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Application filed by Юрий Леонидович СидорюкfiledCriticalЮрий Леонидович Сидорюк
Priority to UAA200811752UpriorityCriticalpatent/UA74111U/en
Publication of UA74111UpublicationCriticalpatent/UA74111U/en
Secondary nozzle for a gas turbine comprising a flange or flange, an elongated nozzle body extending from the flange, and at least one fuel premix injector spaced and parallel to the nozzle body; and the combustion chamber of a gas turbine.