CPC B32B 27/12 (2013.01) [B32B 3/12 (2013.01); B32B 5/18 (2013.01); B32B 5/24 (2013.01); B32B 7/14 (2013.01); B32B 27/06 (2013.01); B32B 37/1207 (2013.01); B64D 11/00 (2013.01); C09J 5/00 (2013.01); C09J 9/00 (2013.01); C09J 163/00 (2013.01); C09J 179/08 (2013.01); B32B 2037/1215 (2013.01); B32B 2255/10 (2013.01); B32B 2262/0269 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2307/3065 (2013.01); B32B 2451/00 (2013.01); B32B 2605/003 (2013.01); B32B 2605/18 (2013.01); C09J 2463/00 (2013.01); C09J 2479/08 (2013.01)] | 6 Claims |
1. An interior member for an aircraft, comprising:
a substrate including a honeycomb sandwich panel or a foam core sandwich panel and an intermediate layer that covers a surface of the honeycomb sandwich panel or a surface of the foam core sandwich panel,
a decorative layer that covers a surface of the substrate,
an adhesive layer that is arranged vertical stripes, horizontal stripes, wavy stripes, diagonal stripes, or dots and that adheres to the decorative layer to the substrate so as to meet a required adhesive strength, and
a peel layer that is disposed between the intermediate layer and the adhesive layer and that includes a release agent to decrease an adhesive force of the adhesive layer to the intermediate layer, wherein
the decorative layer is-pasted to the surface of the substrate via the adhesive layer, and the decorative layer pasted to the surface of the substrate is peelable by heating at a temperature lower than a heat-resistant temperature of the substrate,
the adhesive layer has a softening temperature lower than the heat-resistant temperature of the substrate, and does not include an unfoamed foaming agent and foam,
a resin forming the adhesive layer consists of a thermoplastic resin having an adhesive strength decreased by heating at a temperature lower than the heat-resistant temperature of the substrate, and
the intermediate layer is formed by a filler and has an uneven surface facing the adhesive layer.
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