Seal land with air injection for cavity purging

Patent metadata

Field	Value
Publication number	US-9803503-B2
Application number	US-201213438871-A
Country	US
Kind code	B2
Filing date	Apr 4, 2012
Priority date	Jul 24, 2006
Publication date	Oct 31, 2017
Grant date	Oct 31, 2017

Abstract

An exhaust liner assembly including an interface between moveable parts includes a seal liner having a plurality of slots. The size of each slot varies with the circumferential position of the liner assembly to provide a stable cavity pressure within the interface to create a stable barrier about the entire circumference of the exhaust liner assembly.

First claim

What is claimed is:

1. A seal land comprising:
a plurality of inlets that supply an airflow through the seal land, wherein the plurality of inlets define a varying flow area dependent on a circumferential position to provide circumferentially varying flow field that changes based on a circumferential location; and
an injection guide in communication through a flow path with the plurality of inlets, the injection guide defining an outlet for airflow exiting the seal land.

2. The seal land as recited in claim 1 , wherein the plurality of inlets vary in size to provide the opening for airflow that varies dependent on a circumferential position.

3. The seal land as recited in claim 1 , wherein the plurality of openings vary in number dependent on a circumferential position to provide the opening for airflow that varies dependent on a circumferential position.

4. The seal land as recited in claim 1 , wherein the plurality of openings are disposed on an inner periphery of the seal land and the airflow varies with a position of the opening along the inner periphery.

5. The seal land as recited in claim 2 , wherein the plurality of inlets vary in size in at least two of a plurality of circumferential locations.

6. The seal land as recited in claim 3 , wherein the circumferential locations of the plurality of openings are grouped unequally about the seal land for controlling airflow into an axial gap.

7. The seal land as recited in claim 6 , wherein the size of the plurality of openings varies to provide a desired pressure that varies depending on the circumferential location.

8. The seal land as recited in claim 1 , wherein the injection guide is disposed radially inward of the plurality of inlets.

9. The seal land as recited in claim 8 , including a spacer disposed at the outlet of the injection guide that defines an opening for airflow exiting the seal land.

10. The seal land as recited in claim 1 , wherein the plurality of inlets comprise separate openings defined about the circumference of the seal land.

11. The seal land as recited in claim 10 , including a plurality of fastener lands disposed between the plurality of inlets.

12. The seal land as recited in claim 11 , wherein a number of the plurality of inlets disposed between the plurality of fastener lands varies based on a circumferential position.

13. The seal land as recited in claim 2 , wherein the plurality of inlets is defined as a slot including a circumferential width, the circumferential width varying based on a circumferential position.

14. The seal land as recited in claim 1 , wherein the seal land is disposed within a liner assembly and the airflow is directed into a gap defined by the liner assembly.

Assignees

• Lavin Jeffrey R
• Murphy Michael J
• United Technologies Corp

Inventors

• Lavin Jeffrey R
• Murphy Michael J

Classifications

• F01D25/30 Primary

  Exhaust heads, chambers, or the like · CPC title

• F02K1/822

  Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors · CPC title

• F01D25/12

  Cooling · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic