The extensive use of adhesive bonding in the manufacture of critical aircraft structures has focussed attention on the limitation of current N.D.T. methods to quantify joint strength. It is, however, recognised that N.D.T. alone cannot control adhesive bonding and must, therefore, take its place in a quality control programme. This paper outlines the problems and introduces some routes to solutions which are being developed.
Quality control of adhesive bonding in the manufacture of aircraft structures
Qualitaetsueberwachung von Klebverbindungen im Flugzeugbau
Structural Adhesives in Engineering. I Mech E Conf. ; 6 , Jun ; 133-138
1986
6 Seiten, 8 Bilder
Conference paper
English
Adhesive Bonding of Aircraft Primary Structures
SAE Technical Papers | 1980
|Adhesive Bonding of High Modulus Composite Aircraft Structures
SAE Technical Papers | 1971
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2021
|TIBKAT | 2021
|