An aircraft system (20) includes a first propulsor (36A), a second propulsor (36B), a drivetrain and an intermittent combustion engine (66). The first propulsor (36A) includes a first propulsor rotor (42A) and a first vane array (44A). The second propulsor (36B) includes a second propulsor rotor (42B) and a second vane array (44). The drivetrain includes a drive structure (100) and a transmission (106). An output (118) of the transmission (106) is coupled to the first propulsor rotor (42A) and the second propulsor rotor (42B) through the drive structure (100). The intermittent combustion engine (66) is configured to drive rotation of the first propulsor rotor (42A) and the second propulsor rotor (42B) through the drivetrain.
AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
FLUGZEUGANTRIEBSSYSTEM MIT INTERMITTIERENDEM VERBRENNUNGSMOTOR/N
SYSTÈME DE PROPULSION D'AÉRONEF AVEC MOTEUR(S) À COMBUSTION INTERMITTENTE
2024-04-17
Patent
Electronic Resource
English
AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
European Patent Office | 2024
|AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
European Patent Office | 2024
|AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
European Patent Office | 2024
|AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
European Patent Office | 2024
|AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
European Patent Office | 2024
|