FIELD: transport.
SUBSTANCE: invention relates to fuselage, aircraft and space ship. Proposed fuselage comprises inner skin structure consisting of top inner skin, bottom inner skin and window lining. Top inner skin is separated from bottom inner skin in some sections to form zone of glasing. Window lining is arranged in glasing zone and comprises glasing unit including lattice structure to absorb loads originating in fuselage. Fuselage comprises outer skin structure consisting of top outer skin jointed with top inner skin, and bottom outer skin jointed with bottom inner skin. Top outer skin separated from bottom skin in some sections to form zone of glasing. Glasing unit comprises two separate glasses to be set flush with appropriate inner and outer skins to form lattice structure.
EFFECT: lower weight and overall dimensions.
8 cl, 8 dwg
