Method for repairing a composite article

Method for repairing a damaged or defective part (2) of a composite or sheet-like article (1). The method comprises the steps of placing a repair patch (3) over the damaged or defective part of the article, locating a pressure chamber including moulding tool means (7) over at least the damaged or de...

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Bibliographische Detailangaben
1. Verfasser:	WESTERDAHL, ANDERS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	Method for repairing a damaged or defective part (2) of a composite or sheet-like article (1). The method comprises the steps of placing a repair patch (3) over the damaged or defective part of the article, locating a pressure chamber including moulding tool means (7) over at least the damaged or defective part (2) of the article (1) and curing. The method comprises the further step of applying a viscous material (5) in the vicinity of the damaged or defective part (2) of the article (1) before curing and heating the viscous material (5) so that it becomes less viscous and flows into any undesired gaps between the moulding tool means (7) and the article (1).