Production method for producing load-bearing fuselage panels and fuselage panels producible thereby
A manufacturing method and technology of fuselage panels, applied in the direction of fuselage, fuselage bulkhead, fuselage frame, etc., can solve problems such as complexity and large-scale manufacturing
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[0115] FIG. 1 shows a fuselage panel 10 for forming part of a load-bearing fuselage structure 12 and part of the outer wall of a passenger cabin 14 of an aircraft, such as, for example, an aircraft. The fuselage panel 10 is constructed in a sandwich structure or as a sandwich element 16 with an inner shell 18 , an outer shell 20 and a core 22 therebetween.
[0116] The inner shell 18 is formed by an inner panel 24 which serves to form an interior space limitation 26 of the passenger compartment 14 .
[0117] The outer skin 20 is formed by an outer skin 28 for forming a part of the fuselage structure 12 and a part of the outer delimitation of the aircraft fuselage.
[0118] The core 22 is formed by filler panels 30 into which functional elements 32 of the fuselage structure 12 , of the passenger cabin 14 or of other systems of the aircraft are integrated.
[0119] The fuselage panel 10 is therefore basically constructed from three main elements in principle. The outer skin 28...
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