Abstract: The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems 1-3, 10-12, 22-24, 46-48, in particular of electrical and hydraulic lines, air-conditioning lines, electrical and hydraulic appliances, sanitary and catering equipment or the like, into the at least one shell part and/or the at least one floor grid 13, 41, and assembly of the at least one shell part and of the at least one floor grid 13, 41 into the at least one fuselage section 32.

Abstract: Methods and apparatuses for ensuring the dimensional constancy of multisegment physical structures, in particular aircraft structures, during assembly are disclosed. The method includes setting up a spatially-fixed three-dimensional coordinate system which encloses the subsequent assembled physical structure and introducing a plurality of segments of the physical structure to be assembled into the spatially-fixed three-dimensional coordinate system. The method includes recording the positions of the individual segments and the positions of already assembled groups of segments repeatedly within the spatially-fixed three-dimensional coordinate system during assembly.

Abstract: The invention relates to a method for ensuring the dimensional constancy of multisegment physical structures, in particular aircraft structures, during assembly, having the following steps: a spatially-fixed three-dimensional coordinate system (90) which encloses the subsequent assembled physical structure is set up; a plurality of segments (31, 32, 33) of the physical structure to be assembled are introduced into the spatially-fixed three-dimensional coordinate system (90); the positions of the individual segments (31, 32, 33) and of already assembled groups of segments (31, 32, 33) are recorded repeatedly within the spatially-fixed three-dimensional coordinate system (90) during assembly; and the position of a respective segment (31, 32, 33) or of a respective already assembled group of segments (31, 32, 33) is corrected if a respective record shows that the positions of the respective segment (31, 32, 33) or of the respective already assembled group of segments (31, 32, 33) is outside a tolerance band, whi

Abstract: The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems 1-3, 10-12, 22-24, 46-48, in particular of electrical and hydraulic lines, air-conditioning lines, electrical and hydraulic appliances, sanitary and catering equipment or the like, into the at least one shell part and/or the at least one floor grid 13, 41, and assembly of the at least one shell part and of the at least one floor grid 13, 41 into the at least one fuselage section 32.