| 基于AMESim的涡扇发动机控制系统综合仿真 |
| |
| 引用本文： | 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[J].航空动力学报,2010,25(12):2816-2820. |
| |
| 作者姓名： | 任新宇 王建礼 赵小龙 |
| |
| 作者单位： | 1. 西北工业大学动力与能源学院,西安,710072
2. 中国航空工业集团公司西安航空动力控制公司,西安,710077 |
| |
| 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.
|
| 关 键 词： | 航空发动机 AMESim 系统仿真 模块化建模方法 |
| 收稿时间： | 4/25/2010 6:13:59 PM |
| 修稿时间： | 8/16/2010 9:01:46 AM |
Simulation of turbofan engine main fuel control system based on AMESim |
| |
| REN Xin-yu,WANG Jian-li and ZHAO Xiao-long.Simulation of turbofan engine main fuel control system based on AMESim[J].Journal of Aerospace Power,2010,25(12):2816-2820. |
| |
| Authors: | REN Xin-yu WANG Jian-li and ZHAO Xiao-long |
| |
| Affiliation: | Northwestern Polytechnical University |
| |
| Abstract: | Based on the AMEsim simulation environment, an turbofan engine control system simulation platform is developed. Used the Modularization modeling method, the system is subdivided into different subsystem, such us sensors, fuel system, electronic controller, actuators and the engine itself. Every module is built, tested and encapsulated into the aero-engine control system module library. Maked use of the module library, the engine system model can be established easily. Taked for instance main fuel control system, described modularity modeling methods. The results show that system model can reflect the complex integration and coupling of subsystem. Combinatorial optimization using system model can improve system capability. |
| |
| Keywords: | aero-engine control system AMESim simulation system simulation |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
|
点击此处可从《航空动力学报》下载全文 |
|
