Cryogenic fuel tanks for use in aircraft structures

Cryogenic fuels tanks (218, 220) for use in airfoil-shaped aircraft structures (1200) are disclosed herein. An example apparatus disclosed herein an airfoil-shaped structure (1200) disposed outboard of a fuselage of an aircraft (100). The example apparatus also includes a first cryogenic fuel tank (...

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Bibliographische Detailangaben
Hauptverfasser:	Stuhr, Victor K, Sankrithi, Mithra M.K.V, Barmichev, Sergey D
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	Cryogenic fuels tanks (218, 220) for use in airfoil-shaped aircraft structures (1200) are disclosed herein. An example apparatus disclosed herein an airfoil-shaped structure (1200) disposed outboard of a fuselage of an aircraft (100). The example apparatus also includes a first cryogenic fuel tank (118) disposed inside the airfoil-shaped structure (1200).