A clamp suitable for use in an anti-icing system of a gas turbine engine is provided is disclosed. The clamp has a clasping portion for clasping a heating element. Two resilient arms extend from the clasping portion to a substantially rigid outer collar. Translational movement of the clasping portion, which may be created by radial expansion of an annular heating element being clasped thereby, can be accommodated by the clamp by elastic deformation of the resilient arms. This allows radial expansion of the heating element to be accommodated without relative rotation between the clasping portion and the heating element.


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    Titel :

    Gas turbine engine anti-icing mounting arrangements


    Weitere Titelangaben:

    Aufhängung für Enteisungsanordnungen von Gasturbinenmotoren
    Agencements de montage d'un essemble anti-givrage de turbine à gaz


    Beteiligte:
    HINDLE ANDREW (Autor:in) / LITTLEY BENJAMIN (Autor:in) / JOHNSON ALANA (Autor:in) / LAMBERT KEITH (Autor:in)

    Erscheinungsdatum :

    21.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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