Composite article

Details Composite article Composite article

F - Mech Eng,Light,Heat,Weapons

16

D

F16D 69/02 (2006.01) C04B 35/83 (2006.01)

Patent

CA 2531799

A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from compressed C-C or from C-C impregnated with boron and/or silicon. The wear layer (23) may be fabricated from C-C.

L'invention concerne un article composite (21) s'utilisant dans un système puits de chaleur de freins d'aéronef. Ledit article comprend une couche médiane (22) présentant une section de face et une couche d'usure (23) fixée à la section de face. La couche d'usure (23) présente une masse volumique inférieure à celle de la couche médiane (22). Ladite couche médiane (22) peut être produite à partir de C-C comprimé ou de C-C imprégné de bore et/ou de silicium. La couche d'usure (23) peut être produite à partir de C-C.

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