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US 8,128,030 B2Granted
Line system for an aircraft
AssigneeAirbus Operations GmbH
InventorHeiko Dannenberg
Life of this patent
Estimating the term…
Abstract
A line system for an aircraft, in particular an airplane, having multiple assemblies, in particular multiple fuselage sections of a fuselage cell and multiple wing shells, the line system including multiple lines for transmitting power and/or information, wherein the lines are integrated on and/or in a support layer, the support layer being situated on and/or in the shell-shaped assemblies.
Claims7
A structural assembly for an aircraft comprising:
- at least first and second aircraft fuselage sections constructed to be joined to form a larger aircraft assembly;
- a support layer integrally constructed on a surface facing an interior of the aircraft of said at least first and second fuselage sections;
- a line system comprising multiple paths for transmitting at least one of power and information, said line system integrally constructed on or in said support layer;
- and
- couplings constructed in said at least first and second aircraft fuselage sections connected to said multiple paths, to connect the line system of said at least first and second fuselage sections, when said at least first and second fuselage sections are joined.
2 more elements
Dependencies are inferred from the claim text.