Inter-turbine ducts

Patent metadata

Field	Value
Publication number	US-10294807-B2
Application number	US-201615159355-A
Country	US
Kind code	B2
Filing date	May 19, 2016
Priority date	May 19, 2016
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

An inter-turbine duct includes a first annular wall with a ceramic composite material and including a first plurality of layers and a second plurality of layers, the first plurality of layers including a slot extending therethrough; and a first vane with a material of a metal alloy or a ceramic material. The first vane has a first end and a flange extending through the slot with the flange extending away from the first end and being retained between the first plurality of layers and the second plurality of layers of the first annular wall.

First claim

What is claimed is:

1. An inter-turbine duct, comprising:
a first annular wall including a first plurality of layers and a second plurality of layers, each of the first plurality of layers and the second plurality of layers composed of a ceramic composite material, the first plurality of layers defining a slot that extends through the first plurality of layers;
a second annular wall including a plurality of layers and an opening defined through the plurality of layers; and
a first vane comprising a material selected from a group consisting of a metal alloy and a ceramic material, the first vane having a first end, a second end opposite the first end, a post that extends outwardly from the second end of the first vane and a flange that extends outwardly from the first end of the first vane, the flange extending through the slot defined in the first plurality of layers, the flange is retained between the first plurality of layers and the second plurality of layers of the first annular wall and the post of the second end of the first vane extends through the opening of the second annular wall such that a slip joint is formed between the post and the opening of the second annular wall.

2. The inter-turbine duct of claim 1 , wherein the first annular wall is an outer annular wall.

3. The inter-turbine duct of claim 1 , wherein the first annular wall is an inner annular wall.

4. The inter-turbine duct of claim 1 , wherein the first end of the first vane includes a post that extends from the flange, the second plurality of layers of the first annular wall defines an opening and the post extends through the opening defined in the second plurality of layers of the first annular wall and radially away from the first annular wall, the post configured to be received within a cylindrical space defined by a portion of an engine case.

5. The inter-turbine duct of claim 1 , wherein the first vane includes an internal cavity that extends from the first end of the first vane to the second end of the first vane, the internal cavity having an opening at the first end of the first vane, and the flange defines at least a portion of the first end of the first vane.

6. The inter-turbine duct of claim 5 , further comprising a retention insert disposed at least partially within the internal cavity of the first vane and extending through an opening defined in the second plurality of layers of the first annular wall.

7. The inter-turbine duct of claim 1 , wherein the first vane comprises a silicon carbide composite.

8. The inter-turbine duct of claim 1 , wherein the ceramic composite material comprises an aluminum oxide ceramic composite.

9. The inter-turbine duct of claim 1 , wherein the first vane includes a first edge extending between the first end and the second end, and a second edge opposite the first edge, the first vane having a length defined between the first edge and the second edge, the flange having a length that is less than the length of the first vane, and the length of the flange is greater than a length of the slot.

10. An inter-turbine duct comprising:
a first annular wall including a first plurality of layers and a second plurality of layers each comprising a first ceramic material, the first plurality of layers including a plurality of slots defined through the first plurality of layers;
a second annular wall comprising a plurality of layers composed of a second ceramic material and including a plurality of openings defined through the plurality of layers and extending between an inner surface and an outer surface of the second annular wall; and
a plurality of vanes extending between the first annular wall and the second annular wall, each vane comprising a material selected from a group consisting of a metal alloy and a ceramic material, each vane having a first end, a second end opposite the first end, and a flange, the second end of each vane having a post extending through a corresponding opening of the plurality of openings of the second annular wall such that a slip joint is formed between the post and the corresponding opening of the plurality of openings of the second annular wall, the flange of each vane extending through a corresponding slot of the plurality of slots, the flange of each vane extending away from the first end of a corresponding vane and being retained between the first plurality of layers and the second plurality of layers of the first annular wall.

11. The inter-turbine duct of claim 10 , wherein the first annular wall is an outer annular wall and the second annular wall is an inner annular wall.

12. The inter-turbine duct of claim 10 , wherein the first annular wall is an inner annular wall and the second annular wall is an outer annular wall.

13. The inter-turbine duct of claim 10 , wherein the first end of a vane of the plurality of vanes includes a post that extends from the flange, the second plurality of layers of the first annular wall defines an opening and the post extends through the opening of the second plurality of layers of the first annular wall and radially away from the first annular wall, the post configured to be received within a cylindrical space defined by a portion of an engine case.

14. The inter-turbine duct of claim 10 , wherein the vane includes an internal cavity that extends from the first end of the vane to the second end of the vane, the internal cavity having an opening at the first end of the vane and the flange defines at least a portion of the first end of the vane.

15. The inter-turbine duct of claim 14 , further comprising a retention insert disposed at least partially within the internal cavity of the vane and extending through an opening defined in the second plurality of layers of the first annular wall.

16. The inter-turbine duct of claim 10 , wherein the plurality of vanes comprise a silicon carbide composite.

17. The inter-turbine duct of claim 10 , wherein the first ceramic material comprises an aluminum oxide ceramic composite.

18. The inter-turbine duct of claim 10 , wherein the plurality of vanes comprise the metal alloy.

Assignees

• Honeywell Int Inc

Inventors

• Kington Harry Lester
• Neumann James

Classifications

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic

• C04B2237/365

  Silicon carbide · CPC title

• C04B2237/765

  at least one member being a tube · CPC title

• F01D9/041 Primary

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