A fuel manifold adapted to communicate with at least one fuel tank of an aircraft is presented. The manifold defines an enclosure adapted to be filled with fuel and to have an internal pressure P1 higher than the internal pressure P2 of the fuel tank. The enclosure includes at least one ceiling and at least one side wall provided with overflow holes adapted to communicate with the fuel tank. The manifold includes a mechanism for discharging an air pocket, trapped between the ceiling and the level of the overflow holes, to the fuel tank.
COLLECTEUR DE CARBURANT POUR RESERVOIR D'UN AERONEF
FUEL MANIFOLD FOR AN AIRCRAFT TANK
KRAFTSTOFFVERTEILER FÜR TANK EINES LUFTFAHRZEUGS
2024-04-24
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |