Method for repairing a damaged composite component having fibre optics
The invention is directed to a method for repairing a damaged composite fiber component of an aircraft having at least one integrated fiber optic, the damaged area including both a damaged composite structure and a damaged optical fiber, comprising mechanically removing material from the damaged are...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | The invention is directed to a method for repairing a damaged composite fiber component of an aircraft having at least one integrated fiber optic, the damaged area including both a damaged composite structure and a damaged optical fiber, comprising mechanically removing material from the damaged area, to form a removed area, exposing ends of the damaged composite fiber component in an edge area of the removed area, splicing-in a bridging fiber optic portion for restoring an optical connection, laying the bridging fiber optic along an edge area of the removed area, and pressing and gluing-in a repair patch into the removed area. |
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