| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine combustor including a flow sleeve structure improved in vibration-resisting performance.SOLUTION: A gas turbine combustor includes a liner 5, a transition piece 4, and a flow sleeve 7 composed of a plurality of split pieces integrated by welding a tie piece 8 along their butting portions. The tie piece is continuously extended along the longitudinal direction of the butting portions of the split pieces, and composed of a first member 81 disposed to cover the butting portions, and a second member 82 formed on an end portion of the first member, being wider than the first member, and having a cutout portion 10. |
