ACTUATOR FOR AVIATION APPLICATIONS
ACTUATOR FOR AVIATION APPLICATIONS
- New search for: HAAR JAN
- New search for: ARNOLD UWE
- New search for: MEUNIER MARTIN
- New search for: WINTJEN CARSTEN
- New search for: MÜLLER MATTHIAS
- New search for: PFLÜGER WERNER
- New search for: HAAR JAN
- New search for: ARNOLD UWE
- New search for: MEUNIER MARTIN
- New search for: WINTJEN CARSTEN
- New search for: MÜLLER MATTHIAS
- New search for: PFLÜGER WERNER
An actuator for aviation applications, in particular for adjusting rotor blades in a helicopter, may include an electromechanical drive assembly connected to an output drive via a downstream transmission, where the drive assembly is divided into sub-drives that can be operated independently, and where at least two sub-drives are spatially separated from one another in that the transmission is placed between these sub-drives. The transmission may include at least two harmonic gearings coupled to one another by at least one first coupling element, where a first harmonic gearing is located inside a non-rotating first housing, where a second harmonic gearing is located inside a rotating second housing, and where the second housing is connected to the output drive.
Document information
ACTUATOR FOR AVIATION APPLICATIONS
2023-06-29
Patent
Electronic Resource
English
| IPC: | B64C AEROPLANES , Flugzeuge |