This paper describes work that was done to demonstrate the practical appliation of bonded repair procedures that provided significantly improved environmental durabilty. Results of the work led to the recommendation of the phosphoric acid nontank anodize process for surface preparation of aluminum for bonded repairs. The repairs were accomplished under both on the aircraft and off-the-aircraft conditions. The repairs were nondestruviely and destructively evaluated, including examination of the bond surfaces with a scanning electron microscope. (DePo)
Demonstration of an improved method for repair of bonded aircraft structure
Verbessertes Verfahren fuer die Reparatur geklebter Flugzeugteile
1979
10 Seiten, 14 Bilder, 1 Tabelle, 13 Quellen
Conference paper
English
Application of Bonded Composite Repair Technology to Civil Aircraft — B747 Demonstration Programme
Emerald Group Publishing | 1993
|Application of Bonded Composite Repair Technology to Civil Aircraft - B74M Demonstration Programme
British Library Online Contents | 1993
|Bonded repair of aircraft structures
TIBKAT | 1988
|Bonded repair of aircraft structures
SLUB | 1988
|