Temperatures measured for variety of conditions by thermocouples, leads of which were brought away from turbine by means of rotating slip rings and stationary brushes; it was estimated that maximum temperature at rim of rotor at rated altitude would be approximately 1175 F for this particular installation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Turbosupercharger-rotor temperatures in flight


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Barton, E.R. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    12 pages


    Anmerkungen:

    10 Supp plates


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    ENGINE WITH TURBOSUPERCHARGER

    NIWA YASUSHI / SUMIMOTO HIROSHI / NAKAJIMA MITSUHIRO | Europäisches Patentamt | 2017

    Freier Zugriff

    Cooling hood for turbosupercharger

    Engineering Index Backfile | 1945



    First turbosupercharger application on airliner

    Engineering Index Backfile | 1948