System for developing composite repair patches on aircraft or other composite structures

A system for generating a repair patch for a damaged area of a composite structure may include a scanning module, a repair patch model generator and a cutting tool. The scanning module may be deployed at the location of the damaged composite structure. The scanning module may be configured to scan t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Salah Lamia, Brown Brian M, Tomblin John
Format: Patent
Sprache:eng
Schlagworte:
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