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.
MULTI-ENGINE AIRCRAFT AND METHOD OF OPERATING A MULTI-ENGINE AIRCRAFT
MEHRMOTORIGES FLUGZEUG UND VERFAHREN ZUM BETRIEB EINES MEHRMOTORIGEN FLUGZEUGS
AÉRONEF MULTIMOTEUR ET PROCÉDÉ D'EXPLOITATION D'UN AÉRONEF MULTIMOTEUR
2024-05-15
Patent
Electronic Resource
English