The damper segment can be assembled between adjacent segments of a pressurized gas pipe of an aircraft engine. The damper segment can have a proximal end, a distal end, a rigid tube at the proximal end, a damper tube extending between the rigid tube and the distal end, the damper tube being made of a metal mesh, a proximal catch structurally connecting a proximal end of the damper tube to the rigid tube, and a distal catch structurally connected between a distal end of the damper tube and the distal end, the damper tube having an unsupported length extending between the distal catch and the proximal catch, the rigid tube having a liner portion projecting into the distal segment, the liner portion extending internally relative the damper tube.


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    Titel :

    DAMPER SEGMENT FOR PRESSURIZED GAS PIPE OF AIRCRAFT ENGINE


    Weitere Titelangaben:

    SEGMENT D~AMORTISSEUR POUR TUYAU DE GAZ SOUS PRESSION D~UN MOTEUR D~AERONEF


    Beteiligte:
    LEFEBVRE GUY (Autor:in) / SYNNOTT REMY (Autor:in)

    Erscheinungsdatum :

    06.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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