全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...

航空活塞发动机使用升限分析

, PP. 1568-1572

Full-Text   Cite this paper   Add to My Lib

Abstract:

通过对某航空活塞增压发动机仿真分析与实验研究,以使用高度上可调节范围作为该类发动机使用升限的一般标准,依据其工作过程和控制规律探讨了使用范围变化的内在原因,提出了与压气机、涡轮参数有关的方程.为提高动力性能,设计了匹配良好的二级增压系统,依据该标准仿真分析了其极限高度与使用升限的可调范围,并给出进一步的改进建议.

References

[1]  尹泽勇, 李上福, 李概奇.无人机动力装置的现状与发展[J]航空发动机, 2007, 33 (1):10-15 Yin Zeyong.Current state and development of the unmanned aerial vehicle powerplants[J].Aero-Engine, 2007, 33(1):10-15(in Chinese)
[2]  BRP-Rotex Gmbh.Maintenance manual for Rotex engine type 914F[M].Astria:BRP-Rotex Gmbh, 2007
[3]  尹泽勇, 李上福, 李概奇.无人机动力装置的现状与发展[J]航空发动机, 2007, 33 (1):10-15 Yin Zeyong.Current state and development of the unmanned aerial vehicle powerplants[J].Aero-Engine, 2007, 33(1):10-15(in Chinese)
[4]  魏名山, 张志, 何永玲.带不同类型调节阀的二级增压系统结构与性能对比[J].内燃机工程, 2009, 30(1):51-55 Wei Mingshan, Zhang Zhi, He Yongling.Configuration and performance comparisons between regulated two-stage turbo-charging systems with different valves[J].Chinese Internal Combustion Engine Engineering, 2009, 30(1):51-55(in Chinese)
[5]  BRP-Rotex Gmbh.Maintenance manual for Rotex engine type 914F[M].Astria:BRP-Rotex Gmbh, 2007
[6]  魏名山, 张志, 何永玲.带不同类型调节阀的二级增压系统结构与性能对比[J].内燃机工程, 2009, 30(1):51-55 Wei Mingshan, Zhang Zhi, He Yongling.Configuration and performance comparisons between regulated two-stage turbo-charging systems with different valves[J].Chinese Internal Combustion Engine Engineering, 2009, 30(1):51-55(in Chinese)
[7]  徐斌, 魏玲, 赵鹏.活塞式航空发动机二级涡轮增压系统匹配分析[J].北京航空航天大学报, 2008, 34(5):551-554 Xu Bin, Wei Ling, Zhao Peng. Match analysis on two-stage turbocharging system of piston aero-engine[J].Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(5):551-554(in Chinese)
[8]  胡延领.基于螺旋桨特性的增压系统匹配研究[D].北京:北京航空航天大学交通科学与工程学院, 2010 Hu Yanling.Research of turbocharging system based on the propeller characteristics[D].Beijing:School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, 2010(in Chinese)
[9]  朱大鑫.涡轮增压与涡轮增压器[M].北京:机械工业出版社, 1992:229-230 Zhu Daxin.Turbocharging and turbo-charger[M].Beijing:China Machine Press, 1992:229-230(in Chinese)
[10]  徐斌, 夏绍军.航空活塞发动机两级增压匹配方法研究[J].航空动力学报, 2012, 3(1):496-500 Xu Bin, Xia Shaojun.Matching of two-stage supercharging aircraft piston engines[J].Journal of Aerospace Power, 2012, 3(1):496-500(in Chinese)
[11]  Qusai Z, Munzer A, Ebaid S Y.Modeling and simulation of a gas turbine engine for power generation[J].Transactions of the ASME, 2006, 128(0):302-311
[12]  Winkler N. Transient simulations of heavy-duty dieselengines with focus on the turbine[R].Sweden:Royal Institute of Technology KTH, 2008
[13]  Renberg U.1D engine simulation of a turbocharged SI engine with CFD computation on components[D].Sweden:Royal Institute of Technology, 2008
[14]  徐斌, 魏玲, 赵鹏.活塞式航空发动机二级涡轮增压系统匹配分析[J].北京航空航天大学报, 2008, 34(5):551-554 Xu Bin, Wei Ling, Zhao Peng. Match analysis on two-stage turbocharging system of piston aero-engine[J].Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(5):551-554(in Chinese)
[15]  胡延领.基于螺旋桨特性的增压系统匹配研究[D].北京:北京航空航天大学交通科学与工程学院, 2010 Hu Yanling.Research of turbocharging system based on the propeller characteristics[D].Beijing:School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, 2010(in Chinese)
[16]  朱大鑫.涡轮增压与涡轮增压器[M].北京:机械工业出版社, 1992:229-230 Zhu Daxin.Turbocharging and turbo-charger[M].Beijing:China Machine Press, 1992:229-230(in Chinese)
[17]  徐斌, 夏绍军.航空活塞发动机两级增压匹配方法研究[J].航空动力学报, 2012, 3(1):496-500 Xu Bin, Xia Shaojun.Matching of two-stage supercharging aircraft piston engines[J].Journal of Aerospace Power, 2012, 3(1):496-500(in Chinese)
[18]  Qusai Z, Munzer A, Ebaid S Y.Modeling and simulation of a gas turbine engine for power generation[J].Transactions of the ASME, 2006, 128(0):302-311
[19]  Winkler N. Transient simulations of heavy-duty dieselengines with focus on the turbine[R].Sweden:Royal Institute of Technology KTH, 2008
[20]  Renberg U.1D engine simulation of a turbocharged SI engine with CFD computation on components[D].Sweden:Royal Institute of Technology, 2008

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133