The development and mechanical characterization of candidate nonflammable aerospace hydraulic fluids for use over the temperature range of -54 to 135 Cel is described. The criteria of selection of the base fluids to enhance their viscosity-temperature and antiwear characteristics is discussed. Bulk modulus data are presented for the candidate fluids. Results from the mechanical characterization of candidate fluids in typical aerospace hydraulic pumps are presented. (Wassmann)


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    Title :

    Development and mechanical evaluation of nonflammable aerospace -54 Cel to 135 Cel hydraulic fluids


    Additional title:

    Entwicklung und mechanische Ueberpruefung von nichtbrennbaren Weltraumhydraulikfluessigkeiten fuer den Bereich -54 Cel bis 135 Cel


    Contributors:

    Published in:

    Publication date :

    1980


    Size :

    10 Seiten, 5 Bilder, 10 Tabellen, 2 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Development and mechanical evaluation of nonflammable aerospace (-54 Cel to 133 Cel) hydraulic fluids

    Snyder, C.E. / Gschwender, L.J. / Campbell, W.B. | Tema Archive | 1982


    Nonflammable hydraulic system development for aerospace

    Snyder, C.E. / Gschwender, L.J. | Tema Archive | 1984


    Nonflammable Aircraft Hydraulic Systems Development

    Snyder, Jr., Carl E. / Gandee, Gregory W. / Gschwender, Lois J. et al. | SAE Technical Papers | 1982