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US 2008/0185478 A1Published application
Line system for an aircraft
AssigneeAirbus Deutschland 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.
Claims8
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,
- said line system comprising 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.
Dependencies are inferred from the claim text.