FUEL SYSTEM FOR AN AIRCRAFT COMPRISING A FUEL MIXING DEVICE

The invention relates to a fuel system for an aircraft (1) comprising at least one wing tank (5a) having at least one manifold (7), a transfer system, able to supply the manifold (7) with fuel, and a filling system, able to introduce fuel into the fuel system from an external source of fuel, compris...

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Bibliographische Detailangaben
1. Verfasser:	VOZY, Thibaut
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	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 HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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