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
2020-05-06
Patent
Electronic Resource
English
Engineering Index Backfile | 1940
|SAE Technical Papers | 1940
|Theoretical Pressure Histories for Cryogenic Fuel Tanks
AIAA | 1967
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