Low-ductility turbine shroud and mounting apparatus

• US 8,740,552 B2
• Filed: 05/28/2010
• Issued: 06/03/2014
• Est. Priority Date: 05/28/2010
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Marusko, Mark Willard, Albers, Joseph Charles, Dziech, Aaron Michael, Johnson, Christopher Ryan
• Primary Examiner(s): Wiehe, Nathaniel
• Assistant Examiner(s): Brownson, Jeffrey A
• Application Number:
  US12/790,209
• Publication Number:
  US 20110293410A1
• Time in Patent Office: 1,467 Days
• Field of Search: 415/173.2
• US Class Current: 415/173.1
• CPC Class Codes: F01D 11/08 for sealing space between rotor blade tips and stator specially-shaped blade tips therefor F01D5/20
• CPC Class Codes: F01D 11/122 with erodable or abradable material blades having cutting or grinding tips F01D5/20
• CPC Class Codes: F01D 9/04 forming ring or sector
• CPC Class Codes: F05D 2250/70 Shape
• CPC Class Codes: F05D 2300/2261 of silicon
• CPC Class Codes: F05D 2300/228 Nitrides
• CPC Class Codes: F05D 2300/603 Composites; e.g. fibre-reinforced
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A turbine shroud apparatus for a gas turbine engine includes an arcuate turbine shroud segment of low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed inner and outer walls, the walls extending between opposed first and second end faces. At least a portion of each of the forward and aft walls is oriented at an acute angle to the outer wall. Radially inner ends of the forward and aft walls are substantially closer together than radially outer ends thereof.

Claims

1. A turbine shroud apparatus for a gas turbine engine, comprising:

(a) a plurality of arcuate shroud segments arranged to form an annular shroud, each of the shroud segments comprising low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed inner and outer walls, the walls extending between opposed first and second end faces, wherein at least a portion of each of the forward and aft walls is oriented at an acute angle to the outer wall, and wherein radially inner ends of the forward and aft walls are substantially closer together than radially outer ends thereof; and

(b) an annular stationary structure including substantially rigid annular forward and aft bearing surfaces which bear directly against the forward and aft walls, respectively, of the shroud segment, so as to restrain the shroud segments from axial movement and radially inward movement relative to the stationary structure, wherein one of the bearing surfaces includes at least one tab extending therefrom, each of the at least one tabs received in a notch formed in one of the shroud segments so as to prevent relative rotation of the shroud segment and the stationary structure.

2. The apparatus of claim 1 wherein each of the forward and aft walls extends along a straight line between its radially inner and outer ends.

3. The apparatus of claim 1 wherein:

(a) each of the forward and aft walls includes;

(i) an outer portion extending inward from the outer wall, wherein radially inner ends of the radially outer portions are closer together than radially outer ends thereof; and

(ii) an inner portion which extends between the outer portion and the inner wall in a substantially radial direction; and

(b) the forward and aft bearing surfaces bear against the outer portions of the forward and aft walls, respectively.

4. The apparatus of claim 1 wherein the shroud segments comprise a ceramic matrix composite material.

5. The apparatus of claim 1 wherein the stationary structure includes:

(a) an annular turbine case surrounding the shroud segments;

(b) a flange extending radially inward from the turbine case and defining the aft bearing surface; and

(c) a removably mounted retainer extending radially inward from the turbine case and defining the forward bearing surface.

6. The apparatus of claim 1 wherein the stationary structure carries a locating pin which extends radially inward and engages a recess or hole formed in the outer wall of one of the shroud segments to as to prevent relative rotation of the shroud segment and the stationary structure.

7. The apparatus of claim 1 further including at least one shroud loading spring disposed between the stationary structure and the shroud segments which urges the shroud segments towards the bearing surfaces.

8. The apparatus of claim 7 wherein a leaf-type shroud loading spring is disposed between each of the shroud segments and the stationary structure.

9. The apparatus of claim 7 wherein each shroud loading spring is retained by a locating pin carried by the stationary structure.

10. The apparatus of claim 1 wherein the outer wall of at least one of the shroud segments includes at least one rib extending therefrom which bears against a locating pin carried by the stationary structure so as to prevent relative rotation of the shroud segment and the stationary structure.