A system and method of coupling a nose cone (110) to a turbine machine is provided. Nose cone assembly weight and coupling difficulty are each reduced by reducing or eliminating the number of bolts used to mount the nose cone to the turbine machine, as well as the support or retaining ring. The disclosed nose cone comprises a plurality of hub mounting elements including one or more bayonet flanges (132), two or more apertures (160) defined by a flange forming an annular hub mating surface of the nose cone (110) and configured to receive a fastener therethrough, and one or more pilot flanges.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LOW WEIGHT NOSE CONE ASSEMBLY


    Weitere Titelangaben:

    LEICHTGEWICHTIGE NASENHAUBENBAUGRUPPE
    ENSEMBLE DE CÔNE D'ENTRÉE DE FAIBLE POIDS


    Beteiligte:
    SCOTT MATTHEW (Autor:in)

    Erscheinungsdatum :

    09.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    LOW WEIGHT NOSE CONE ASSEMBLY

    SCOTT MATTHEW A | Europäisches Patentamt | 2018

    Freier Zugriff

    Low weight nose cone assembly

    SCOTT MATTHEW A | Europäisches Patentamt | 2019

    Freier Zugriff

    Nose cone assembly

    BOTTOME KRISTOFER J | Europäisches Patentamt | 2015

    Freier Zugriff

    Snap fit nose cone assembly

    SCOTT MATTHEW A | Europäisches Patentamt | 2019

    Freier Zugriff

    SNAP FIT NOSE CONE ASSEMBLY

    SCOTT MATTHEW A | Europäisches Patentamt | 2018

    Freier Zugriff