摘要:
A method for controlling a temperature distribution within a combustor (10) having a plurality of chamber sections (38A..., 38F) comprises controlling a fuel-to-air ratio in the chamber sections (38A..., 38F). At least two chamber sections (38A, 38B) have different fuel-to-air ratios to create a non-uniform temperature distribution within the combustor to reduce thermoacoustic instabilities.
摘要:
A method for controlling a temperature distribution within a combustor (10) having a plurality of chamber sections (38A..., 38F) comprises controlling a fuel-to-air ratio in the chamber sections (38A..., 38F). At least two chamber sections (38A, 38B) have different fuel-to-air ratios to create a non-uniform temperature distribution within the combustor to reduce thermoacoustic instabilities.