This paper describes the application of hydrofluidics to stability augmentation systems. Criteria for selecting fluidics for a specific application are presented. A typical hydrofluidic system is presented to show principles of operation, transfer functions, and component performance. A brief description of the power supply system shows how this system is integrated into existing aircraft without extensive modifications to the hydraulic power supply. Major problem areas of noise, leakage, and contamination are discussed.


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    Titel :

    Hydrofluidic Flight Controls


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970



    Erscheinungsdatum :

    1970-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Development and Flight Test of an Advanced Hydrofluidic Stabilization System

    D. Bengtson / J. Hedeen / R. Helfinstine | NTIS | 1976


    Advanced Hydrofluidic Stabilization System

    M. E. Ebsen / J. O. Hedeen | NTIS | 1972


    Evolution of the hydrofluidic liquid SAS

    EVANS, RICHARD A. / FOSDICK, G.W. | Emerald Group Publishing | 1972



    Flight Controls

    Dryden, Joe Bill | Online Contents | 1994