A actuator arrangement is disclosed in which the high-lift device support that supports and guides movement of a high-lift device, such as a flap, is in axial alignment with a control actuator assembly that controls one or more control surfaces. This allows a single support fairing to be sufficient for covering both the track member and the control actuator assembly and allowing for reduced drag and weight.
ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT
30.11.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT
Europäisches Patentamt | 2023
|Actuator arrangement for a wing assembly of an aircraft
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2024
|Europäisches Patentamt | 2021
|Actuator device for wing assembly of aircraft, wing assembly and aircraft
Europäisches Patentamt | 2023
|