Non-linearly deflecting brush seal land

Patent metadata

Field	Value
Publication number	US-9957825-B2
Application number	US-201615016007-A
Country	US
Kind code	B2
Filing date	Feb 4, 2016
Priority date	Oct 11, 2013
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

A brush seal land is disclosed. The brush seal land may comprise a first portion configured to be coupled to a turbine disc of an aircraft engine and a second portion having a contact surface. The brush seal land may comprise a concave annular structure. The second portion may deflect through a clearance area in response to contact with a brush. The second portion may not deflect in response to contact with a brush after the second portion has deflected through a clearance area in response to contact with the brush. The contact surface comprises tungsten carbide. The brush seal land may comprise INCONEL. The brush seal land may be configured to be coupled to an annular member extending from the turbine disc. The brush seal land may reduce abrasion to an annular member extending from the turbine disc by a brush.

First claim

What is claimed is:

1. A generally C-shaped brush seal land comprising:
a concave annular structure configured to rotate with a turbine disc;
a first portion of the concave annular structure configured to couple to an annular member extending from the turbine disc; and
a second portion of the concave annular structure radially opposing the first portion and configured to deflect towards the first portion to close a clearance area between the second portion and the turbine disc in response to contact with a brush seal,
wherein the second portion deflects through the clearance area in response to contact with the brush seal up to the point at which the second portion contacts the turbine disc, and does not deflect further due to contact between the second portion and the turbine disc.

2. The brush seal land of claim 1 , wherein the brush seal land comprises an austenitic nickel-chromium alloy.

3. The brush seal land of claim 1 , wherein the second portion includes a contact surface configured for contact with the brush.

4. The brush seal land of claim 3 , wherein the contact surface comprises tungsten carbide.

5. The brush seal land of claim 1 , wherein the brush seal land is configured to reduce abrasion to the annular member extending from the turbine disc.

6. The brush seal land of claim 1 , wherein the brush seal land is configured to be used with a brush of the brush seal to separate a high pressure zone from a low pressure zone.

7. The brush seal land of claim 1 , wherein the first portion is configured to be coupled to the turbine disc using pressure.

8. A brush seal comprising:
a generally C-shaped brush seal land configured to be coupled to an annular extending member from a turbine disc; and
a brush configured to make contact with the brush seal land, the brush seal land comprising:
a concave annular structure configured to rotate with a turbine disc;
a first portion of the concave annular structure configured to couple to an annular member extending from the turbine disc; and
a second portion of the concave annular structure radially opposing the first portion and configured to deflect towards the first portion to close a clearance area between the second portion and the turbine disc in response to contact with a brush seal,
wherein the second portion deflects through the clearance area in response to contact with the brush seal up to the point at which the second portion contacts the turbine disc, and does not deflect further due to contact between the second portion and the turbine disc.

9. The brush seal of claim 8 , wherein the brush seal is configured to deflect in response to contact with the brush seal land.

10. The brush seal of claim 8 , wherein the brush seal land comprises an austenitic nickel-chromium alloy.

11. The brush seal of claim 8 , wherein the brush seal land comprises a contact surface configured for contact with the brush.

12. The brush seal of claim 11 , wherein the contact surface comprises tungsten carbide.

13. The brush seal of claim 8 , wherein the brush seal land and the brush separate a high pressure zone from a low pressure zone.

14. The brush seal of claim 8 , wherein the first portion is coupled to the turbine disc by a pressure.

Assignees

• United Technologies Corp

Inventors

• Duong Loc Quang
• Hu Xiaolan

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F16J15/3288 Primary

  Filamentary structures, e.g. brush seals · CPC title

• F05D2240/56

  Brush seals · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic

• F01D11/00 Primary

  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