Review of jet hydraulic system data indicated that two-thirds of all hydraulic system incidents during past 2 yr have been due to external system leakage in areas of lines, fittings, hoses, and seals; these areas must be given extensive consideration in design of SST; preliminary studies indicate that approximately 700 hydraulic hp may be used for various hydraulic systems; this might include 250 hp for flight control system; it is anticipated that hydraulic system operational temperatures will vary from 350 to 500 F.


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    Titel :

    Supersonic transport aircraft hydraulic systems


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Billet, A.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Supersonic Transport Aircraft

    Emerald Group Publishing | 1961


    Supersonic transport aircraft

    Russell, A.E. | Engineering Index Backfile | 1962


    Supersonic transport aircraft

    Engineering Index Backfile | 1961