| 摘要 |
The turbine has a flow channel (3) through which the surrounding air flows. A section (7) includes a constant cross section, into which the surrounding air is introduced, where an air acceleration device (39) is provided in the section (7). A section (7) is designed in the form of a venture nozzle, and a section (13) is designed in the form of a Laval nozzle (12). A section (15) includes another air acceleration device, which serves for production of air, which is guided into the flow channel. An independent claim is also included for a method for producing electricity from surrounding. |
