A mounting apparatus for a turbine exhaust case (TEC) is provided. The mounting apparatus may include a neck, support links and a plurality of fastening pins. The neck may include an upper portion that is receivable within a pylon associated with the TEC and at least one neck aperture extending therethrough. The support links may downwardly extend from a lower portion of the neck. The support links may be configured to at least partially receive a section of the TEC. Each support link may include at least one link aperture extending therethrough. The fastening pins may include at least one neck pin extending through the neck aperture and at least one link pin extending through the link aperture of each support link.


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    Titel :

    REDUNDANT FASTENING OF A TURBINE EXHAUST CASE MOUNT


    Weitere Titelangaben:

    REDUNDANTE BEFESTIGUNG EINES TURBINENABGASGEHÄUSES
    FIXATION REDONDANTE D'UN CARTER D'ÉCHAPPEMENT DE TURBINE


    Beteiligte:
    SUCIU GABRIEL L (Autor:in) / ALVANOS IOANNIS (Autor:in)

    Erscheinungsdatum :

    23.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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