[1] TODESCHI M.A380 flight control actuation lessons learned on EHAs design[C]//Proceedings of the International Conference on Recent Advances in Aerospace Actuation Systems and Components,2007:21-26.
[2] TAKEBAYASHI W,HARA Y.Thermal design tool for EHA[C]//Proceedings of the International Conference on Recent Advances in Aerospace Actuation Systems and Components,2004:15-19.
[3] LI J,ZHANG X,YIN Y B.Dynamic temperature simulation of an accumulator in aircraft hydraulic systems[C]//2011 International Conference on Fluid Power and Mechatronics (FPM).Piscataway,NJ:IEEE Press,2011:653-657.
[4] STADLBAUER K,POLTSCHAK F,RAFETSEDER D,et al.A spice-based lumped parameter thermal model with geometrically distributed elements for electro-hydraulic actuators[C]//2012 International Symposium on Power Electronics,Electrical Dri-ves,Automation and Motion(SPEEDAM).Piscataway,NJ:IEEE Press,2012:511-516.
[5] LI C G,JIAO Z X.Calculation method for thermal-hydraulic system simulation[J].Journal of Heat Transfer,2008,130(8):084503.
[6] SCOTT T,UPHOLD J.Thermal modeling of power steering system performance[C]//SAE World Congress & Exhibition,2008:1039-1044.
[7] LANA E D, DE NEGRI V J.A new evaluation method for hydraulic gear pump efficiency through temperature measurements[C]//SAE 2006 Commercial Vehicle Engineering Congress & Exhibition,2006:3503.
[8] LI J,XU J L,ZHANG X,et al.An estimation method of the fluid temperature for commercial aircraft hydraulic systems[C]//2010 International Conference on Mechanic Automation and Control Engineering (MACE).Piscataway,NJ:IEEE Press,2010:2962-2965.
[9] 卢宁,付永领,孙新学.基于AMEsim的双压力柱塞泵的数字建模与热分析[J].北京航空航天大学学报,2006,32(9):1054-1058.LU N,FU Y L,SUN X X.Digital modeling and thermal analysis of double pressure piston pump based on AMEsim[J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(9):1054-1058(in Chinese).
[10] 李永林,徐浩军,曹克强,等.航空柱塞泵全工况效率分析及热力学建模[J].北京航空航天大学学报,2010,36(12):1470-1472.LI Y L,XU H J,CAO K Q,et al.Efficiency analysis and thermodynamic modeling of aircraft piston pump in all conditions[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(12):1470-1472(in Chinese).
[11] NAVARRO R.Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft:NASA/TM-97-206224[R].Washington,D.C.:NASA,1997.
[12] ANDERSSON J,KRUS P,NILSSON K,et al.Modelling and simulation of heat generation in electro-hydrostatic actuation systems[C]//Proceedings of the 4th JHPS International Symposium on Fluid Power,1999:537-542.
[13] JOHANSSON B,ANDERSSON J,KRUS P.Thermal modelling of an electro-hydrostatic actuation system[C]//Proceedings of the International Conference on Recent Advances in Aerospace Actuation Systems and Components,2001:48-53.
[14] ENGELHARDT J.Thermal simulation of an aircraft fluid power system with hydraulic-electrical power conversion units[C]//Proceedings of the 1st FPNI-PhD Symposium,2000:435-448.
[15] LI K,LV Z,LU K,et al.Thermal-hydraulic modeling and simulation of piston pump in electro-hydrostatic actuator system[C]//2015 International Conference on Fluid Power and Mechatronics (FPM).Piscataway,NJ:IEEE Press,2015:1097-1101.
[16] 盛敬超.液压流体力学[M].北京:机械工业出版社,1980.SHENG J C.Hydraulic fluid mechanics[M].Beijing:China Machine Press,1980(in Chinese). |