Method for coating a fiber composite component for an...

Details Method for coating a fiber composite component for an... Method for coating a fiber composite component for an...

C - Chemistry, Metallurgy

23

C

C23C 4/02 (2006.01) B64D 45/02 (2006.01) C23C 4/04 (2006.01) C23C 4/12 (2006.01)

Patent

CA 2722108

The invention relates to a method for coating a fiber composite component (1) for an aircraft or spacecraft. According to said method, a surface layer (8) of the fiber composite component (1) which is interspaced from the fibers (3) that have been introduced into the fiber composite component (1) to protect them is pretreated in at least some sections thereof to form an adhesive layer (1); at least one functional layer (17, 18) is then applied to the formed adhesive layer (13). A corresponding fiber composite component (1) comprises at least one functional layer (17, 18) which is applied to an adhesive layer (13).

L'invention concerne un procédé pour l'application d'un revêtement sur un élément composite (1) renforcé par des fibres pour un aéronef ou un véhicule spatial. Selon ce procédé, on procède, en vue de la formation d'une couche adhésive (13), au prétraitement d'au moins certaines parties d'une couche de surface (8) de l'élément composite (1) située à distance des fibres (3) insérées dans l'élément composite (1) pour la protection de ces dernières, puis on procède à l'application d'au moins une couche fonctionnelle (17, 18) sur la couche adhésive formée (13). L'invention concerne également un élément composite (1) renforcé par des fibres qui présente au moins une couche fonctionnelle (17, 18) appliquée sur une couche adhésive (13).

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