An aircraft (101) comprising: one or more main engines (104a, 104b); a first fuel in a first fuel tank (111a) configured to be fed towards at least one of the one or more main engines through a first fuel line; and a second fuel different to the first fuel in a second fuel tank (111b) configured to be fed towards at least one of the one or more main engines through a second fuel line; the first fuel being anhydrous ammonia and the second fuel being a fuel other than anhydrous ammonia.
Dual fuel aircraft
2020-12-02
Patent
Electronic Resource
English
Avgas/Ethanol Dual-Fuel Aircraft Engine/Conversion
SAE Technical Papers | 1997
|Avgas/Ethanol Dual-Fuel Aircraft Engine/Conversion
British Library Conference Proceedings | 1997
|