Cabin lining element for an aircraft cabin and rib for an aircraft fuselage structure
AssigneeAirbus Operations GmbH
InventorsStephan RISSE, Rainer MÜLLER
Life of this patent
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Abstract
A cabin lining element for an aircraft cabin which is arranged in the interior of an aircraft fuselage structure, having a fuselage structure side and a cabin side. The cabin lining element comprises an electrically contactable heating lacquer layer at least in regions on its fuselage structure side. A rib is provided for an aircraft fuselage structure, having at least one foot portion on the outer skin facing side and a cabin facing side head portion. The rib comprises an electrically contactable heating lacquer layer at least in regions on a side of the head portion facing the cabin.
Claims9
A rib for an aircraft fuselage structure, comprising
- at least one foot portion on an outer skin facing side, and
- one cabin facing side head portion,
- wherein the rib comprises an electrically contactable heating lacquer layer at least in regions on a cabin-facing side of the head portion.
Dependencies are inferred from the claim text.