| 主权项 |
1. A gas turbine comprising
a combustion chamber with an exhaust section through which a combustion gas is exhaustable, a plenum chamber, a compressor for generating a compressed fluid, wherein the plenum chamber is coupled to the compressor such that a first quantity of the compressed fluid is injectable into the plenum chamber at a radially inner wall of the plenum chamber, and a guide vane section with at least one airfoil, wherein the guide vane section is coupled to the exhaust section such that the combustion gas is flowable against the airfoil, wherein the exhaust section and the guide vane section are housed inside the plenum chamber, wherein the airfoil comprises a first flow chamber which is formed such that a second quantity of the compressed fluid is flowable through the guide vane section from the compressor in the direction from the radially inner wall to a radially outer wall of the plenum chamber before being discharged into the plenum chamber, and wherein the second quantity of compressed fluid which is streamable through the guide vane section is larger than the first quantity of the compressed fluid. |
