<p>The stator vane carrier (10) has a tubular wall (20) with an inflow lateral end (16) and an outflow lateral end (18) lying opposite to inflow lateral end for fluid flowing in an inner space (40) of the stator vane carrier in a flow path of a gas turbine. A cooling duct (26) is provided in a wall for a cooling agent, which extends from a cooling agent inlet to a cooling agent outlet (36). A groove is provided in an outer surface (22) of the wall for each cooling duct, which is locked by a cover for the admission of the cooling duct. An independent claim is included for a gas turbine with a pressured core.</p>
