| 摘要 |
PROBLEM TO BE SOLVED: To provide an improved combustor liner guide stopper for a gas turbine combustor, and a method for attaching a liner guide stopper.SOLUTION: A combustor for a gas turbine includes a casing, a flow sleeve at least partially disposed within the casing, a combustion liner at least partially disposed within the flow sleeve, a liner stopper feature part extending from the combustion liner, and a liner guide stopper including a first end separated from a second end configured to be at least partially engaged with the liner stopper feature part, and the liner guide stopper extends through the casing and the flow sleeve. |
