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 :

    17.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Inlet turbine and transmission for high-mach engines

    DIERKSMEIER DOUGLAS D / RICE EDWARD C / TOMLINSON STEVEN W et al. | Europäisches Patentamt | 2021

    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. | SAE Technical Papers | 1954


    Inlet protection for aircraft gas turbine engines

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