TY - JOUR
T1 - Bonded repair of composite aircraft structures
T2 - A review of scientific challenges and opportunities
AU - Katnam, K. B.
AU - Da Silva, L. F.M.
AU - Young, T. M.
PY - 2013/8
Y1 - 2013/8
N2 - Advanced composite materials have gained popularity in high-performance structural designs such as aerospace applications that require lightweight components with superior mechanical properties in order to perform in demanding service conditions as well as provide energy efficiency. However, one of the major challenges that the aerospace industry faces with advanced composites - because of their inherent complex damage behaviour - is structural repair. Composite materials are primarily damaged by mechanical loads and/or environmental conditions. If material damage is not extensive, structural repair is the only feasible solution as replacing the entire component is not cost-effective in many cases. Bonded composite repairs (e.g. scarf patches) are generally preferred as they provide enhanced stress transfer mechanisms, joint efficiencies and aerodynamic performance. With an increased usage of advanced composites in primary and secondary aerospace structural components, it is thus essential to have robust, reliable and repeatable structural bonded repair procedures to restore damaged composite components. But structural bonded repairs, especially with primary structures, pose several scientific challenges with the current existing repair technologies. In this regard, the area of structural bonded repair of composites is broadly reviewed - starting from damage assessment to automation - to identify current scientific challenges and future opportunities.
AB - Advanced composite materials have gained popularity in high-performance structural designs such as aerospace applications that require lightweight components with superior mechanical properties in order to perform in demanding service conditions as well as provide energy efficiency. However, one of the major challenges that the aerospace industry faces with advanced composites - because of their inherent complex damage behaviour - is structural repair. Composite materials are primarily damaged by mechanical loads and/or environmental conditions. If material damage is not extensive, structural repair is the only feasible solution as replacing the entire component is not cost-effective in many cases. Bonded composite repairs (e.g. scarf patches) are generally preferred as they provide enhanced stress transfer mechanisms, joint efficiencies and aerodynamic performance. With an increased usage of advanced composites in primary and secondary aerospace structural components, it is thus essential to have robust, reliable and repeatable structural bonded repair procedures to restore damaged composite components. But structural bonded repairs, especially with primary structures, pose several scientific challenges with the current existing repair technologies. In this regard, the area of structural bonded repair of composites is broadly reviewed - starting from damage assessment to automation - to identify current scientific challenges and future opportunities.
KW - Adhesive bonding
KW - Bonded scarf repair
KW - Composite machining
KW - Composite materials
KW - Non-destructive testing
KW - Surface preparation
UR - http://www.scopus.com/inward/record.url?scp=84880722068&partnerID=8YFLogxK
U2 - 10.1016/j.paerosci.2013.03.003
DO - 10.1016/j.paerosci.2013.03.003
M3 - Review article
AN - SCOPUS:84880722068
SN - 0376-0421
VL - 61
SP - 26
EP - 42
JO - Progress in Aerospace Sciences
JF - Progress in Aerospace Sciences
ER -