The XF3-30 is the low-bypass-ratio turbofan engine which has been developed to power the XT-4 intermediate trainer for the Japan Air Self Defence Force. This engine has been designed and tested in accordance with the requirements of MIL-E-5007D with some modifications to meet the particular requirements of an intermediate trainer and circumstances in Japan. All of the qualification tests including endurance tests, low cycle fatigue test, altitude test, foreign object ingestion test and environmental icing test were successfully completed by Mar. 1986 and flight test of the XT-4 trainer aircraft powered by two of the XF3-30 engines has proceeded without any-engine related problems.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Development of the XF3-30 turbofan engine


    Weitere Titelangaben:

    Entwicklung des Blaesertriebwerks XF3-30


    Beteiligte:
    Yamada, H. (Autor:in) / Hamatani, H. (Autor:in) / Ishizawa, K. (Autor:in)

    Erschienen in:

    ASME-Papers ; Jun ; 1-7


    Erscheinungsdatum :

    1987


    Format / Umfang :

    7 Seiten, 8 Bilder, 3 Tabellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Turbofan engine

    NICHOLAS GRECH / CHRISTOPHER A MOSLEY / JOHN R WELLS | Europäisches Patentamt | 2020

    Freier Zugriff

    TURBOFAN ENGINE

    LIESER JAN / BOEHNING PEER | Europäisches Patentamt | 2019

    Freier Zugriff

    Geared turbofan engine

    BREEN CLIVE | Europäisches Patentamt | 2021

    Freier Zugriff

    GEARED TURBOFAN ENGINE

    BREEN CLIVE | Europäisches Patentamt | 2020

    Freier Zugriff