| 摘要 |
Contrarotating outward-flow gas turbine without stators and with two rotors (1 and 2) which set in motion the power shaft (3) and the compressor shaft (17), respectively. The inlet air (19) is sent through the impellers (20) of the outward-flow compressor to the manifold (22) and from there to the regenerator (24) where it is preheated; then, it reaches the combustion chamber (14) and from there it expands to the rotors, and finally passes through the exhaust manifold (27). The rotors (1 and 2) contrarotate coaxially on their bearings (11), both rotors having one or a plurality of rings of vanes (5, 6, 7, 8), and additionally flow guiding fins (9). <IMAGE> |
