Although the introduction of turbine engines in commercial aircraft brought many anticipated advantages in increased safety and reliability, many problems involving basic reliabilities arose to plague the operators. Underlying causes for various design limitations are preoccupation of the airlines, military inheritance, inadequate development, demonstrations in lieu of tests, knowledge interchange, and others.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Turbine Engine Reliability - Stage II


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1963-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW STAGE PRESSURE TURBINE

    SUCIU GABRIEL L / MERRY BRIAN D / DYE CHRISTOPHER M et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Analysis of factors affecting turbine engine reliability

    Rummel, K. / Byrne, M. | Tema Archiv | 1974


    Gas turbine engine with low stage count low pressure turbine

    SUCIU GABRIEL L / MERRY BRIAN D / DYE CHRISTOPHER M et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

    SUCIU GABRIEL L / MERRY BRIAN D / DYE CHRISTOPHER M et al. | Europäisches Patentamt | 2020

    Freier Zugriff