An aircraft (1) includes first and second engines (10, 10A, 10B), one or more aircraft rotors (12, 12P) associated with the first and second engines (10, 10A, 10B), a first epicyclic gearbox (20) having: a) an output operatively connected at least one of the one or more aircraft rotors (12, 12P), and b) an input defined by a sun gear (32) of the first epicyclic gearbox (20); and a second epicyclic gearbox (58) having: a) an output operatively connected to at least one of the one or more aircraft rotors (12, 12P), and b) an input defined by a sun gear (60) of the second epicyclic gearbox (58). Output of the first epicyclic gearbox (20) is defined by the carrier (40). Output of the second epicyclic gearbox (58) is defined by its ring gear (62). A multi-engine aircraft (1) and a method of operating a multi-engine aircraft (1) are also described.


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    Title :

    MULTI-ENGINE AIRCRAFT AND METHOD OF OPERATING A MULTI-ENGINE AIRCRAFT


    Additional title:

    MEHRMOTORIGES FLUGZEUG UND VERFAHREN ZUM BETRIEB EINES MEHRMOTORIGEN FLUGZEUGS
    AÉRONEF MULTIMOTEUR ET PROCÉDÉ D'EXPLOITATION D'UN AÉRONEF MULTIMOTEUR


    Contributors:

    Publication date :

    2024-05-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



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