An aircraft having an aircraft fuselage that has an outer skin includes an air sucking fuselage component with an outer surface that is perforated at least in some regions, and a suction profile body. The suction profile body is arranged on the outer skin, forms a local bulge in the outer skin, and further includes a suction opening that is arranged at a location at which there is the lowest pressure, for example at a position furthest away from the outer skin. The suction opening is connected to a suction connection of the air sucking fuselage component. In this way laminarization of the flow at the air sucking fuselage component may take place without the use of active air conveying devices.
Aircraft having an aircraft fuselage and an air sucking fuselage component
2017-04-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft fuselage section, aircraft fuselage and aircraft
European Patent Office | 2023
|Fuselage component for an aircraft, method for producing a fuselage component, and aircraft
European Patent Office | 2023
|