A gas turbine engine comprising a compressor, a compressor case surrounding the compressor and a compressor tip injector system is disclosed. The compressor tip injector system comprises a cabin blower system comprising a cabin blower compressor arranged in use to compress air used in a cabin of an aircraft and by the compressor tip injector system. The compressor case comprises one or more injectors of the compressor tip injector system through which in use air from the cabin blower compressor is injected towards blade tip ends of blades of the compressor as they rotate.


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    Titel :

    Compressor tip injector


    Beteiligte:
    KNIGHT GLENN A (Autor:in) / MAGUIRE ALAN R (Autor:in) / ROBINSON DANIEL (Autor:in) / BOSTOCK GEORGE (Autor:in) / WILSON MARK J (Autor:in)

    Erscheinungsdatum :

    2018-12-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



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    GAS TURBINE WITH COMPRESSOR BLADE TIP INJECTOR

    KNIGHT GLENN / MAGUIRE ALAN / ROBINSON DANIEL et al. | Europäisches Patentamt | 2016

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