FUEL SUPPLY APPARATUS FOR AIRCRAFT ENGINE

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 rig...

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Bibliographische Detailangaben
Hauptverfasser:	MORIOKA, Noriko, OYORI, Hitoshi
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS PARACHUTES PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	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.