Skirted leaf seal apparatus

Patent metadata

Field	Value
Publication number	US-11719191-B2
Application number	US-202117352605-A
Country	US
Kind code	B2
Filing date	Jun 21, 2021
Priority date	Jun 21, 2021
Publication date	Aug 8, 2023
Grant date	Aug 8, 2023

Abstract

In some embodiments, apparatuses are provided herein useful to sealing a gap between a movable flap and a stationary structure, such as a gap between a gas turbine engine nozzle flap and a corresponding sidewall. An apparatus for sealing such a gap may be a dynamic skirted leaf seal which may include a flap arm and a wall arm opposite the flap arm. A distal end portion of the flap arm may comprise a first skirt and the distal end portion of the wall arm may comprise a second skirt that engages the first skirt. When positioned in a gap between the movable flap and the stationary structure, the skirted leaf seal may exert a force to urge the flap arm towards the flap and to urge the wall arm towards the structure to seal the gap.

First claim

What is claimed is:

1. A seal apparatus for sealing a gap between a movable flap and a stationary structure, the seal apparatus comprising:
a first seal having a first proximal end portion, a first distal end portion with a first bend, and a first skirt extending away from the first bend; and
a second seal having a second proximal end portion, a second distal end portion with a second bend, and a second skirt extending away from the second bend, the second seal opposite the first seal and forming an interior space therebetween,
wherein the first seal biases away from the second seal to seal the gap, and wherein the first skirt engages the second skirt at a first surface of contact to seal the interior space.

2. The seal apparatus of claim 1 , wherein the first seal and the second seal are a single piece of material.

3. The seal apparatus of claim 1 , wherein the first seal and the second seal are flexurally related such that the first seal and the second seal have a predetermined movement.

4. The seal apparatus of claim 1 , wherein the first proximal end portion is coupled to the second proximal end portion at a connecting portion.

5. The seal apparatus of claim 4 , wherein an attachment member rotatably attaches the connecting portion to the stationary structure such that the connecting portion is able to rotate about the attachment member.

6. The seal apparatus of claim 1 , wherein the first bend engages the movable flap at a second surface of contact, the second surface of contact sealing a space between the first seal and the movable flap.

7. The seal apparatus of claim 6 , wherein the second bend engages the stationary structure at a third surface of contact, the third surface of contact sealing a space between the second seal and the stationary structure.

8. The seal apparatus of claim 1 , wherein the first seal and the second seal are in sliding contact at the first surface of contact.

9. The seal apparatus of claim 1 , wherein the first seal and the second seal include a common attachment for mounting the first seal and the second seal for relative rotation, and wherein the first seal is a first elongate sheet and the second seal is a second elongate sheet.

10. The seal apparatus of claim 1 , wherein the first surface of contact seals the interior space between the second seal and the first seal.

11. A gas turbine nozzle, comprising:
a stationary sidewall;
a movable flap adjacent the stationary sidewall; and
a seal apparatus disposed between the stationary sidewall and the movable flap to seal a gap between the stationary sidewall and the movable flap, the seal apparatus operably coupled to the movable flap and comprising:
a first seal having a first proximal end portion, a first distal end portion with a first bend, and a first skirt extending away from the first bend; and
a second seal having a second proximal end portion, a second distal end portion with a second bend, and a second skirt extending away from the second bend, the second seal opposite the first seal and forming an interior space therebetween, wherein the first seal biases away from the second seal to seal the gap, and wherein the first skirt engages the second skirt at a first surface of contact to seal the interior space.

12. The gas turbine nozzle of claim 11 , wherein the seal apparatus exerts a force to urge the first seal towards the movable flap and to urge the second seal towards the stationary sidewall to seal the gap.

13. The gas turbine nozzle of claim 11 , wherein the first seal and the second seal are a single piece of material.

14. The gas turbine nozzle of claim 11 , wherein the first seal and the second seal include a common attachment for mounting the first seal and the second seal for relative rotation, and wherein the seal apparatus is operably coupled to the movable flap via a housing, the housing comprising a cantilever coupled to the common attachment.

15. The gas turbine nozzle of claim 14 , wherein the cantilever counteracts a core pressure of the gas turbine nozzle.

16. The gas turbine nozzle of claim 11 , wherein the first proximal end portion and the second proximal end portion are coupled together at a connecting portion, and wherein an attachment member rotatably attaches the connecting portion to the stationary sidewall such that the connecting portion is able to rotate about the attachment member.

17. A method of sealing using a seal apparatus, the seal apparatus comprising: a first seal having a first proximal end portion and a first distal end portion with a first skirt extending from the first distal end portion; and a second seal having a second proximal end portion and a second distal end portion with a second skirt extending from the second distal end portion, the second seal opposite the first seal and forming an interior space therebetween, wherein the first seal biases away from the second seal to seal a gap, the method comprising:
contacting at least two surfaces of the gap with the first distal end portion and the second distal end portion;
moving automatically at least the second distal end portion relative to one of the at least two surfaces in response to the gap changing size; and
engaging automatically the first skirt with the second skirt at a first surface of contact between the first skirt and second skirt to seal the interior space.

18. The method of claim 17 , wherein the method seals the gap using at least two seal apparatuses.

19. The method of claim 17 , further wherein the first proximal end portion and the second proximal end portion are coupled together at a connecting portion, and wherein an attachment member rotatably attaches the connecting portion to one of the at least two surfaces, and rotating the connecting portion about the attachment member in response to a force applied to the seal apparatus by at least one of the at least two surfaces.

20. The method of claim 19 , wherein the attachment member is a knuckle or a hollow tube.

Assignees

• Gen Electric

Inventors

• Shealy James
• Corsmeier Donald M

Classifications

• F05D2260/52

  involving springs · CPC title

• F05D2260/38

  by a spring, i.e. spring loaded or biased towards a certain position · CPC title

• F02K1/805 Primary

  Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps · CPC title

• F02K1/1207 Primary

  of one series of flaps hinged at their upstream ends on a fixed structure (F02K1/1215 - F02K1/1292 take precedence) · CPC title

• F05D2240/57

  Leaf seals · CPC title