Assembly for sealing a gap between components of a turbine engine

Patent metadata

Field	Value
Publication number	US-10196911-B2
Application number	US-201414775412-A
Country	US
Kind code	B2
Filing date	Mar 14, 2014
Priority date	Mar 14, 2013
Publication date	Feb 5, 2019
Grant date	Feb 5, 2019

Abstract

A turbine engine assembly includes a first component, a second component and a third component arranged along an axis. The first component houses at least a portion of the third component. The assembly also includes a seal carrier, a seal land and a seal element, which seals a gap between the seal carrier and the seal land. The seal carrier is connected to the first component, and includes a groove surface and a groove. A first portion of the seal carrier seals a gap between a second portion of the seal carrier and the second component. The seal land is connected to the third component and includes a seal land surface. The seal element extends radially into the groove. The seal element is axially engaged with the groove surface and radially engaged with the seal land surface.

First claim

What is claimed is:

1. An assembly for a turbine engine, comprising:
a turbine engine first component, a turbine engine second component and a turbine engine third component arranged along an axis, the first component housing at least a portion of the third component;
a seal carrier connected to the first component and including a groove surface and a groove, wherein a first portion of the seal carrier at least partially seals a gap between a second portion of the seal carrier and the second component;
a seal land connected to the third component and including a seal land surface; and
a seal element extending radially into the groove and at least partially sealing a gap between the seal carrier and the seal land, wherein the seal element is axially engaged with the groove surface and radially engaged with the seal land surface;
wherein the seal element comprises a piston seal.

2. The assembly of claim 1 , wherein the first portion of the seal carrier is located radially within and axially overlaps the second component.

3. The assembly of claim 2 , wherein the first portion of the seal carrier radially engages the second component.

4. The assembly of claim 2 , wherein
the second component includes a first surface;
the first portion of the seal carrier extends radially outward to a second surface that axially overlaps the first surface; and
a control gap is defined radially between the first surface and the second surface.

5. The assembly of claim 2 , further comprising a second seal element radially engaged between the second component and the first portion of the seal carrier.

6. The assembly of claim 5 , wherein the second seal element comprises an annular seal device.

7. The assembly of claim 5 , wherein the seal carrier includes one or more retainers that axially locate the second seal element relative to the portion of the seal carrier.

8. The assembly of claim 2 , wherein
the seal carrier includes a base and a flange;
the base includes the second portion of the seal carrier and the groove surface; and
the flange extends axially from the base, and includes the first portion of the seal carrier.

9. The assembly of claim 1 , wherein the seal carrier includes a base that extends radially inwards from the first component to an inner side, and the groove extends radially into the base from the inner side.

10. The assembly of claim 1 , wherein
the seal carrier includes a base and a cantilevered leg that connects to the base to the first component;
the base and the cantilevered leg define a channel, and the base defines the groove; and
the channel extends axially into the seal carrier to the cantilevered leg, and radially within the seal carrier between the base and the cantilevered leg.

11. The assembly of claim 1 , wherein the seal carrier is attached to the first component.

12. The assembly of claim 1 , wherein the seal carrier is formed integral with the first component.

13. The assembly of claim 1 , wherein
the first component comprises a turbine engine case;
the third component comprises a guide vane arrangement that includes an outer platform; and
the seal land is connected to the outer platform.

14. The assembly of claim 13 , wherein the second component comprises a blade outer air seal.

15. The assembly of claim 1 , further comprising:
a turbine engine case attached to the first component and housing at least a portion of the second component;
wherein a first plenum extends radially between the first component and the third component, and a second plenum extends radially between the turbine engine case and the second component; and
wherein the seal carrier includes one or more passages that direct air between the first plenum and the second plenum.

16. The assembly of claim 1 , further comprising:
a turbine engine case attached to the first component and housing at least a portion of the second component;
wherein a first plenum extends radially between the first component and the third component, and a second plenum extends radially between the turbine engine case and the second component; and
wherein the first component includes one or more passages that direct air between the first plenum and the second plenum.

17. The assembly of claim 1 , wherein the groove surface is configured perpendicular to the axis.

18. The assembly of claim 1 , wherein the seal element comprises a surface that is perpendicular to the axis.

19. An assembly for a turbine engine, comprising:
a case, a turbine engine component and a guide vane arrangement arranged along an axis, the case housing at least a portion of the guide vane arrangement;
a seal carrier connected to the case and including a first side groove surface and a second side groove surface that at least partially define a groove, wherein a portion of the seal carrier sealingly engages the turbine engine component, and the first and second groove surfaces are each perpendicular to the axis;
a seal land connected to the guide vane arrangement and including a seal land surface; and
a seal element extending radially into the groove and at least partially sealing a gap between the seal carrier and the seal land, wherein the seal element is axially engaged with the first side groove surface and radially engaged with the seal land surface.

20. The assembly of claim 19 , wherein the seal element is configured as a piston seal.

Assignees

• United Technologies Corp
• United Technologies Corp

Inventors

• Jenkins Decari S
• Farah Jorge I

Classifications

• F01D11/005 Primary

  Sealing means between non relatively rotating elements · CPC title

• F01D11/08

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title

• F05D2240/58

  Piston ring seals · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2220/30

  in turbines · CPC title