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).
Cryogenic fuel tanks for use in aircraft structures
Kryogene Treibstofftanks zur Verwendung in Flugzeugstrukturen
Réservoirs de carburant cryogène pour utilisation dans structures d'avion
06.05.2020
Patent
Elektronische Ressource
Englisch
Engineering Index Backfile | 1940
|SAE Technical Papers | 1940
|Theoretical Pressure Histories for Cryogenic Fuel Tanks
AIAA | 1967
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