Churning losses analysis on the thermal-hydraulic model of a high-speed electro-hydrostatic actuator pump

Author:

Zhang Junhui,Li Ying,Xu Bing,Chen Xia,Pan Min

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference25 articles.

1. C, Simulation of a prototype electrically powered integrated actuator for civil aircraft;Crowder;Proc. Inst. Mech. Eng., Part G: J. Aerospace Eng.,1997

2. D. Van Den Bossche, The A380 flight control electrohydrostatic actuators, achievements and lessons learnt, in: Proceedings of 25th International Congress of the Aeronautical Sciences, Hamburg, Germany, 2006, pp. 1–8.

3. Discussion on the Reynolds equation for the slipper bearing modeling in axial piston pumps;Chao;Tribol. Int.,2018

4. Analysis of the cylinder block tilting inertia moment and its effect on the performance of high-speed electro-hydrostatic actuator pumps of aircraft;Zhang;Chin. J. Aeronaut.,2017

5. Spline design for the cylinder block within a high-speed electro-hydrostatic actuator pump of aircraft;Chao;Meccanica,2017

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