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The present invention relates to a turbine blade of a gas turbine with an airfoil arranged on a blade root and having at least one cooling air duct running in the longitudinal direction of the turbine blade, arranged inside the turbine blade and extending through the blade root, characterized in tha

The present invention relates to a turbine blade of a gas turbine with an airfoil arranged on a blade root and having at least one cooling air duct running in the longitudinal direction of the turbine blade, arranged inside the turbine blade and extending through the blade root, characterized in that at least one swirl-generating element is arranged in the transitional area between blade root and airfoil in the cooling air duct, with the swirl-generating element including an outer ring and several swirl-generating stator vanes arranged thereon, which are connected to a centric area, as well as to a method for its manufacture.

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1. A method for manufacturing a turbine blade, comprising the steps of: casting the turbine blade, the turbine blade including: a blade root;an airfoil arranged on the blade root;a cooling air duct running in a longitudinal direction of the turbine blade positioned inside and extending through the b

1. A method for manufacturing a turbine blade, comprising the steps of: casting the turbine blade, the turbine blade including: a blade root;an airfoil arranged on the blade root;a cooling air duct running in a longitudinal direction of the turbine blade positioned inside and extending through the blade root and the airfoil;providing a swirl-generating element manufactured as a separate component from the turbine blade from the step of casting the turbine blade, the swirl-generating element including an outer ring, a centric area and a plurality of swirl-generating stator vanes connecting between the outer ring and the centric area;after the step of casting the turbine blade, inserting the swirl-generating element through the blade root with a center axis of the swirl-generating element in a position transverse to a blade longitudinal axis;rotating the swirl-generating element in the cooling air duct;positioning the swirl-generating element in a transitional area in the cooling air duct between the blade root and the airfoil with the center axis substantially parallel to the blade longitudinal axis;providing the swirl-generating element with a locking recess to engage an engaging lug provided in the cooling air duct such that the locking recess is engaged with the engaging lug and the swirl-generating element is locked in the turbine blade upon the positioning. 2. The method of claim 1, and further comprising dimensioning the outer ring smaller than the cooling air duct at the blade root to be insertable into the cooling air duct from the blade root. 3. The method of claim 1, and further comprising providing that the swirl-generating element is made from a same material as the turbine blade. 4. The method of claim 1, and further comprising providing the swirl-generating element as a casting. 5. A method for manufacturing a turbine blade, comprising the steps of: providing a core for casting the turbine blade, the turbine blade including: a blade root,an airfoil arranged on the blade root and includinga cooling air duct running in a longitudinal direction of the turbine blade positioned inside and extending through the blade root and the airfoil,positioning a swirl-generating element in a transitional area in the core between the blade root and the airfoil in the cooling air duct, the swirl-generating element including an outer ring, a centric area and a plurality of swirl-generating stator vanes arranged connecting between the outer ring and the centric area;providing the swirl-generating element in the core for casting the turbine blade and wherein the swirl-generating element remains after removal of the core as a one-piece constituent of the turbine blade.