A first embodiment of a hollow wingtip device that can be selectively releasably connected to the wing of an aircraft is described herein. An interior of the hollow wingtip device comprises a compartment. A second embodiment of a hollow wingtip device is described comprising a compartment in an interior of the hollow wingtip device, an opening configured to provide access to the compartment and a cover for covering the opening. An aircraft comprising the hollow wingtip devices, a wing, and electrical equipment is also provided. Methods for providing a hollow wingtip device, and methods for installing electrical equipment on aircraft are also described.
AIRCRAFT WINGTIP ANTENNA/SENSOR MOUNT
20.06.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |