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
2025-06-11
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |