Flap seal spring and sealing apparatus

Patent metadata

Field	Value
Publication number	US-9234433-B2
Application number	US-201213472996-A
Country	US
Kind code	B2
Filing date	May 16, 2012
Priority date	Jun 1, 2011
Publication date	Jan 12, 2016
Grant date	Jan 12, 2016

Abstract

A biasing means is provided for securing a plurality of sealing components which are arranged to seal gaps between adjacent structural components in a turbine, the biasing means having three foot regions joined in a substantially linear fashion by two resilient curved arms, wherein each arm has securing means for securing the biasing means to one of said structural components such that when the biasing means is secured to said one of said structural components, each of said foot regions contacts one of said sealing components and the curved arms urge the sealing components towards one of said structural components so that the sealing components collectively create a seal over the gap between said structural components. An apparatus for sealing gaps between adjacent structural components which includes the biasing means is also provided as is a method of sealing gaps in a turbine.

First claim

The invention claimed is:

1. A biasing means for securing a plurality of primary sealing components and secondary sealing components, the primary and secondary sealing components being arranged to seal at least one gap between adjacent structural components in a turbine, the biasing means comprising:
at least three foot regions joined in a substantially linear fashion by two resilient curved arms, each arm including securing means for securing the biasing means to one of primary and secondary sealing components such that: (i) at least two foot regions is in direct contact with at least two respective secondary sealing components, (ii) one foot region is in direct contact with the primary sealing component, and (iii) one of said secondary sealing components and the curved arms urge the primary sealing components towards one of said structural components so that the secondary sealing components form a seal over the at least one gap between said structural components.

2. The biasing means according to claim 1 , wherein each securing means corresponds to a hole through which a pin can be inserted to secure the biasing means.

3. The biasing means according to claim 2 , wherein the holes are circular and the biasing means further includes stress reduction means configured to reduce a stress concentration around each of said holes.

4. The biasing means according to claim 3 , wherein the stress reduction means include further holes which are configured to reduce said stress concentration.

5. An apparatus for sealing a gap between two structural components of a turbine, the apparatus comprising:
a plurality of primary sealing components,
a plurality of secondary sealing components, and
the biasing means according to claim 1 for securing said sealing components to the structural components.

6. The apparatus according to claim 5 , wherein the apparatus is arranged, in use, to seal said gap by:
the primary sealing components being arranged to seal the majority of said gap with gaps being present between each pair of primary sealing components to allow for expansion or movement of said primary sealing components;
each secondary sealing component sealing a gap between a pair of primary sealing components;
a first primary sealing component being urged into contact with one of said structural components by the biasing means; and
at least one secondary sealing component being urged into contact with said first primary sealing component by the biasing means.

7. The apparatus according to claim 5 , wherein:
the foot regions of the biasing means include a central foot region and two end foot regions each joined to said central foot region by a respective one of said arms, and
in use, the first primary sealing component is urged into contact with said structural component by the central foot region of the biasing means and a secondary sealing component is urged into contact with said first primary sealing component by one of said end foot regions.

8. A turbine having a plurality of structural components with a gap between said structural components, the gap being sealed by a plurality of sealing components, the sealing components of the turbine comprising:
a plurality of primary sealing components,
a plurality of secondary sealing components, and
the biasing means according to claim 1 for securing said sealing components to the structural components, wherein:
the primary sealing components seal the majority of said gap with gaps being present between each pair of primary sealing components to allow for expansion or movement of said primary sealing components;
each secondary sealing component seals a gap between a pair of primary sealing components;
a first primary sealing component is urged into contact with one of said structural components by the biasing means; and
at least one secondary sealing component is urged into contact with said first primary sealing component by the biasing means.

9. The turbine according to claim 8 , wherein:
the foot regions of the biasing means include a central foot region and two end foot regions each joined to said central foot region by a respective one of said arms, and
the first primary sealing component is urged into contact with said structural component by the central foot region of the biasing means and a secondary sealing component is urged into contact with said first primary sealing component by one of said end foot regions.

10. A method of sealing a gap between two structural components in a turbine, the method including the steps of:
sealing a majority of the gap with a plurality of primary sealing components with gaps being left between each adjacent pair of primary sealing components to allow for expansion or movement of said primary sealing components;
sealing each gap between said plurality of primary sealing components with a secondary sealing component;
securing a first primary sealing component by urging it into contact with one of said structural components with a biasing means; and
securing at least one secondary sealing component by urging it into contact with said first primary sealing component with the biasing means, wherein
the biasing means includes at least three foot regions joined in a substantially linear fashion by two resilient curved arms, each arm includes securing means for securing the biasing means to one of primary and secondary sealing components such that: (i) at least two foot regions is in direct contact with at least two respective secondary sealing components, and (ii) one foot region is in direct contact with the primary sealing component.

11. The method according to claim 10 , the curved arms urge the secondary sealing components towards one of the primary sealing components so that the sealing components collectively create a seal over the gap between said structural components.

12. The method according to claim 10 , wherein each securing means corresponds to a hole through which a pin can be inserted to secure the biasing means.

13. A flap seal spring for securing a plurality of sealing components arranged to seal at least one gap between adjacent structural components in a turbine, the flap seal spring comprising:
at least two resilient curved arms, each arm including at least one hole through which a pin is inserted; and
three foot regions joined in a substantially linear fashion by the at least two resilient curved arms such that when the flap seal spring is secured to one of the structural components, each of the foot regions contacts one of the sealing components and the curved arms urges the sealing components towards one of the structural components so that the sealing components collectively form a seal over the at least one gap between the structural components.

14. The flap seal spring according to claim 13 , wherein the at least one hole is circular.

15. The flap seal spring according to claim 13 , further comprising:
at least one triangular shaped hole configured to reduce a stress concentration around the at least one hole.

16. The flap seal spring according to claim 15 , further comprising:
at least one connector hole linking the at least one triangular shaped hole to the at least one hole.

17. The flap seal spring according to claim 15 , wherein at least one side of the at least one triangular shaped hole is curved.

18. The flap seal spring according to claim 13 , wherein an arm around the at least one hole has a curved profile.

Assignees

• Helvaci Caner H
• Rolls Royce Plc

Inventors

• Helvaci Caner H

Classifications

• F01D11/005 Primary

  Sealing means between non relatively rotating elements · CPC title

• Y10T29/49826

  Assembling or joining · CPC title

• F16J15/0887

  the sealing effect being obtained by elastic deformation of the packing · CPC title

• F01D11/00

  Preventing or minimising internal leakage of working-fluid, e.g. between stages (sealings in general F16J {; sealing arrangements for transition ducts of combustor cans F01D9/023}) · CPC title