| 摘要 |
A gas turbine with a single can combustor and a gases bifurcated collector, wherein the combustor (5) comprises a gas chamber (7) whose axis is substantially orthogonal to the main machine axis (X) and delimited by a wall (9) obtained on which are primary holes (15), through which the air required to complete the combustion - coming from a compressor (2) - passes, and holes for dilution air (16a, 16b) near the outlet section of the gas chamber wherein the latter is introduced into the gases bifurcated collector (18, 20) whose mean lying plane is substantially orthogonal to the main axis (X), the dilution air holes (16a) obtained around the direction of the main axis (X) have a larger section with respect to the dilution air holes (16b) obtained around the direction orthogonal to said main axis (X). Thus, improved homogenization of the temperature of the hot gases entering into the turbine is attained. |
