The problem of the reduction of the vulnerability to damage of aircraft hydraulic systems is divided into two catagories. Various methods of attack upon each catagory are outlined and the suggestion made that the problem be attacked from both sides and by several methods simultaneously. When all engineers cooperate they can design hydraulic systems having very low relative vulnerability thus permitting full enjoyment of the weight savings, reliability, ease of repair, flexibility, and accuracy of control, which hydraulic systems provide.This paper is presented in the hope that it will stimulate thought by all aircraft engineers to the end that our airplanes will be not only better but safer.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    REDUCTION OF VULNERABILITY OF AIRCRAFT HYDRAULIC SYSTEMS


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Field, Howard (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1945-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Fire/Explosion Vulnerability Reduction of Advanced Aircraft

    Mahood, Levelle | SAE Technical Papers | 1990


    Vulnerability Reduction Features for Commercial Derivative Combat Aircraft

    Anderson, Torger / Williamsen, Joel / Truett, Leonard | AIAA | 2006


    Aircraft hydraulic systems

    Neese, William A. | TIBKAT | 1987


    Aircraft hydraulic systems

    Neese, William A. | TIBKAT | 1991