| 摘要 |
<p>The method for reheating a gas flowing through a turbine in a main flow direction is implemented in such a way that a fuel which is fed to the gas (11) is combusted, forming self-igniting micro-diffusion flames. An oxidation medium is fed to the gas directly upstream of the feed position for fuel, as seen in the main flow direction. Oxygen, compressed air, or cooling air is used as the oxidation medium. Independent claims are included for the following: (1) a component (30), especially for implementing the proposed method for reheating gas flowing through a turbine, with openings (42) in an outer wall (46), each of which is small in such a way that during feed of a first medium, formed as fuel, micro-diffusion flames (33) result; and (2) a turbine with a component for implementing the proposed method for reheating gas flowing through a turbine.</p> |
