A fuel tank for an aircraft, including a fuel pumping system which includes a set of hoses, first ends of which are distributed over a lower part of the tank, a manifold to which second ends of the different hoses of the set of hoses are connected as input, an output of the manifold being connected to a fuel pump, a fuel level sensor associated with each hose of the set of hoses and placed in the vicinity of the first end of said hose, and a valve associated with each hose and controlled by a control system which is configured such that when the fuel level sensor associated with this hose detects a low fuel level, the valve is controlled into a closed position, and otherwise the valve is controlled into an open position.
RÉSERVOIR DE CARBURANT POUR AÉRONEF
FUEL TANK FOR AIRCRAFT
KRAFTSTOFFTANK FÜR EIN FLUGZEUG
11.06.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |