| 摘要 |
The invention relates to a gas turbine (1) comprising a duct (11) for carrying gas from a gas turbine inlet (9) to a gas turbine outlet (10) and an outer housing (19, 20, 21) arranged radially outside a wall structure (12, 13, 14), which defines the radially outer limits of the gas duct (11): the gas turbine (1) between the said inlet (9) and outlet (10) being constructed from a plurality of modules (6, 7, 8), each of which comprises a part of the said outer housing (19, 20, 21) and a part of the wall structure (12, 13, 14) of the gas duct; at least two adjacent parts of the wall structure (12, 13, 14) of the gas duct being arranged at a distance from one another; and at least one pressure dividing element (27, 33, 42) being designed to divide off a pressure area (P1, P3, P4, P5, P6) in the gas duct (11) at the junction between the said two adjacent parts of the wall structure (12, 13, 14) of the gas duct and the said outer housing (19, 20, 21) in which the said pressure dividing element (27, 33, 42) consists of a pressure wall extending from the wall structure (12, 13, 14) of the gas duct to the outer housing (19, 20, 21).
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