The present invention provides a fuselage (10) for an aircraft (1) or spacecraft, the fuselage (10) comprising: a first fuselage section (11) having a support structure with a load bearing outer skin (12); and a second fuselage section (13) having a non-load bearing outer skin (14) and a space frame structure (15) for supporting the non-load bearing outer skin (14), wherein the non-load bearing outer skin (14) comprises at least one skin area (16), which is configured to be openable for venting a compartment, which is at least sectionwise enclosed by the at least one skin area (16). Further the present invention provides an aircraft (1) or spacecraft comprising such a fuselage (10).
FUSELAGE FOR AN AIRCRAFT OR SPACECRAFT, AND AIRCRAFT OR SPACECRAFT
RUMPF FÜR EIN LUFT- ODER RAUMFAHRZEUG SOWIE LUFT- ODER RAUMFAHRZEUG
FUSELAGE POUR AÉRONEF OU ENGIN SPATIAL, ET AÉRONEF OU ENGIN SPATIAL
27.08.2025
Patent
Elektronische Ressource
Englisch
AN AIRCRAFT OR SPACECRAFT FUSELAGE WITH A STRUCTURAL JUNCTION
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