FIELD: transport.
SUBSTANCE: invention relates to aircraft fuselage element section and connecting means for connection with adjacent section. Fuselage element includes section with skin and means for connection with adjacent section. Said skin comprises first section at one end. Note here that fuselage section comprises fuselage stiffness lengthwise element. Connecting means comprises connecting element for connection of fuselage section with adjacent section. Connecting means are brought in contact with outer surface of the skin first section. Note here the said lengthwise stiffness element is composed by stringent extending partially along lengthwise axis level with connecting means.
EFFECT: ruled out disturbance of aerodynamics at the level of connector, easier assembly and lower weight, higher stability ay the level of connector.
16 cl, 15 dwg
