A fuel transfer system for an aircraft includes an upper tank, a lower tank, a fuel transfer line connecting the upper tank to the lower tank, an upper fuel transfer line outlet in the lower tank, a lower fuel transfer line outlet in the lower tank, an upper float valve associated with the upper fuel transfer line outlet, and a lower float valve associated with the lower fuel transfer line outlet. The upper fuel transfer line outlet, which is in the lower tank, is in fluid communication with the upper tank. The lower fuel transfer line outlet, which is located in the lower tank, is in fluid communication with the upper tank.
FUEL TRANSFER SYSTEM CONTROLLED BY FLOAT VALVES
DURCH SCHWIMMERVENTILE GESTEUERTES BRENNSTOFFTRANSFERSYSTEM
SYSTÈME DE TRANSFERT DE CARBURANT COMMANDÉ PAR DES VANNES À FLOTTEUR
2019-01-16
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |