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.


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    Title :

    Dual fuel aircraft


    Publication date :

    2020-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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