Aero engines for marine propulsion offer very low size and weight advantages which, however, are obviated by the size of the ducting necessary to transport the inlet air and exhaust gases. Early failures were due to imposing unrealistic space constraints, and current installations are based upon considerable research and model testing to avoid a recurrence. More recently, and due to revised thinking on silencing, it is shown that duct size and top weight can be substantially reduced, thus providing immediately available installation advantages. (Kursetz)


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    Titel :

    Marine gas turbine inlet and exhaust systems for the R.N.


    Weitere Titelangaben:

    Systeme an Ansaugleitungen und Abgasleitungen fuer Marinegasturbinen fuer die englische Kriegsmarine


    Beteiligte:
    Tayler, C.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1978


    Format / Umfang :

    12 Seiten, 14 Bilder, 2 Tabellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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