Method for repairing a damaged outer skin region on an aircraft

Details Method for repairing a damaged outer skin region on an aircraft Method for repairing a damaged outer skin region on an aircraft

C - Chemistry, Metallurgy

23

C

C23C 24/04 (2006.01)

Patent

CA 2649208

The invention relates to a method for repairing a damaged outer skin region on an aircraft, in which the possibility exists for repairing possible damage to a plated layer, which is adhered to the outer skin of a passenger aircraft and protects the latter in the undamaged state from corrosion. With it, the plated layer can be repeated in the area of existing damage without incidental reworking.

L'invention concerne un procédé pour réparer une région endommagée de revêtement externe sur un aéronef, dans lequel on peut réparer un dommage possible sur une couche plaquée, qui est collée sur le revêtement externe d'un aéronef de passagers et dans lequel on peut protéger de la corrosion ce dernier dans l'état non endommagé. Selon le procédé, la couche plaquée peut être répétée dans la zone d'un dommage existant sans une réfection temporaire.

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