A heat shield assembly (300) includes a first heat shield segment (302) having a first end and a second end spaced from the first end, and a heat shield retainer (304) including a radial extension, wherein a torque bar aperture extends through the radial extension, the torque bar aperture configured to receive a torque bar. The heat shield retainer is secured from radial movement via the radial extension.


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    Title :

    HEAT SHIELD RETAINER AND METHODS


    Additional title:

    HITZESCHILDHALTERUNG UND VERFAHREN
    DISPOSITIF DE RETENUE DE BOUCLIER THERMIQUE ET PROCÉDÉS


    Contributors:

    Publication date :

    2021-01-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge



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