FIELD: turbines or turbomachines.
SUBSTANCE: disclosed is combustion chamber (9) of a gas turbine, comprising flame tube (15), casing (17), in which at least combustion tube (15) of the combustion chamber is located, and a supporting device for the flame tube. Supporting device for flame tube comprises separate supporting elements (19) located between fire tube (15) and combustion chamber casing (17). Each supporting element (19) contains supporting component (31) of the flame tube, which is attached to flame tube (15) of the combustion chamber, and supporting component (41) of the jacket, attached to combustion chamber casing. Each supporting component (41) of casing comprises socket (43) for casing retainer, fixed on casing (17) of combustion chamber, and detachable casing stopper (45), connected to said socket (43) with possibility of disconnection.
EFFECT: disclosed is a replaceable supporting device for a flame tube of combustion chambers of a gas turbine.
15 cl, 10 dwg
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