of turbofan engine main fuel control system based on AMESim

1.
School of Power and Energy, Northwestern Polytechnical University,Xian 71007
2.
Xian Aero-engine Controls Company, Aviation Industry Corporation of China,Xian 710077,China

摘要

摘要: 以AMESim为平台,采用模块化的设计方法,分别建立航空发动机、传感器、燃油系统、电子控制器和执行机构数学模型.将模块封装打包建立涡扇发动机控制系统模型库,并将之组成为完整的发动机及调节器系统综合仿真平台.以主燃油控制系统为例,介绍了各仿真模块的建立过程,仿真结果表明,系统模型能反映各子系统之间的复杂集成和耦合关系,利用系统模型仿真进行组合优化能够有效提高系统性能.
- 航空发动机 /
- 控制系统 /
- AMESim仿真 /
- 系统仿真 /
- 模块化建模方法
Abstract: Based on the AMESim simulation environment,a turbofan engine control system simulation platform was developed.Using the modularization modeling method,the system was subdivided into different subsystems,such us sensors,fuel system,electronic controller,actuators and the engine itself.Every module was built,tested and encapsulated into the aero-engine control system module library.With the module library,the engine system model could be established easily.Taking main fuel control system,for example,the modularity modeling methods was described.The results show that system model can reflect the complex integration and coupling of subsystem.Combinatorial optimization using system model can improve the system capability.
- aero-engine /
- control system /
- AMESim simulation /
- system simulation /

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参考文献(12)

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