| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine system under consideration of an optimum diffuser function. SOLUTION: This gas turbine system includes a compressor (102) activated to output air stream (101), a diffuser (106) activated to diffuse the air stream (101), a fuel nozzle (118) activated to receive fuel and to emit the fuel into a combustor (124), and at least one bleed duct (120) activated to guide the bleed air to the fuel nozzle (118) from the downstream of the combustor (124). COPYRIGHT: (C)2011,JPO&INPIT |
