A method includes receiving pump cycle location data (144) associated with a fluid power system (102) of an aircraft. The fluid power system (102) includes a plurality of pumps (104), including at least a first pump (106), a second pump (108), and a third pump (110). Based on the pump cycle location data (144) having a first value, the method includes activating the first pump (106) as a primary pump. Based on the pump cycle location data (144) having a second value, the method includes activating the second pump (108) as the primary pump. The method also includes activating the third pump (110) as a secondary pump when the fluid power system (102) is in a multiple-pump operating mode.
DYNAMIC ACTIVATION OF PUMPS OF A FLUID POWER SYSTEM
DYNAMISCHE AKTIVIERUNG VON PUMPEN EINER FLUIDTECHNISCHEN ANLAGE
ACTIVATION DYNAMIQUE DE POMPES D'UN SYSTÈME D'ALIMENTATION DE FLUIDE
13.10.2021
Patent
Elektronische Ressource
Englisch
Pumps for fluid power applications
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