Patent ID: 9605549
Date: 2017-03-28
CPC Classifications: B33Y,F01D,F05D,Y02T,Y10T

Claim:
1. A stationary blade ring for a turbomachine comprising: a plurality of rotatable stationary blades; an inner ring for radial inner stabilization of the stationary blades; a seal for sealing a radial clearance between the inner ring and a diametrically opposed rotor section; and bearing bodies for supporting the stationary blades in the inner ring, each stationary blade being supported via a bearing journal in a bearing hole of an individual bearing body of the bearing bodies, each bearing body having a cuboid main body in which the bearing hole is formed; the inner ring being composed of two half rings supporting the bearing bodies, each of the half rings spanning a circumferential angle of 180 degrees, and each having a U-shaped profile including, with respect to a flow direction of a main flow, a front wall, a rear wall and a circumferential wall connecting the front and rear walls.