IP Library › Granted Patent US 10,850,460
Granted Patent B2
US 10,850,460 · App. 16/694,339 · Granted Dec 1, 2020

Processes for repairing complex laminating composites

Inventors: Denver R. Whitworth (North Richland Hills, TX); Eric W. Nottorf (Fort Worth, TX); Vance N. Cribb (Aledo, TX); Dumitru Jitariu (Flower Mound, TX)
Assignee: TEXTRON INNOVATIONS INC.
B29C73/10B29C73/26B29C70/30B29C2073/264
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Quick Facts
Patent No.
US 10,850,460
App. No.
16/694,339
Granted
Dec 1, 2020
Kind
B2
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.

Claims (12)

1. A method for repairing a laminated composite having a plurality of plies, the method comprising:

locating damage to one or more of the plurality of plies, the location of the damaged one or more of the plurality of plies forming a repair region;

removing the damaged one or more of the plurality of plies from the repair region, wherein the damaged one or more of the plurality of plies are scored before being removed, wherein fibers within the damaged one or more of the plurality of plies are taken hold of to begin removing the damaged one or more of the plurality of plies, wherein the scoring is performed in such a way that the damaged one or more of the plurality of plies are not completely cut through;

affixing a sacrificial plug to the repair region;

peeling and removing at least one layer of the sacrificial plug; and

adding at least one replacement ply to the repair region.

2. The method of claim 1 , wherein the sacrificial plug is formed of the same material as the plurality of plies forming the laminated composite.

3. The method of claim 1 , wherein the peeling and removing step is repeated until each layer of the sacrificial plug has been removed, and

wherein the thickness of the at least one replacement ply added to the repair region is equivalent to the thickness of the layers of the sacrificial plug that are removed.

4. The method of claim 1 further comprising:

applying a patch after the sacrificial plug is affixed to the repair region.

5. The method of claim 1 , wherein the damaged one or more of the plurality of plies are removed through peeling.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 25, 2019
From: WHITWORTH, DENVER; NOTTORF, ERIC; CRIBB, VANCE; JITARIU, DUMITRU
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 051106/0942 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 25, 2019
From: BELL HELICOPTER TEXTRON INC.; BELL HELICOPTER RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 051109/0795 →
Continuity (3)
Division 15810957 · Nov 13, 2017
Division 13433106 · Mar 28, 2012
Related Publication 20200086593A1 · Mar 19, 2020