| 摘要 |
PROBLEM TO BE SOLVED: To provide an annular combustion chamber, which allows a quick assembly and disassembly, combined with improved thermal properties.SOLUTION: A first zone of a combustion chamber of a gas turbine receives a fuel/air mixture of a plurality of burners. A second zone guides hot gases from the first zone to an entrance of a turbine section. Each of liner segments 22a located at a transition between the first zone and the second zone includes a leading edge 35a, a trailing edge 35d and two sidewalls 35b, 35c, and is provided with axial mounting means 27, 31 at the leading edge 35a and the trailing edge 35d, such that the liner segment 22a can be installed in the axial direction and is axially fixed by segments 21c of the neighboring first zone 18. Spacer ribs 30 are provided at the leading edge 35a in order to form a gap 29 of a minimum width between the liner segments 22a and the fixing segments 21c of the neighboring first zone 18. |
