Control method for a gas turbine plant
Provided is a control method for a gas turbine plant having a first and a second (14) combustors in series, such that combustion gases produced in said first combustor flow into said second combustor. The second combustor having a fuel lance (27) with internal partitions, for injecting at least one...
Saved in:
Main Authors | , , , , , |
---|---|
Format | Patent |
Language | English French German |
Published |
24.07.2013
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Be the first to leave a comment!