Boas segmented heat shield

Patent metadata

Field	Value
Publication number	US-10138750-B2
Application number	US-201615071439-A
Country	US
Kind code	B2
Filing date	Mar 16, 2016
Priority date	Mar 16, 2016
Publication date	Nov 27, 2018
Grant date	Nov 27, 2018

Abstract

A seal assembly includes a seal arc segment defining first and second seal supports with a carriage defining first and second support members. The first support member supports the seal arc segment in a first ramped interface, and the second support member supports the seal arc segment in a second ramped interface. A spring is configured to bias the seal arc segment axially. A heat shield is radially inward of the spring.

First claim

What is claimed is:

1. A seal assembly, comprising:
a seal arc segment defining first and second seal supports;
a carriage defining first and second support members, the first support member supporting the seal arc segment in a first ramped interface and the second support member supporting the seal arc segment in a second ramped interface;
a spring configured to bias the seal arc segment axially; and
a heat shield radially inward of the spring and having a radially-extending leg disposed axially between the spring and the seal arc segment.

2. The seal assembly as recited in claim 1 , wherein the spring is configured to bias the seal arc segment axially toward the carriage.

3. The seal assembly as recited in claim 1 , wherein the seal arc segment has a circumferential length, and the heat shield extends circumferentially substantially the circumferential length of the seal arc segment.

4. The seal assembly as recited in claim 1 , wherein the heat shield includes a first axially-extending leg radially inward of the spring.

5. The seal assembly as recited in claim 4 , wherein the heat shield includes a radially outer end with a second axially-extending leg.

6. The seal assembly as recited in claim 5 , wherein the axially-extending leg radially inward of the spring extends in a first axial direction and the second axially-extending leg extends in a second axial direction opposite from the first axial direction.

7. The seal assembly as recited in claim 5 , wherein the second axially-extending leg is disposed radially outward of the seal arc segment.

8. The seal assembly as recited in claim 1 , the seal arc segment having first and second axial ends, the spring adjacent the first axial end and configured to bias the second axial end against the carriage.

9. The seal assembly as recited in claim 1 , wherein the heat shield is a first material, and the carriage is a second material different from the first material.

10. The seal assembly as recited in claim 1 , wherein
the carriage and the spring define a first cavity,
the heat shield and the spring define a second cavity, and
the spring includes a passage configured to provide communication between the first cavity and the second cavity.

11. The seal assembly as recited in claim 1 , wherein the radially-extending leg interfaces with a portion of a surface of a sidewall of the seal arc segment axially opposite the sidewall from a second surface interior to a pocket of the seal arc segment.

12. A gas turbine engine, comprising:
a rotor rotatable about an axis;
a seal arc segment radially outward of the rotor defining first and second seal supports;
a carriage defining first and second support members, the first support member supporting the seal arc segment in a first ramped interface and the second support member supporting the seal arc segment in a second ramped interface;
a spring configured to bias the seal arc segment axially; and
a heat shield radially inward of the spring and having a radially-extending leg disposed axially between the spring and the seal arc segment.

13. The gas turbine engine as recited in claim 12 , wherein the heat shield includes an axially-extending leg radially inward of the spring.

14. The gas turbine engine as recited in claim 13 , further comprising:
a vane structure spaced axially from the rotor, wherein the axially-extending leg extends axially in the axial space between the vane structure and the rotor.

15. The gas turbine engine as recited in claim 11 , wherein the spring is configured to bias the seal arc segment axially toward the carriage.

16. The gas turbine engine as recited in claim 11 , wherein the seal arc segment has a circumferential length, and the heat shield extends circumferentially substantially the circumferential length of the seal arc segment.

17. The gas turbine engine as recited in claim 11 , wherein
the carriage and the spring define a first cavity,
the heat shield and the spring define a second cavity, and
the spring includes a passage configured to provide communication between the first cavity and the second cavity.

18. A method of assembling a seal assembly, comprising:
providing a seal arc segment, the seal arc segment defining first and second seal supports;
supporting the seal arc segment on a carriage defining first and second support members, the first support member supporting the seal arc segment in a first ramped interface and the second support member supporting the seal arc segment in a second ramped interface;
biasing the seal arc segment axially with a spring; and
providing a heat shield radially inward of the spring and having a radially-extending leg disposed axially between the spring and the seal arc segment.

19. The method as recited in claim 18 , wherein the heat shield includes an axially-extending leg radially inward of the spring.

20. The method as recited in claim 18 , further comprising:
providing fluid to a cavity between the spring and the radially extending leg to pressurize the cavity.

Assignees

• United Technologies Corp

Inventors

• Mccaffrey Michael G
• Hagan Benjamin F
• Griffin David Richard

Classifications

• F05D2260/231

  Preventing heat transfer · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/08

  Cooling (of machines or engines in general F01P); Heating; Heat-insulation (of blade-carrying members, of blades F01D5/00) · CPC title