Current design of variable-geometry elements of prototype supersonic transport, including wing-pivot joint, services routing, and actuator system, has undergone number of refinements prior to definition of present configuration; effort has resulted in wing-pivot joint that is similar to any other structural element and that is expected to require only in-place inspection during life of airplane; design of movable services and accessibility provided for outboard wing services in wing-pivot-joint area are expected to require only slightly more maintenance than that required for fixed-wing design; actuation system utilizes proved highly reliable, redundant hydraulic and mechanical elements.


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    Titel :

    Maintainability considerations in variable geometry aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Onewein, L.J. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Supersonic



    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Maintainability Considerations in Variable Geometry Aircraft

    Onewein, L. J. | SAE Technical Papers | 1967


    Aerodynamic Design Considerations of Variable Geometry Aircraft

    Herring, R. N. / Landgraf, S. K. | SAE Technical Papers | 1967


    Aerodynamic design considerations of variable geometry aircraft

    Landgraf, S.K. / Herring, R.N. | Engineering Index Backfile | 1967



    Aircraft design for maintainability

    MAJOROS, ANTHONY | AIAA | 1989