Processes for repairing complex laminated composites
AssigneeBell Helicopter Textron Inc.
InventorsDenver R. Whitworth, Eric W. Nottorf, Vance N. Cribb, III, Dumitru Jitariu
Life of this patent
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Abstract
Complex laminated composites may be repaired by removal of individual damaged plies through peeling in order to exploit the weaker interlaminar properties of these composites. Upon removal of the individual damaged plies through peeling, replacement plies may be added to restore the laminated composite. In addition, when damage extends through the thickness of a laminated composite, a plug may be used to allow plies to be replaced while maintaining contour within the repair region. A caul plate also may be used to stiffen and maintain the contour of a repair region while peeling and removing plies from the repair region.
Claims7
A method for repairing a laminated composite, the method comprising:
- mapping dimensions and arrangement of a plurality of plies forming the laminated composite;
- defining a repair region by identifying at least one of the plurality of plies that is damaged;
- scoring the one or more damaged plies before peeling occurs, wherein fibers within the one or more damaged plies are taken hold of to begin peeling and removing the one or more damaged plies, wherein the scoring is performed in such a way that the one or more damaged plies are not completely cut through;
- peeling and removing the one or more damaged plies from the repair region,
- wherein each of the one or more damaged plies is separately peeled and removed;
- and
- adding at least one replacement ply to the repair region,
- wherein the number of replacement plies added is at least equal to the number of damaged plies that are separately peeled and removed so as to preserve ply drops within the laminated composite, and
- wherein the number of replacement plies match ply for ply the damaged plies that have been separately peeled and removed.
Dependencies are inferred from the claim text.