Design and Evaluation of Novel Composite Aircraft Repairs

2003-01-3016

09/08/2003

Event
World Aviation Congress & Exposition
Authors Abstract
Content
One of the most common damages occurred found on commercial airframes are dents and gouges. The usual repair for these damages includes installation of metallic doublers with rivets or with hi-loks. Sometimes these doublers are of complex design, because of multiple angles of the original damaged skin. Many times the damages are in hard to reach areas. In these cases the traditional metallic doubler repairs are not only time consuming and but also expensive. As the numerous holes are be drilled through the original structure, its fatigue life is adversely affected. For airline operators, time is valuable and they cannot afford to lose revenue by spending longer time for repairs. The use of bonded composite doublers offers the airframe manufacturers and aircraft repair facilities an alternative repair process that alleviates the abovementioned concerns. Instead of riveting multiple steel or aluminum plates to facilitate an aircraft repair, it is now possible to bond a single Boron-Epoxy composite doubler to the damaged structure.
Meta TagsDetails
DOI
https://doi.org/10.4271/2003-01-3016
Pages
11
Citation
Sheth, N., and Roach, D., "Design and Evaluation of Novel Composite Aircraft Repairs," SAE Technical Paper 2003-01-3016, 2003, https://doi.org/10.4271/2003-01-3016.
Additional Details
Publisher
Published
Sep 8, 2003
Product Code
2003-01-3016
Content Type
Technical Paper
Language
English