The aircraft gas turbine inlet guiding cone has a cone-shaped body, which is mounted at a holding ring (3) mounted at a fan rotor disk. The body is formed in a single piece over an axial length. The body is connected at a cone-shaped storage area with a rigidly formed cone-shaped carrier area. The carrier area is mounted at the fan rotor disk. A glass fiber strand and a carbon fiber strand are connected parallel to each other in the inlet guiding cone. The inlet guiding cone is made up of titanium alloy, prepreg and aluminum alloy.


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    Titel :

    Fluggasturbinen-Einlaufkonus


    Weitere Titelangaben:

    Inlet nose cone for an aircraft gas turbine powerplant
    Cône d'entrée d'une turbine à gaz pour aéronef


    Beteiligte:

    Erscheinungsdatum :

    26.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge