Citation: | Modeling simulation and optimization of oil system based on MATLAB/Simulink[J]. Journal of Aerospace Power, 2017, 32(3): 740-748. doi: 10.13224/j.cnki.jasp.2017.03.028 |
[1] |
Volponi A J.Gas turbine engine health management:past,present,and future trends[J].Journal of Engineering for Gas Turbines and Power,2014,136(5):051201.1-051201.20.
|
[2] |
吴大观.涡轮风扇发动机及其系统的性能研究[M].北京:国防工业出版社,1986.
|
[3] |
Cheng A K.SSME alternate turbopumps axial thrust balance and secondary flow models[R].Sverdrup Technology MSFC Group Report No.322-002-91-153-R01,1992.
|
[4] |
Majumdar A K,Bailey J,Schallhorn P,et al.A generalized fluid system simulation program to model flow distribution in fluid networks[J].AIAA 98-3682,1998.
|
[5] |
李林蔚,高红霞.航空滑油系统设计与性能分析研究现状与进展[J].机电工程技术,2008,37(8):95-98,144.LI Linwei,GAO Hongxia.Development of aeroengine oilsystem design and performance analysis[J].Mechanical and Electrical Engineering Technology,2008,37(8):95-98,144.(in Chinese)
|
[6] |
苏立超,刘振侠,吕亚国.航空发动机润滑系统滑油压力仿真计算[J].科学技术与工程,2012,12(1):97-101,136.SU Lichao,LIU Zhenxia,L Yaguo.Simulation and calculation of aeroengine oil system pressure[J].Science Technology and Engineering,2012,12(1):97-101,136.(in Chinese)
|
[7] |
朱鹏飞,刘振侠,任国哲,等.航空发动机管路系统流动与换热的仿真平台[J].推进技术,2014,35(11):1523-1529.ZHU Pengfei,LIU Zhenxia,REN Guozhe,et al.Simulation platform of aero-engine pipeline system on flow and heat transfer[J].Journal of Propulsion Technology,2014,35(11):1523-1529.(in Chinese)
|
[8] |
刘振侠,黄生勤,吕亚国,等,航空发动机润滑系统通用分析软件开发[J].航空动力学报,2007,22(1):12-17.LIU Zhenxia,HUANG Sengqin,L Yaguo,et al.General analysis software of aeroengine lubrication system design[J].Journal of Aerospace Power,2007,22(1):12-17.(in Chinese)
|
[9] |
郁丽,李国权.节流通风的航空发动机轴承腔腔压计算方法[J].航空动力学报,2012,27(11):2616-2621.YU Li,LI Guoquan.Calculation method of bearing chamber pressure for aero-engine throttling vent lubrication system[J].Journal of Aerospace Power,2012,27(11):2616-2621.(in Chinese)
|
[10] |
刘波,周强,程礼,等.构建航空发动机滑油系统稳态模型[J].推进技术,2005,26(6):556-559.LIU Bo,ZHOU Qiang,CHENG Li,et al.Construction of steady model for engine oil system[J].Journal of Propulsion Technology,2005,26(6):556-559.(in Chinese)
|
[11] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第12册 传动及润滑系统[M].北京:航空工业出版社,2002.
|
[12] |
Chun S M.Network analysis of an engine lubrication system[J].Tribology International,2003,36(8):609-617.
|
[13] |
吴丁毅.直通式蓖齿封严特性的实验研究[J].推进技术,1997,18(3):79-81,97.WU Dingyi.An experimental investigation on seal character of straight-through labyrinth[J].Journal of Propulsion Technology,1997,18(3):79-81,97.(in Chinese)
|
[14] |
杜发青,吉洪湖,帅海山,等,齿形几何参数对直通篦齿封严泄漏特性影响的正交实验[J].航空动力学报,2013,28(4):825-831.DU Faqing,JI Honghu,SHUAI Haishan,et al.Orthogonal experimental of effect of fin geometrical parameters on leakage of straight-through labyrinth seals[J].Journal of Aerospace Power,2013,28(4):825-831.(in Chinese)
|
[15] |
周强,刘波,程礼,等,航空发动机滑油系统稳态模型的算法构造[J].航空计算技术,2005,35(2):98-101.ZHOU Qiang,LIU Bo,CHENG Li,et al.The algorithm construction of aero-engine oil system model[J].Aeronautical Computer Technique,2005,35(2):98-101.(in Chinese)
|
[16] |
吕亚国,刘振侠.航空发动机管壳式燃-滑油散热器换热特性计算[J].航空动力学报,2014,29(12):2830-2835.L Yaguo,LIU Zhenxia.Heat transfer characteristics calculation for aero-engine shell-tube fuel-oil heat exchanger[J].Journal of Aerospace Power,2014,29(12):2830-2835.(in Chinese)
|
[17] |
杨春信,张丽娜,郭晖.发动机滑油散热系统性能研究[J].航空动力学报,2003,18(6):813-818.YANG Chunxin,ZHANG Lina,GUO Hui.Method for predicting the performance of oil cooling system and its application[J].Journal of Aerospace Power,2003,18(6):813-818.(in Chinese)
|
[18] |
张书刚,郭迎清,陆军.基于 GasTurb/MATLAB 的航空发动机部件级模型研究[J].航空动力学报,2012,27(12):2850-2856.ZHANG Shugang,GUO Yingqing,LU Jun.Research on aircraft engine component-level models based on GasTurb/MATLAB[J].Journal of Aerospace Power,2012,27(12):2850-2856.(in Chinese)
|
[19] |
Agte J,Shougarian N,Weck O D.Multistate analysis and optimization of a geared turbofan engine lubrication system[R].AIAA-2012-5637,2012.
|
[20] |
Klingsporn M.Advanced transmission and oil system concepts for modern aero-engines[R].ASME Paper GT2004-53578,2004.
|