Patent ID: 8622708

Claim:
A stator blade for a turbomachine which is exposable to an axial throughflow, comprising: a blade root, including two oppositely disposed sides and also including a platform; a blade airfoil which is arranged on the platform; and a projecting shaped piece, wherein the blade root on a first side of the two sides includes a first projecting shaped piece in which provision is made for a threaded hole for a radial tensioning of the stator blade in a circumferential groove of a carrier structure of a turbomachine using a first tensioning screw which is screwed into the threaded hole and supported on a bottom of the circumferential groove, and wherein the blade root on a second side of the two sides includes a recess for accommodating a second projecting shaped piece of an adjacent stator blade, including a second tensioning screw which is screwed into the second projecting shaped piece.