Patent ID: 8128357

Claim:
A stator blade segment for a thermal turbomachine, comprising: a platform having at least one essentially flat surface; a profiled blade airfoil arranged on and extending away from the essentially flat surface of the platform facing away from the blade airfoil; a plurality of fastening elements for fastening the stator blade segment onto an associated stator blade carrier arranged on the essentially flat side of the platform that faces away from the blade airfoil, wherein at least one of the fastening elements is a separately produced component connected in a fixed manner to the essentially flat surface of the platform that faces away from the blade airfoil, and comprises a fastening hook which projects from the platform and a connecting element having a flat bearing surface arranged in a recess formed on the essentially flat surface of the platform facing away from the airfoil, such that the fastening element is connected in a locking manner at least in an axial direction.