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

涡扇发动机加减速控制规律设计的功率提取法
引用本文:陈玉春,徐思远,刘振德,屠秋野,于守志.涡扇发动机加减速控制规律设计的功率提取法[J].航空动力学报,2009,24(4):867-874.
作者姓名:陈玉春  徐思远  刘振德  屠秋野  于守志
作者单位:1.西北工业大学 动力与能源学院, 西安 710072
摘    要:为了简单、快速和准确地设计双轴涡扇发动机加、减速控制规律,提出了一种加、减速控制规律设计的新方法——功率提取法:在发动机稳态特性计算模型的基础上,分别从高、低压转子提取额外功率,使得高压压气机工作点(线)沿等换算转速线移动,并保证低压转子转速满足预定的要求,在同时考虑风扇和压气机喘振裕度限制、涡轮进口总温限制以及燃烧室熄火边界的条件下,利用适当的描述形式,可以快速而准确地获得最优双轴涡扇发动机加、减速控制规律.对某型涡扇发动机加速控制规律的改进设计结果表明,提出的加、减速控制规律的设计方法具有直观、快速、准确而有效的优点. 

关 键 词:加、减速特性    加、减速控制规律    涡扇发动机    功率提取法    优化设计
收稿时间:2008/3/18 0:00:00
修稿时间:1/7/2009 4:10:17 PM

Power extraction method for acceleration and deceleration control law design of turbofan engine
CHEN Yu-chun,XU Si-yuan,LIU Zhen-de,TU Qiu-ye and YU Shou-zhi.Power extraction method for acceleration and deceleration control law design of turbofan engine[J].Journal of Aerospace Power,2009,24(4):867-874.
Authors:CHEN Yu-chun  XU Si-yuan  LIU Zhen-de  TU Qiu-ye and YU Shou-zhi
Institution:1.School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China2.The 3rd academy of China Aerospace Science and Industry Corporation, Beijing 100074, China
Abstract:A new and effective method - power extraction method (PEM), which is a simple, rapid and accurate tool of turbofan engine for acceleration and deceleration control law design is proposed in this paper. Based on the steady-state performance computing model, virtual power extractions of fan shaft and compressor shaft were introduced to make the steady-state operating points (line) move from the normal operating points (line) at the constant corrected line of compressor, and the speeds of fan shaft and compressor shaft were maintained at given values. Taking surge margin limit of compressor and fan, total temperature limit of turbine inlet and the flameout limit of combustor into account, using appropriate form to describe the acceleration and deceleration control law, and combined with the experiences of research and the development of turbine engines, the acceleration and deceleration control law of turbofan was designed rapidly and accurately. The computing results of the improved acceleration control law of some turbofan engine indicate that the VPEM is accurate and effective.
Keywords:acceleration and deceleration characteristics  acceleration and deceleration control law  aerospace propulsion system  turbofan engine  power extraction method (PEM)  design optimization
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