Patent ID: 8147190

Claim:
A stator vane for a gas turbine, which stator vane comprises: a vane airfoil which extends in a longitudinal direction of the stator vane and is delimited by a leading edge and a trailing edge; an outer platform, an inner side of which is positioned for exposure to turbine gas, and on which at least one hook-like fastening element projects outwards in a region of the trailing edge; at least one locating slot arranged above the trailing edge for fastening the stator vane on a casing or on an element of a gas turbine; means for reducing thermal and mechanical stresses in a region of transition between the trailing edge and the outer platform, the means for reducing being located on the outer platform of the stator vane, between the locating slot and the trailing edge of the vane airfoil; and wherein the trailing edge is set back in a turbine gas flow direction by a distance (a) in relation to the fastening element.