Concept and technique for solving problems associated with prediction and control of flight component failures which are attributed to contamination of power transmission fluid are presented; systems and applications considered are hydraulic type flight control servo actuators as used on B-58 Bomber, Century series type fighter aircraft, missiles, etc; technique assumes that these failures are probabilistic; mathematical models are established and comparisons made between calculated and measured values of contamination in system to determine degree of acceptability of fluid.


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    Titel :

    Criteria for contamination level in flight control systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Schmitt, V.R. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Hydraulic equipment



    Erscheinungsdatum :

    1967


    Format / Umfang :

    18 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Criteria for Contamination Level in Flight Control Systems

    Schmitt, Vernon R. | SAE Technical Papers | 1968


    Design criteria for optimal flight control systems

    GOVINDARAJ, K. / RYNASKI, E. | AIAA | 1979



    Design Criteria for Optimal Flight Control Systems

    K.S. Govindaraj / E.G. Rynaski | AIAA | 1980