A spinner for a gas turbine engine is disclosed. The spinner may include a body extending between a first and second end comprised of a cured chopped unidirectional fiber pre-impregnated material. The body may have a generally conical shape and may further be plated with a metal or metal alloy.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Gas Turbine Engine Spinner


    Beteiligte:
    KLING COLIN J (Autor:in) / BUGAJ SHARI L (Autor:in) / ROACH JAMES T (Autor:in)

    Erscheinungsdatum :

    2016-06-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    Gas turbine engine spinner

    KLING COLIN J / BUGAJ SHARI L / ROACH JAMES T | Europäisches Patentamt | 2019

    Freier Zugriff

    Gas turbine engine with reinforced spinner

    ROACH JAMES T / COOK III GRANT O / KLING COLIN J et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    GAS TURBINE ENGINE WITH REINFORCED SPINNER

    ROACH JAMES T / COOK III GRANT O / KLING COLIN J et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Crosswind performance aircraft engine spinner

    CLARK ADAM WAYNE / CEDAR RICHARD DAVID / RIDDLE DAVID BAKER | Europäisches Patentamt | 2019

    Freier Zugriff

    CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER

    CLARK ADAM WAYNE / CEDAR RICHARD DAVID / RIDDLE DAVID BAKER | Europäisches Patentamt | 2017

    Freier Zugriff