Boron/Epoxy Patching Efficiency Studies

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 1-2, Issue , 2002, Pages 375-397

  Baker, A A ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; BORON; CRACKS; CURING; EFFICIENCY; FREQUENCY MODULATION; GRAPHITE; GROWTH RATE; MICROMETERS;

BONDED COMPOSITE REPAIRS; CONSTANT AMPLITUDE; CRACK GROWTH BEHAVIOR; CURING TEMPERATURE; ELECTRICAL CONDUCTIVITY; METALLIC STRUCTURES; RADIUS OF CURVATURE; REINFORCING MATERIALS;

FATIGUE OF MATERIALS;

EID: 84940870239     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50015-2     Document Type: Chapter

References (10)

1. Baker A.A. Crack patching: Experimental studies, practical applications. Bonded Repair of Aircraft Structures 1988, 107-173. Chapter 6, Martinus Nijhoff, Melbourne, Australia. A.A. Baker, R. Jones (Eds.).
2. Baker A.A. Bonded composite repair of metallic aircraft components. Paper 1 in AGARD-CP-550 Composite Repair of Military Aircraft Structure 1994.
3. Rose L.R.F. Theoretical analysis of crack patching. Bonded Repair of Aircraft Structures 1988, 107-173. Chapter 5, Martinus Nijhoff. A.A. Baker, R. Jones (Eds.).
4. Wang C.H., Rose L.R.F. Bonded repair of cracks under mixed mode loading. Int. J. of Solids 1998, 35:2748-2773.
5. Baker A.A. Repair efficiency in fatigue-cracked panels reinforced with boron/epoxy patches. Fatigue and Fracture of Engineering Materials and Structures 1993, 16:753-765.
6. Chalkley P.D., Baker A.A. Development of a generic repair joint for certification of bonded composite repairs. Int. J. Adhesion and Adhesives 1999, 19:121-132.
7. Baker A.A., Chester R.J. Minimum surface treatments for adhesively bonded repairs. Int. J. of Adhesives and Adhesion 1992, 12:73-78.
8. Baker A.A., Beninati O. Repair efficiency in composite patched panels after removal of corrosion damage. Proc. of Int. Aerospace Conf. 1997, 53-60.
9. Baker A.A. On the certification of bonded composite repairs to primary aircraft structure. Proc. of ICCM 11 1997, Volume 1:1-24. Gold Coast Australia, July.
10. Baker A.A., Rose L.R., Walker K.F. Repair substantiation for a bonded composite repair to F-111 lower wing skin. Applied Composite Materials 1999, 6:251-267.