An inlet assembly for a high-mach engine includes a gas turbine core, an inlet turbine, and a core-flow director. When in a closed position, the core-flow director forces air to interact with the inlet turbine before entering the gas turbine core.


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    Titel :

    Inlet turbine for high-mach engines


    Beteiligte:

    Erscheinungsdatum :

    2020-10-06


    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



    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 AND TRANSMISSION FOR HIGH-MACH ENGINES

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

    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