Effective mission capability of future V/STOL aircraft demands significant propulsion system advancements in lower specific weight, higher specific performance, improved operational reliability, and improved structural integrity; major design innovations include light weight blades, integrated propeller and gearbox, variable camber, shrouded propellers, and redundant control systems; they were applied to two VTOL aircraft programs, XC-142 and X-22A; paper describes development programs and current hardware status and defines their performance, weight, and functional potentials.


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    Titel :

    Advanced propeller developments for V/STOL aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Rosen, G. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 VTOL-STOL



    Erscheinungsdatum :

    1965


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Advanced Propeller Developments for V/STOL Aircraft

    Rosen, George | SAE Technical Papers | 1965



    PROPELLER WHIRL FLUTTER CONSIDERATIONS FOR V/STOL AIRCRAFT

    Bennett, R. M. / Reed, W. H., III | NTRS | 1963


    Ducted propeller for STOL airplanes

    Raspet, A. | Engineering Index Backfile | 1960