Two systems of a first pump unit (7a) and a third pump unit (7c) that supply fuel of a fuselage fuel tank (3a), and a second pump unit (7b) and a fourth pump unit (7d) that supply fuel of fuel tanks (3b, 3c) in both right and left wings are provided corresponding to a left-wing engine (5a) and a right-wing engine (5b), respectively. A supply source of the fuel to be supplied to the left-wing engine (5a) or the right-wing engine (5b) is switched by switching of the pump unit to be turned on.
FUEL SUPPLY APPARATUS FOR AIRCRAFT ENGINE
TREIBSTOFFVERSORGUNGSVORRICHTUNG FÜR EIN FLUGZEUGTRIEBWERK
DISPOSITIF D'ALIMENTATION EN COMBUSTIBLE POUR MOTEUR D'AÉRONEF
08.01.2020
Patent
Elektronische Ressource
Englisch
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