The patent application relates to a vortex swirler for use in the combustion chamber of a gas turbine having a plurality of swirler vanes and a deflector. The swirler vanes are used in conjunction with the fuel nozzle of the combustion chamber in order to provide a primary mixing of fuel and air in the region of the vanes. The deflector is formed in conjunction with a plurality of appertures in order to direct air against the walls of the combustion chamber for purposes of cooling the walls.


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    Title :

    Induced Vortex Swirler


    Contributors:

    Publication date :

    1974


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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