The present invention relates to a thermal-layered veneer product for aircraft interior components. The product 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.

    本发明涉及一种用于航空器内部部件的含热层的饰面制品,其可以包括至少一个基材层。含热层的饰面制品可以包括布置在所述至少一个基材层上的至少一个导热层。所述至少一个导热层可以包括至少一个穿孔石墨层。含热层的饰面制品可以包括布置在所述至少一个导热层上的涂敷有非阻燃剂的至少一个饰面层。所述至少一个饰面层可以是非阻燃涂层。所述至少一个基材层、所述至少一个导热层或所述至少一个饰面层中的一者或多者可以符合FAR 25.853燃烧测试。


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    Title :

    THERMAL-LAYERED VENEER PRODUCT FOR AIRCRAFT INTERIOR COMPONENTS


    Additional title:

    用于航空器内部部件的含热层的饰面制品


    Contributors:

    Publication date :

    2021-09-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge



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