Segmented annular seal

Patent metadata

Field	Value
Publication number	US-10082039-B2
Application number	US-201615341598-A
Country	US
Kind code	B2
Filing date	Nov 2, 2016
Priority date	Nov 2, 2016
Publication date	Sep 25, 2018
Grant date	Sep 25, 2018

Abstract

An annular seal includes an annular outer casing, a plurality of seal segments, and a plurality of spring components. The plurality of seal segments is coupled to the annular outer casing to cumulatively form an annular sealing surface, the annular sealing surface is configured to face a rotating structure to inhibit fluid leakage between the rotating structure and the annular sealing surface, and each seal segment of the plurality of seal segments is configured for independent radial movement relative to other seal segments of the plurality of seal segments. In various embodiments, the plurality of spring components are configured to bias the plurality of seal segments relative to the radial movement.

First claim

What is claimed is:

1. An annular seal comprising:
an annular outer casing comprising a flange and a portion defining a plurality of radially extending mount holes;
a plurality of seal segments, wherein:
the plurality of seal segments is coupled to the annular outer casing to cumulatively form an annular sealing surface, wherein each seal segment of the plurality of seal segments comprises a trunnion, wherein the trunnion of each seal segment of the plurality of seal segments is configured to be received within a respective one of the plurality of radially extending mount holes;
the annular sealing surface is configured to face a rotating structure to inhibit fluid leakage between the rotating structure and the annular sealing surface; and
each seal segment of the plurality of seal segments is configured for independent radial movement relative to other seal segments of the plurality of seal segments; and

a plurality of spring components configured to bias the plurality of seal segments relative to the radial movement, wherein the plurality of spring components are disposed at least one of forward of and aft of the portion of the annular outer casing such that the plurality of spring components are disposed outside of the plurality of radially extending mount holes.

2. The annular seal of claim 1 , wherein the trunnion of each seal segment of the plurality of seal segments is configured to slide within a respective one of the plurality of radially extending mount holes.

3. The annular seal of claim 1 , wherein the plurality of radially extending mount holes are cylindrical and the trunnion of each seal segment of the plurality of seal segment is cylindrical.

4. The annular seal of claim 1 , wherein the plurality of spring components are independent of and separable from the plurality of seal segments.

5. The annular seal of claim 1 , wherein the plurality of spring components comprises two spring components per seal segment of the plurality of seal segments.

6. The annular seal of claim 5 , wherein the two spring components comprise a forward spring component and an aft spring component.

7. The annular seal of claim 6 , wherein the forward spring component and the aft spring component are coupled to the flange of the annular outer casing and to a radially outer surface of each seal segment of the plurality of seal segments.

8. The annular seal of claim 1 , wherein the plurality of spring components are positioned against at least one of a forward side and an aft side of the portion of the annular outer casing.

9. The annular seal of claim 8 , further comprising a support ring configured to hold the plurality of spring components between the support ring and at least one of the forward side and the aft side of the portion of the annular outer casing.

10. The annular seal of claim 1 , wherein each spring component of the plurality of spring components comprises opposing segments and integral stops, wherein the integral stops are configured to engage each other to limit radially outward movement and are configured to engage the opposing segments to limit radially inward movement.

11. A gas turbine engine comprising:
a rotating structure;
an annular outer casing comprising a flange and a portion defining a plurality of radially extending mount holes;
a plurality of seal segments, wherein:
the plurality of seal segments is coupled to the annular outer casing to cumulatively form an annular sealing surface, wherein each seal segment of the plurality of seal segments comprises a trunnion, wherein the trunnion of each seal segment of the plurality of seal segments is configured to be received within a respective one of the plurality of radially extending mount holes;
the annular sealing surface is configured to face the rotating structure to inhibit fluid leakage between the rotating structure and the annular sealing surface; and
each seal segment of the plurality of seal segments is configured for independent radial movement relative to other seal segments of the plurality of seal segments; and

a plurality of spring components configured to bias the plurality of seal segments relative to the radial movement, wherein the plurality of spring components are disposed at least one of forward of and aft of the portion of the annular outer casing such that the plurality of spring components are disposed outside of the plurality of radially extending mount holes.

12. The gas turbine engine of claim 11 , wherein the rotating structure is a rotating shaft of the gas turbine engine.

13. The gas turbine engine of claim 11 , wherein the rotating structure is a series of airfoil rotors of the gas turbine engine.

14. The gas turbine engine of claim 11 , wherein the annular outer casing is coupled to at least one of a fan section, a compressor section, and a turbine section of the gas turbine engine.

15. A method of manufacturing an annular seal, the method comprising:
forming a plurality of seal segments;
forming a plurality of spring components that are independent of and separable from the plurality of seal segments;
coupling the plurality of seal segments to an annular outer casing such that the plurality of seal segments cumulatively forms an annular sealing surface, wherein the annular outer casing comprises a flange and a portion defining a plurality of radially extending mount holes, wherein each seal segment of the plurality of seal segments comprises a trunnion, wherein coupling the plurality of seal segments to the annular outer casing comprises inserting the trunnion of each seal segment of the plurality of seal segments into a respective one of the plurality of radially extending mount holes; and
coupling the plurality of spring components to the plurality of seal segments and the annular outer casing, wherein the plurality of spring components are disposed at least one of forward of and aft of the portion of the annular outer casing such that the plurality of spring components are disposed outside of the plurality of radially extending mount holes.

16. The method of claim 15 , wherein coupling the plurality of seal segments to the annular outer casing comprises inserting trunnions of the plurality of seal segments into radially extending mount holes of the annular outer casing.

17. The method of claim 15 , wherein coupling the plurality of spring components to the plurality of seal segments comprises coupling a forward spring component and an aft spring component, of the plurality of spring components, to a forward portion of each spring component and an aft portion of each spring component, respectively, of the plurality of spring components.

18. The gas turbine engine of claim 11 , wherein:
the plurality of spring components comprises two spring components per seal segment of the plurality of seal segments;
the two spring components comprise a forward spring component and an aft spring component; and
the forward spring component and the aft spring component are coupled to the flange of the annular outer casing and to a radially outer surface of each seal segment of the plurality of seal segments.

19. The gas turbine engine of claim 11 , wherein:
the plurality of spring components are positioned against at least one of a forward side and an aft side of the portion of the annular outer casing; and
the gas turbine engine further comprises a support ring configured to hold the plurality of spring components between the support ring and at least one of the forward side and the aft side of the portion of the annular outer casing.

Assignees

• United Technologies Corp

Inventors

• Hanson Russell B

Classifications

• F04D29/32

  for axial flow pumps · 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

• F04D29/053

  Shafts · CPC title

• F16J15/447

  Labyrinth packings · CPC title

• F16J15/442

  segmented · CPC title