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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Demonstration of an improved method for repair of bonded aircraft structure


    Weitere Titelangaben:

    Verbessertes Verfahren fuer die Reparatur geklebter Flugzeugteile


    Beteiligte:
    Horton, R.E. (Autor:in)


    Erscheinungsdatum :

    1979


    Format / Umfang :

    10 Seiten, 14 Bilder, 1 Tabelle, 13 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Application of Bonded Composite Repair Technology to Civil Aircraft - B74M Demonstration Programme

    Barthlomeusz, R. A. / Paul, J. J. / Roberts, J. D. | British Library Online Contents | 1993


    Application of Bonded Composite Repair Technology to Civil Aircraft — B747 Demonstration Programme

    Rarthlomeusz, R,A. / Paul, J.J. / Roberts, J.D. | Emerald Group Publishing | 1993


    Bonded repair of aircraft structures

    Baker, Alan A. ;Jones, R. | TIBKAT | 1988


    Bonded repair of aircraft structures

    Baker, Alan A. | SLUB | 1988


    Bonded/Fusion Repair of Aircraft Structures

    W. Becker / J. Ho | NTIS | 1990