| 摘要 |
A system (100, 200, 300, 400) for heating the inlet-air (130) of a gas turbine (105) is provided. The system (100, 200, 300, 400) may incorporate an external energy source (170) to increase the temperature of the inlet-air (130). The system (100, 200, 300, 400) may extend the turndown of a gas turbine (105) operating at partload. |
