Adhesive bonding of aircraft structures

International Journal of Adhesion and Adhesives

Volumn 20, Issue 5, 2000, Pages 367-376

  Higgins, A ^a  

^a BAE SYSTEMS   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AGING OF MATERIALS; AIRCRAFT MATERIALS; ALUMINUM ALLOYS; BONDING; EPOXY RESINS; PHENOLIC RESINS; RIVETING; STRENGTH OF MATERIALS; VINYL RESINS;

ADHESIVE BONDING;

PLASTIC ADHESIVES;

EID: 0034299816     PISSN: 01437496     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0143-7496(00)00006-3     Document Type: Article

References (9)

1. Various BAe internal studies of long term warm/wet immersion of adhesive bonded lap shear test pieces of Hexcel Redux 775, Hexcel Redux 308A, Cytec FM73 and 3M Co. AF163-2 adhesives.
2. Dixon D. Prediction of lap shear and peel strength of adhesive bonds, and update on results of accelerated environmental testing. BAe Sowerby Research Centre, Report No:JS 13729, May 1997. p. 3.
3. Beevers A. Project 3, Environmental durability of adhesive bonds, Report No.9 Forensic studies of adhesive joints - Part 2 Bonded aircraft structure. September 1995. p. 33.
4. Evans GB. 40 years of structural adhesive bonding. - Chartered Mechanical Engineer 1985, p. 23-27.
5. De Bruyne NA. Redux in aircraft Ciba Company Inc. 1955, Available from Hexcel Composites, Duxford.
6. Aero Research Technical Note, Redux - The first 12 years. Bulletin No. 149, Hexcel Composites Duxford.
7. Aero Research Technical Note, The structure of the DeHavilland Comet bulletin No. 165, Hexcel Composites Duxford.
8. Reavey DG. Marine experience of structural adhesives in Hovercraft. SAMPE Journal 1981; pp 18-21.
9. USA Air Force. Primary Adhesive Bonded Structure Technology (PABST) program - Technical Report AAF/DL/TR76-141 Dec.1976. p. 223-246.