A first embodiment of a hollow dorsal fin (200) that can be selectively releasably connected to the fuselage (120) of an aircraft (100) is described herein. An interior (210) of the hollow dorsal fin (200) comprises a compartment (250). A second embodiment of a hollow dorsal fin (300) is described comprising a compartment (350) in an interior of the hollow dorsal fin (300), an opening (360) configured to provide access to the compartment (350) and a cover (370) for covering the opening (360). An aircraft (100) comprising the hollow dorsal fin (200, 300), a fuselage(120), and electrical equipment (290) is also provided. Methods for providing a hollow dorsal fin (200, 300), and methods for installing electrical equipment (290) on aircraft (100) are also described.
REMOVABLE HOLLOW DORSAL FIN
ABNEHMBARE HOHLE DORSALE RIPPE
AILETTE DORSALE CREUSE AMOVIBLE
2024-06-19
Patent
Electronic Resource
English