FUEL TANK DIFFUSER

There is provided a fuel system (1) for an aircraft. The fuel system comprises a fuel tank (10) for storing fuel (102) during operation of the aircraft and a diffuser (11) disposed inside the fuel tank (10). The diffuser is configured such that it forms part of a flow path configured to connect a fu...

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Bibliographische Detailangaben
Hauptverfasser:	Peachey, Daniel, Petit, David, Bonte, Eric
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS INVEHICLES ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OFTRANSMISSIONS IN VEHICLES ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GASEXHAUST OR FUEL SUPPLY OF PROPULSION UNITS, IN VEHICLES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AUXILIARY DRIVES FOR VEHICLES AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INSTRUMENTATION OR DASHBOARDS FOR VEHICLES PARACHUTES PERFORMING OPERATIONS TRANSPORTING VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	There is provided a fuel system (1) for an aircraft. The fuel system comprises a fuel tank (10) for storing fuel (102) during operation of the aircraft and a diffuser (11) disposed inside the fuel tank (10). The diffuser is configured such that it forms part of a flow path configured to connect a fuel source to the inside of the fuel tank. The diffuser (11) comprises a wall (111) which at least partially defines an internal space (113) of the diffuser; an opening (13) in the wall (111), which provides access to the internal space; and a blocking component (12a) configured to block the opening (13).