首页 | 本学科首页   官方微博 | 高级检索  
     检索      

飞行模拟机的某型涡扇发动机起动模型研究
引用本文:熊海国.飞行模拟机的某型涡扇发动机起动模型研究[J].航空动力学报,2010,25(3).
作者姓名:熊海国
作者单位:哈尔滨工业大学
基金项目:教育部新世纪优秀人才支持计划项目(NCET-04-0325);国家“985”工程资助项目(CDAZ98502211).
摘    要:为了建立适用于飞行模拟机的发动机起动模型,对涡扇类发动机起动过程的建模和仿真方法进行了研究,提出了飞行模拟机起动模型的建模基本原则,以此为指导,基于部件级建模方法建立了主导发动机正常起动动态性能的主要特性模型,并通过构建故障因子建立了典型故障模型,实现了发动机正常起动和起动过程中的故障模拟。正常起动仿真和故障仿真结果与测试数据的对比表明,所建立的正常起动模型正确地反映了发动机在各起动阶段的加速性能,故障模型很好的再现了故障逻辑和故障效应,满足了用于飞行模拟机的发动机起动仿真要求。

关 键 词:计算机应用与仿真  飞行模拟机  部件级建模方法  起动模型  故障模型
收稿时间:2/22/2009 7:20:01 PM

Research on Startup Model of turbofan engine used in a flight simulator
Xiong Hai-Guo.Research on Startup Model of turbofan engine used in a flight simulator[J].Journal of Aerospace Power,2010,25(3).
Authors:Xiong Hai-Guo
Institution:Harbin Institute of Technology
Abstract:In order to establish the aircraft engine startup model used in a flight simulator, the modeling and simulation methods for turbofan engine startup were studied, the basic rules for establishing the startup model were developed, under the guidance of it, the main performance models which dominate the dynamic performance of engine startup in normal working condition were developed based on component modeling method, the typical malfunction models were developed using the designed malfunction factor, the normal engine start-up procedure and malfunctions in the starting process were carried out. The comparisons between the simulation results in normal and fault condition and test data indicate that the normal startup model reflects the accelerating ability of each start-up phase correctly, the malfunction models realize the logic and effects in fault condition, the models developed meet the requirements of flight simulation.
Keywords:computer application  flight simulator  component modeling method  startup model  malfunction model
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》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号