| 摘要 |
The gas turbine has an annular combustion chamber between an annular outer combustion chamber wall on one side and an annular combustion chamber inner wall (28) on the other, which is composed of a number of wall elements fixed to a bearing structure. The bearing structure is composed of components (30) of the wall meeting at horizontal joint points (31), angled to the inner wall surface and joined by screw joints (32).
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