Patent ID: 8413993
Filing Date: 2013-04-09
Classification: F01D,F05D

Abstract:
1. A sealing ring for turbomachines, comprising: a plurality of individual sealing segments; and a plurality of springs, wherein the plurality of springs are installed between the plurality of individual sealing segments, and wherein a plurality of locking elements are provided at a parting joint of the turbomachine for retaining the plurality of sealing segments, and wherein the plurality of individual sealing segments are interconnected in a form-fitting manner at the parting joint, wherein one end of an individual sealing segment at the parting joint includes a projecting cylindrical pin such that the parting joint and the projecting cylindrical pin are one piece, wherein the cylindrical pin extends in an axial direction of the turbomachine and fits into a corresponding recess at an end of an adjacent sealing segment such that the projecting cylindrical pin in the sealing segment and the adjacent sealing segment with the corresponding recess are mating pairs.