AN AIRCRAFT FUSELAGE SECTION

The invention provides an aircraft section comprising a first fuel storage tank and a second fuel storage tank arranged in a caudal tandem configuration. More in particular, the invention refers to an arrangement of said first and second tanks where the corresponding casings housing the conduits con...

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Bibliographische Detailangaben
Hauptverfasser:	BALLESTERO MÉNDEZ, Jorge, JIMÉNEZ RODRÍGUEZ, César Julián, CERNADA MORALES, Daniel, COLMENAREJO MATELLANO, Nuria, GÓMEZ VIZCAÍNO, Raúl José, FERNÁNDEZ RAMÍREZ, Ana
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention provides an aircraft section comprising a first fuel storage tank and a second fuel storage tank arranged in a caudal tandem configuration. More in particular, the invention refers to an arrangement of said first and second tanks where the corresponding casings housing the conduits configured for distribution of fuel to and from inside the tanks are arranged in a common section of the fuselage and spaced between them.