Turbine shroud hanger

• US 5,593,276 A
• Filed: 06/06/1995
• Issued: 01/14/1997
• Est. Priority Date: 06/06/1995
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Proctor, Robert, Linger, David R., Plemmons, Larry W., Brassfield, Steven R., Di Salle, David A.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Lee, Michael S.
• Application Number:
  US08/467,436
• Time in Patent Office: 588 Days
• Field of Search: 415/173.1, 415/173.3, 415/134, 415/138
• US Class Current: 415/173.1
• CPC Class Codes: F01D 11/18 using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
• CPC Class Codes: F01D 25/246 Fastening of diaphragms or stator-rings

Abstract

A turbine shroud hanger is supported from an annular outer casing and includes an annular radial flange and integral forward and aft legs at a radially inner end thereof. The legs extend axially oppositely to each other and include respective distal ends configured for supporting a plurality of arcuate shroud panels radially above a plurality of turbine rotor blades to define a tip clearance therebetween. The legs include circumferentially spaced apart forward and aft slots extending axially from the distal ends thereof toward the radial flange, and completely radially therethrough to bifurcate the legs into circumferential segments for reducing transient thermal expansion of the hanger to reduce in turn expansion of the tip clearance.

Claims

1. A turbine shroud hanger being suspendable radially inwardly from a pair of adjacent radial flanges of an outer casing comprising:

a one-piece annular hanger radial flange and an integral hanger leg at a radially inner end thereof;

said hanger leg including a plurality of circumferentially spaced apart slots extending axially therethrough to bifurcate said leg into circumferential segments for reducing transient thermal expansion of said hanger.

2. A hanger according to claim 1 further comprising:

integral forward and aft hanger legs at said radially inner end of said radial flange;

said forward and aft legs extending axially oppositely to each other and including respective distal ends configured for supporting a plurality of arcuate shroud panels therefrom positionable radially outwardly from a plurality of turbine rotor blades to define a tip clearance therebetween; and

said forward and aft legs including respective pluralities of circumferentially spaced apart forward and aft slots extending axially from said forward and aft distal ends, respectively, toward said radial flange, and completely radially therethrough to bifurcate said forward and aft legs into circumferential segments for reducing transient thermal expansion of said hanger to reduce in turn expansion of said tip clearance as said shroud panels travel with said hanger forward and aft legs.

3. A hanger according to claim 2 wherein said forward and aft slots have respective axial lengths and circumferential widths, and said widths are predetermined in size for accommodating without closing said slots due to circumferential thermal expansion of said forward and aft leg segments upon radial thermal expansion of said hanger.

4. A hanger according to claim 3 wherein said axial lengths of said forward and aft slots are predetermined in size for reducing transient rocking of said forward and aft legs about said radial flange to reduce in turn rocking of said shroud panels for maintaining said shroud panels substantially level during operation to control said tip clearance.

5. A hanger according to claim 4 wherein said forward and aft slots are disposed perpendicular to said radial flange.

6. A hanger according to claim 4 wherein said forward and aft slots extend substantially axially up to said radial flange.

7. A hanger according to claim 4 wherein said forward and aft slots are circumferentially indexed relative to each other at different circumferential positions.

8. A hanger according to claim 7 wherein said forward slots are circumferentially spaced equidistantly between respective ones of said aft slots.

9. A hanger according to claim 4 wherein said forward and aft legs are different in size, and said forward and aft slots have different lengths.

10. A hanger according to claim 4 further including a respective stress relieving aperture at the junction of each of said forward and aft slots with said radial flange.

11. A hanger according to claim 4 wherein:

said radial flange and said forward and aft legs are configured generally in a Y-shape in section to define a shroud cavity radially above said shroud panels;

said radial flange includes a plurality of impingement holes extending therethrough into said shroud cavity between said forward and aft legs for impinging bleed air against said shroud panels and pressurizing said shroud cavity; and

said forward and aft slots are sized to maintain backflow pressure margin in said shroud cavity notwithstanding leakage of said bleed air radially outwardly through said forward and aft slots.