The disclosure relates to a burner Such as for a secondary combustion chamber of a gas
turbine with sequential com bustion having a first and a second combustion chamber, with
an injection device for introduction of at least one gaseous and/or liquid fuel into the burner.
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 gaseous fuel into the burner, the at least one body
being configured as a stream lined body which has a streamlined cross-sectional profile and …