Numerical investigation of effect of a centrifugal boost impeller on suction performance of an aircraft hydraulic pump

Author:

DONG Hongkang,HE Yongling,WANG Yan,KOU Guiyue

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference38 articles.

1. SAE International. Aerospace-system integration factors that affect hydraulic pump life. Warrendale (PA): Aerospace, A-6C4 Power Sources Committee; 2017 Feb. Report No.: AIR1922B.

2. Modeling and control of a novel elector-hydrostatic actuator with adaptive pump displacement;Wang;Chin J Aeronaut,2020

3. SAE International. Commercial aircraft hydraulic systems. Warrendale (PA): Aerospace, A-6A1 Commercial Aircraft Committee; 2015 Sep. Report No.: Air5005A.

4. Effects of splined shaft bending rigidity on cylinder tilt behaviour for high-speed electrohydrostatic actuator pumps;Zhang;Chin J Aeronaut,2019

5. 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,2018

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