An aircraft turbojet engine low-pressure compressor or booster, comprising an inlet structure de-iced by a pressurized hot fluid circulation coming from the high-pressure compressor. The de-icing structure comprises a deformable membrane through the thickness of which the pressurized fluid circulation passes. When there is a build-up of ice on the membrane, the pressurized fluid circulation is blocked, resulting in its pressure deforming the membrane in such a manner as to crack the build-up of ice.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Turbofan engine de-icing compressor and de-icing process


    Beteiligte:

    Erscheinungsdatum :

    15.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    TURBOFAN ENGINE DE-ICING COMPRESSOR AND DE-ICING PROCESS

    RAIMARCKERS NICOLAS | Europäisches Patentamt | 2018

    Freier Zugriff



    The Effect of Crosswinds on Icing at Turbofan Engine Inlet

    Zheng, Mei / Yang, Qian / Dong, Wei et al. | SAE Technical Papers | 2019


    Modeling Commercial Turbofan Engine Icing Risk with Ice Crystal Ingestion

    Veres, Joseph P. / Jorgenson, Philip C. | AIAA | 2013