An aircraft system is provided that includes a first propulsor, a second propulsor, a drivetrain and an intermittent combustion engine. The first propulsor includes a first propulsor rotor and a first vane array. The second propulsor includes a second propulsor rotor and a second vane array. The drivetrain includes a drive structure and a transmission. An output of the transmission is coupled to the first propulsor rotor and the second propulsor rotor through the drive structure. The intermittent combustion engine is configured to drive rotation of the first propulsor rotor and the second propulsor rotor through the drivetrain.
AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)
SYSTEME DE PROPULSION D'AERONEF AVEC MOTEUR(S) A COMBUSTION INTERMITTENTE
2024-01-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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
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