An aircraft with a fuselage that comprises at least one hollow beam element, wherein the at least one hollow beam element accommodates at least one hollow duct element that comprises a tubular duct element wall, and wherein at least one protective spacer is arranged between the tubular duct element wall and the at least one hollow beam element such that free space is available between the tubular duct element wall and the at least one hollow beam element.
AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
2018-09-27
Patent
Electronic Resource
English
Aircraft with a fuselage that comprises at least one hollow beam element
European Patent Office | 2022
|AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
European Patent Office | 2020
AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
European Patent Office | 2018
|AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
European Patent Office | 2021
|ROTARY WING AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE STRUCTURAL STIFFENED PANEL
European Patent Office | 2018
|