Gas turbine combustor
This gas turbine combustor (2) is equipped with: a combustion chamber (50) in which fuel and air are burned to generate combustion gas; multiple fuel nozzles (30) arranged in multiple concentric circular rows; a first plate (32), which is provided downstream from the multiple fuel nozzles (30), and...
Saved in:
Main Authors | , , |
---|---|
Format | Patent |
Language | English |
Published |
18.11.2015
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Be the first to leave a comment!