| 摘要 |
PROBLEM TO BE SOLVED: To provide an inlet bleed heat exchange system and method for a compact gas turbine inlet.SOLUTION: An inlet system for a gas turbine includes an inlet air duct; a silencer disposed in the inlet air duct, the silencer including a plurality of panels with spaces interposed between the panels; and a conduit with orifices disposed to inject inlet bleed heat into each of the spaces. A method of conditioning inlet air for a gas turbine includes causing air to flow through the spaces between the panels of the silencer into the inlet air duct of the gas turbine, and injecting inlet bleed heat through the orifices and into each of the spaces. |
