Some examples of an aircraft engine barrier filtration system include an engine barrier filter layer positioned near an aircraft engine intake. The filter layer filters aircraft engine intake air. The system includes a check valve assembly positioned adjacent to the engine barrier filter layer. The check valve assembly permits the engine intake air to flow into the engine through the filter layer during a first aircraft operation mode and to prevent air flow away from the engine through the filter layer during a second aircraft operation mode that is different from the first aircraft operation mode.


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    Titel :

    Filters for aircraft engine inlets


    Beteiligte:
    BRAND ALBERT G (Autor:in)

    Erscheinungsdatum :

    13.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    FILTERS FOR AIRCRAFT ENGINE INLETS

    BRAND ALBERT G | Europäisches Patentamt | 2015

    Freier Zugriff

    De-Icing of Aircraft Turbine Engine Inlets

    H. A. Rosenthal / D. O. Nelepovitz / H. M. Rockholt | NTIS | 1988


    De-icing of aircraft turbine engine inlets

    Rosenthal, H.A. / Nelepovitz, D.O. / Rockholt, H.M. | Tema Archiv | 1988


    Electro-impulse de-icing of aircraft engine inlets

    NELEPOVITZ, D. / ROSENTHAL, H. | AIAA | 1986


    High Efficiency Ice Protection System (HEIPS) for Aircraft Engine Inlets

    Sweet, David B. / Brown, Keith T. / Layland, Michael J. | SAE Technical Papers | 2004