A turbomachine (10) comprising a nozzle (14) extending along an axial direction (A), said nozzle (14) being configured to convey a hot gas stream (GC), and a mounting pylon (12) for mounting the turbomachine, said pylon (12) extending radially from a base (12a) arranged in the vicinity of the nozzle (14). The turbomachine (10) includes a pylon cooler device (18) having at least one auxiliary gas duct (20) having a gas inlet (20a) configured to take cold gas (GF) from the outside of the nozzle (14), and a gas outlet (20b) opening out in the vicinity of the base (12a) of the pylon (12).


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    Title :

    TURBOMACHINE COMPRISING A DEVICE FOR THE COOLING OF A PYLON


    Contributors:

    Publication date :

    2015-10-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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