FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Fuselage inner side section 3 makes passenger cabin with inner lining. Fuselage section in horizontal projection is geometrically defined by outer skin first and second sections 6 and 7, the latter facing the former. Said first and second section of outer skin along passenger cabin feature in horizontal projection circular-arc-contour with invariable curvature radius. Inner lining is intended for passenger cabin. Fuselage is formed by sections 2.
EFFECT: improved interchangeability.
16 cl, 14 dwg
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