| 摘要 |
The compressor (1) has fuel distributors (15) which rotate with it and which are located between the paddle blades (5). The compressed fuel mist (102) is diverted through a number of holes (8) in a compressor end wall (2) after passing the outer ends of the paddle blades. Jet nozzles (7) behind these holes have outlet parts (9) oriented in the rotation direction and designed to eject the compressed fuel mist for ignition in a combustion chamber (72). A number of blow plates (56) are evenly distributed on the inside of a combustion chamber plate (30). The compressor is designed to rotate in a given direction and comprises a hub, a front cover plate, a rear cover plate and paddle blades. A mixture of air (69) and fuel is delivered to the region between the cover plates, the fuel being supplied from a distributor in the form of a compressed mist. |
