| 摘要 |
PROBLEM TO BE SOLVED: To provide a system and method for control of combustion dynamics in a combustion system.SOLUTION: The present disclosure generally relates to a system with a gas turbine engine including a first combustor and a second combustor. The first combustor includes a first end cover 13 with a first geometry, and the second combustor includes a second end cover 13 with a second geometry. The first geometry has one or more geometric differences relative to the second geometry. |
