Device, system and method for preventing leakage in a turbine

Patent metadata

Field	Value
Publication number	US-9453422-B2
Application number	US-201313790758-A
Country	US
Kind code	B2
Filing date	Mar 8, 2013
Priority date	Mar 8, 2013
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

A turbine disk and blade assembly comprises a turbine disk including a plurality of disk posts extending radially therefrom and a plurality of disk slots between adjacent disk posts. The turbine disk is of a first material having a first coefficient of thermal expansion. The assembly further comprises a plurality of turbine blades. One of the turbine blades is received in each disk slot. The turbine blades are of a second material having a second coefficient of thermal expansion. The assembly further comprises a plurality of seal plates, wherein one of the seal plates is positioned in each disk slot radially inward of the turbine blade. The seal plates are of a material having a coefficient of thermal expansion substantially similar to that of either the disk posts or the turbine blade.

First claim

What is claimed is:

1. A system for preventing air leakage within a turbine, comprising:
a turbine disk including a plurality of disk posts extending radially therefrom and a plurality of disk slots between adjacent disk posts, said turbine disk being of a first material having a first coefficient of thermal expansion;
a plurality of turbine blades, one of said turbine blades being received in each said disk slot, said turbine blades being of a second material having a second coefficient of thermal expansion; and
a plurality of seal plates, wherein one of said seal plates is positioned in each disk slot radially inward of the turbine blade, said seal plates being of a material having a coefficient of thermal expansion substantially similar to that of either said disk posts or said turbine blade such that said seal plates thermally expand or contract an amount similar to a thermal expansion or contraction of at least one of the plurality of disk posts or the plurality of turbine blades; and
a sealing member coupled with at least a portion of said assembly and configured to seal said disk slots, wherein a first end of said sealing member couples with said turbine blades, a second end of said sealing member couples with said turbine disk, and a middle portion between said first and second ends of said sealing member couples with said seal plates and one of the plurality of turbine blades or plurality of disk posts.

2. The system of claim 1 , wherein:
said seal plates comprise one of said first or second materials.

3. The system of claim 1 , wherein at least a portion of a shape of each said seal plate is essentially complementary to at least a portion of each said disk slot.

4. The system of claim 1 , wherein:
when said assembly experiences a change in ambient temperature, said sealing member follows the thermal expansion or contraction of at least a portion of said assembly and maintains the seal of said disk slots.

5. The system of claim 1 , wherein said sealing member envelops at least a portion of each said disk slot.

6. The system of claim 1 , wherein:
said middle portion couples with said seal plates and said disk posts;
said first end follows the thermal expansion of said turbine blades;
said second end follows the thermal expansion of said turbine disk; and
said middle portion follows the thermal expansion of said seal plates and said disk posts.

7. The system of claim 1 , further comprising:
a wire positioned on said assembly adjacent at least a portion of each plate.

8. The system of claim 7 , further comprising:
a channel in said sealing member, wherein said wire is positioned in said channel.

9. The system of claim 7 wherein said wire is adjacent an axially facing face of each seal plate.

10. The system of claim 7 , wherein said wire follows the thermal expansion of at least a portion of said assembly.

11. A method of preventing air leakage within a turbine, comprising:
assembling a turbine blade and disk assembly, the assembly comprising a turbine disk including a plurality of disk posts extending radially therefrom and a plurality of disk slots between adjacent disk posts, the turbine disk and disk posts being of a first material having a first coefficient of thermal expansion, and plurality of turbine blades, each turbine blade being of a second material having a second coefficient of thermal expansion, the assembling step further comprising:
positioning one turbine blade in each disk slot; and
positioning one seal plate in each disk slot radially inward of each turbine blade, each seal plate being of a material having a coefficient of thermal expansion substantially similar to that of either the disk posts or the turbine blades such that the seal plates thermally expand or contract an amount similar to a thermal expansion or contraction of at least one of the plurality of disk posts or the plurality of turbine blades; and
coupling a sealing member with at least a portion of the assembly such that the sealing member seals at least a portion of each disk slot; and
coupling a first end of the sealing member with the blades; coupling the second end of the sealing member with the disk; and coupling a middle portion of the sealing member between the first and second ends with the plates and one of the plurality of blades or plurality of posts.

12. The method of claim 11 , wherein when the assembly experiences a change in ambient temperature, the sealing member follows the thermal expansion or contraction of at least a portion of the assembly and maintains the seal of the slots.

13. The method of claim 11 , further comprising:
coupling the middle portion with the plates and the posts.

14. The method of claim 11 , wherein the coupling step further comprises enveloping at least a portion of each slot with the sealing member.

15. The method of claim 11 , further comprising:
positioning a wire on the assembly adjacent to at least a portion of each plate.

16. The method of claim 15 , wherein the wire is further positioned adjacent an axially facing face of each plate.

Assignees

• Gen Electric

Inventors

• Hile Michael Alan
• Agnew Brian
• Grooms James Hamilton
• Jendrix Richard William

Classifications

• F01D5/3015 Primary

  with side plates · CPC title

• Y10T29/49321

  Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member · CPC title

• F01D5/3084

  the blades being made of ceramics · CPC title

• F01D5/3092

  Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers (F01D5/288 takes precedence) · CPC title

• F05D2300/50212

  dissimilar · CPC title