The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first tank (114) and the injector (74). The second circuit (108) includes a second tank. The fuel is directed from the first tank (114) to the injector (74) during a first mode through the first circuit (106) and independent of the second circuit (108). The fuel is directed from the second tank to the injector (74) during a second mode through the second circuit (108) and independent of the first circuit (106).
AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK
FLUGZEUGKRAFTSTOFFSYSTEM MIT ABNEHMBAREM KRAFTSTOFFTANK
SYSTÈME DE CARBURANT D'AÉRONEF AVEC RÉSERVOIR DE CARBURANT AMOVIBLE
2024-09-18
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |