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
2023-11-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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