COMPONENT FOR STAGED COMBUSTION IN A GAS TURBINE AND CORRESPONDING GAS TURBINE

摘要

The invention relates to a blade (20) for a turbine comprising a blade wall (30, 32), a first channel (36) for guiding a first medium (M1) and a second channel (38) for guiding a second medium (M2) that can be supplied to the turbine blade (20) separately from the first medium (M1). In order to combine both media (M1, M2), which are supplied separately, into one mixture, the turbine blade (20) has least one chamber (40) which is arranged in the interior or in the blade wall (32, 34) and said chamber is connected to said channels (36, 38) via a respective connection line (42, 44). In order to provide a particularly simple component that is eco