Implantation Procedure patch for repairing aircraft structures and patch used in said process.

摘要

Implantation Procedure patch for repairing aircraft structures and patch used in said process. The method and patch used is intended to repair damaged areas on metallic aircraft structures such as cracks, so that the procedure is based primarily on drill two holes on the ends of the crack to prevent this extend, effecting a preliminary study to obtain the patch of composite material and then applying the adhesive as a means of attachment of the patch of composite material on the metallic structure to be repaired, the patch material comprises a number of layers determined prepreg and placed according to a suitable orientation being, complemented with fiber optic sensors that are embedded in the adhesive as bonding means between the patch itself composite and the metal structure on which it is applied.