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Abstract
The axial piston pump for aircraft hydraulics systems and other high pressure hydraulic system applications is presented. This paper discusses the pump’s pressure pulsation and the fundamental frequency. Pressure pulsation associated with single piston failure is explained in relation to its fundamental frequency. A predictive approach in maintenance and pump sub system health monitoring is proposed, using numerical modelling and applicable software.
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Details
1 The Boeing Company, Philadelphia, USA
2 Faculty of Mechanical Engineering, Computer Science and Electrical Engineering, University of Mostar, B&H
3 MSc, Airbus DS GmbH, Germany
4 Faculty of Mechanical Engineering, University of Sarajevo, B&H