| 摘要 |
The invention includes a gas-turbine unit with a compressor. In order to design a compact, single-shaft gas turbine so that it can easily and rapidly coupled as a module to various machines, the invention proposes that the rotor of the compressor and a turbine wheel (12) are located next to each other on the same shaft (14), diffusor blades at the radial extreme of the compressor rotor being located at one side of a plate (54) and guide vanes on the other side of the plate which has openings connecting with cooling channels or cavities in the guide vanes. |
