CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE
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United States of America Patent
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Issued Date -
Jan 23, 2025
app pub date -
Oct 2, 2024
filing date -
Oct 2, 2024
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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.
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