A thermal-layered veneer product for aircraft interior components may include at least one substrate layer. The thermal-layered veneer product may include at least one thermally-conductive layer disposed on the at least one substrate layer. The at least one thermally-conductive layer may include at least one perforated graphite layer. The thermal-layered veneer product may include at least one non-fire-retardant coated veneer layer disposed on the at least one thermally-conductive layer. The at least one veneer layer may be non-fire-retardant coated. One or more of the at least one substrate layer, the at least one thermally-conductive layer, or the at least one veneer layer may be compliant with a FAR 25.853 burn test.
Thermal-Layered Veneer Product for Aircraft Interior Components
2021-11-04
Patent
Elektronische Ressource
Englisch
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