A high-Mach engine includes a gas turbine core, an inlet assembly, and a transmission. The inlet assembly including an inlet turbine and the transmission configured to couple the inlet turbine and a core turbine of the gas turbine core cooperate to control air moving through the high-Mach engine.


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    Titel :

    Inlet turbine and transmission for high-mach engines


    Beteiligte:

    Erscheinungsdatum :

    2021-03-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    INLET TURBINE AND TRANSMISSION FOR HIGH-MACH ENGINES

    DIERKSMEIER DOUGLAS D / RICE EDWARD C / TOMLINSON STEVEN W et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Inlet turbine for high-mach engines

    DIERKSMEIER DOUGLAS D / RICE EDWARD C / TOMLINSON STEVEN W et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Inlet protection for aircraft gas turbine engines

    Litton, R.S. | Engineering Index Backfile | 1954



    INLET PROTECTION FOR AIRCRAFT GAS TURBINE ENGINES

    LITTON, R. S. | SAE Technical Papers | 1954