The composition and working principle of an aircraft hydraulic energy system were introduced, the flow and pressure requirements of hydraulic users was analyzed by combining with the normal condition for each phase of flight missions, and the selection design of main components of the pump source was completed. The flow and pressure in line with supply and demand of the hydraulic system under the normal condition was analyzed, for the subsequent design and demonstration test of aircraft hydraulic energy system provides a theoretical reference.
Analysis on the flow requirement of an aircraft hydraulic energy system
2016-10-01
710968 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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