The patent 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 apertures in order to direct air against the walls of the combustion chamber for purposes of cooling the walls.
Induced Vortex Swirler
1974
4 pages
Report
No indication
English
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