Aircraft hydraulic pump control system

Details Aircraft hydraulic pump control system Aircraft hydraulic pump control system

F - Mech Eng,Light,Heat,Weapons

04

B

F04B 49/06 (2006.01) F04B 1/32 (2006.01) F04B 17/03 (2006.01)

Patent

CA 2213457

A control system for an aircraft's electrically driven hydraulic pump. An electronic motor controller having closed loop feedback is utilized to directly control the prime mover speed in response to pump loading.

Cette invention concerne un système de commande de pompe hydraulique d'avion entraînée par un moteur électrique. Un dispositif électronique de commande de moteur électrique comportant un asservissement en boucle fermée permet de régler directement la vitesse du moteur primaire en fonction du pompage effectué par ladite pompe.

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