| 摘要 |
The gas turbine (1) has a bleed air system (4) for the compressor (2), a tap (5) on the housing (3) of the compressor and a bleed air outlet (6). A bleed-air chamber (7) is formed between the tap and the bleed air outlet. The bleed air system has a device, by which a part of the bleed air (L) is passed out in partial mass flow from the tap. |
