Patent ID: 8402768
Filing Date: 2013-03-26
Classification: F23R

Abstract:
1. A burner for a combustion chamber of a gas turbine, comprising: an injection device for the introduction of at least one gaseous and/or liquid fuel into the burner, wherein the injection device has at least one body which is arranged in the burner with at least one nozzle for introducing the at least one fuel into the burner, the at least one body being configured as a streamlined body which has a streamlined cross-sectional profile and which extends with a longitudinal direction perpendicularly or at an inclination to a main flow direction prevailing in the burner, the at least one nozzle having its outlet orifice at or in a trailing edge of the streamlined body; and with reference to a central plane of the streamlined body, the trailing edge is provided with at least two lobes extending in opposite transverse directions.