A SIGNIFICANT NUMBER of the helicopters presently in the US Army inventory are inherently unstable and use pressurised hydraulic fluid in the hydromechanical flight control system. The development of a hydrofluidic stability-augmentation system which can be integrated into the helicopter primary control system, offering promise of improved reliability, maintainability, and reduced cost over conventional electromechanical stability augmentation systems, has been accomplished.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Evolution of the hydrofluidic liquid SAS


    Beteiligte:
    EVANS, RICHARD A. (Autor:in) / FOSDICK, G.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.06.1972


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Hydrofluidic Servoactuator Development

    H. C. Kent / J. R. Sjolund | NTIS | 1973


    Hydrofluidic Flight Controls

    Posingies, W. M. | SAE Technical Papers | 1970


    Advanced Hydrofluidic Stabilization System

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