Reversible blade rotor seal with protrusions

Patent metadata

Field	Value
Publication number	US-9810087-B2
Application number	US-201514748876-A
Country	US
Kind code	B2
Filing date	Jun 24, 2015
Priority date	Jun 24, 2015
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

A sealing structure for a gas turbine engine includes a rotor that has a rim with slots and a cooling passage. The rotor is rotatable about an axis. First and second blades are arranged in the slots and respectively including first and second shelves facing one another within a pocket that is in fluid communication with the cooling passage. The first and second shelves form an opening. A reversible seal is arranged within the pocket and has a body that is configured for operative association with the first and second blades in any of four orientations to seal the opening in a second condition. The seal includes first and second protrusions respectively extending from first and second faces opposing one another. The first protrusions supported on the rim in a first condition.

First claim

What is claimed is:

1. A sealing structure for a gas turbine engine, comprising:
a rotor that has a rim with slots and a cooling passage, the rotor rotatable about an axis;
a first and second blades arranged in the slots and respectively including first and second shelves facing one another within a pocket that is in fluid communication with the cooling passage, the first and second shelves forming an opening; and
a reversible seal arranged within the pocket and having a body that is configured for operative association with the first and second blades in any of four orientations to seal the opening in a second condition, the seal includes first and second protrusions respectively extending from first and second faces opposing one another, the first protrusions supported on the rim in a first condition.

2. The sealing structure according to claim 1 , wherein the second face is configured to engage the shelves in the second condition, and the second condition is an engine operating condition.

3. The sealing structure according to claim 2 , wherein the second protrusions are located within the opening in the second condition.

4. The sealing structure according to claim 3 , wherein each of the shelves includes a leg that cooperates with the second protrusions to limit axial movement of the reversible seal in the first and second conditions.

5. The sealing structure according to claim 4 , comprising forward and aft covers respectively engaging forward and aft sides of the first and second blades to enclose the pocket, the legs arranged adjacent to the forward side, and the reversible seal configured to be installed from the aft side with the aft cover removed.

6. The sealing structure according to claim 1 , wherein the first and second faces are respectively spaced from the rim and the shelves in the first condition.

7. The sealing structure according to claim 6 , wherein the second protrusions extend into the opening in the first condition.

8. The sealing structure according to claim 1 , wherein the reversible seal extends in a generally axial direction corresponding to the axis, and each of the first and second faces are provided by angled surfaces joined at an apex.

9. The sealing structure according to claim 8 , wherein the apex is flat and is circumferentially centered within the opening in the second condition.

10. The sealing structure according to claim 8 , wherein the reversible seal includes first and second opposing ends spaced apart along the axis, each having a substantially parallelogram shape.

11. The sealing structure according to claim 10 , wherein the first and second opposing ends are parallel to one another, and the first and second faces are rectangular in shape from an elevational view.

12. The sealing structure according to claim 8 , wherein the each of the angled surfaces includes one protrusion that extends a length along the axis, the length less than an axial distanced between axially spaced first and second opposing ends of the reversible seal.

13. The sealing structure according to claim 1 , wherein the blades are turbine blades.

14. The sealing structure according to claim 13 , wherein the blades each include a platform that supports an airfoil, the platforms spaced radially outward relative to the shelves.

15. A seal for a gas turbine engine rotatable stage, the seal comprising:
a body includes first and second protrusions respectively extending from first and second faces opposing one another, the body is reversible 180° about first, second and third axes that are orthogonal relative to one another such that the seal body is installable in any of four unique orientations.

16. The seal according to claim 15 , wherein the reversible seal extends in a generally axial direction corresponding to the axis, and each of the first and second faces are provided by angled surfaces joined at an apex.

17. The seal according to claim 16 , wherein the apex is flat and is circumferentially centered within the opening in the second condition.

18. The seal according to claim 16 , wherein the reversible seal includes first and second opposing ends spaced apart along the axis, each having a substantially parallelogram shape.

19. The seal according to claim 18 , wherein the first and second opposing ends are parallel to one another, and the first and second faces are rectangular in shape from an elevational view.

20. The seal according to claim 16 , wherein the each of the angled surfaces includes one protrusion that extends a length along the axis, the length less than an axial distanced between axially spaced first and second opposing ends of the reversible seal.

Assignees

• United Technologies Corp

Inventors

• Corcoran Christopher
• Snyder Daniel A

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F01D5/3015

  with side plates · CPC title

• F05D2250/72

  symmetric · CPC title

• F05D2240/55

  Seals · CPC title

• F01D11/008

  by spacer elements between the blades, e.g. independent interblade platforms · CPC title