Composite retention feature

Patent metadata

Field	Value
Publication number	US-9506356-B2
Application number	US-201314094304-A
Country	US
Kind code	B2
Filing date	Dec 2, 2013
Priority date	Mar 15, 2013
Publication date	Nov 29, 2016
Grant date	Nov 29, 2016

Abstract

A retention feature for use in a gas turbine engine is disclosed herein. The retention feature includes a ceramic post, an insert, and a braze layer coupling the insert to the ceramic post. The ceramic post includes a body adapted to be coupled to a turbine engine component and a head coupled to the body. The insert is arranged in a space formed in the head and the braze layer extends from the ceramic post to the insert to bond the insert to the ceramic post.

First claim

What is claimed is:

1. A retention feature for use in a gas turbine engine comprising
a ceramic post including a body adapted to be coupled to a turbine engine component and a head coupled to the body, the head formed to include a space that forms a channel opening away from the body and extending through the head of the ceramic post,
a first insert arranged in the space,
a first braze layer extending from the ceramic post to the first insert to bond the first insert to the ceramic post,
a second insert arranged in the space, and
a second braze layer extending from the ceramic post to the second insert to bond the second insert to the ceramic post, wherein the second insert is spaced apart from the first insert,
wherein the first insert is sized to fill a portion of the channel along an axis of the channel, the second insert is sized to fill another portion of the channel along the axis of the channel, and the second insert is spaced apart from the first portion of the channel along the axis.

2. The retention feature of claim 1 , wherein the first insert is U-shaped and the second insert is U-shaped.

3. The retention feature of claim 1 , wherein the first braze layer includes silicon.

4. The retention feature of claim 3 , wherein the first braze layer includes a silicide.

5. The retention feature of claim 4 , wherein the silicide includes at least one of zirconium, molybdenum, hafnium, boron, and carbon.

6. The retention feature of claim 3 , wherein the first braze layer includes inert ceramic fibers.

7. The retention feature of claim 1 , wherein the ceramic post consists essentially of a ceramic matrix composite and includes carbon and silicon.

8. The retention feature of claim 1 , wherein the first insert consists essentially of a ceramic matrix composite.

9. The retention feature of claim 8 , wherein the first insert includes silicon and carbon.

10. The retention feature of claim 8 , wherein the first insert includes ceramic fiber fabric.

11. The retention feature of claim 8 , wherein the first insert includes chopped ceramic fibers.

12. The retention feature of claim 1 , wherein the body of the ceramic post has a proximal end coupled to an airfoil and a distal end coupled to the head and the airfoil includes a ceramic matrix material.

13. The retention feature of claim 1 , wherein the body of the ceramic post has a proximal end coupled to a turbine blade track runner and a distal end coupled to the head and the turbine blade track runner includes a ceramic matrix material.

14. A retention feature for use in a gas turbine engine comprising
a ceramic post including a body adapted to be coupled to a turbine engine component and a head coupled to the body, the head formed to include a space,
a first insert arranged in the space, and
a first braze layer extending from the ceramic post to the first insert to bond the first insert to the ceramic post,
wherein the first insert is U-shaped such that a gap exists between two opposed sides thereof.

15. A method of making a retention feature for use in a gas turbine engine comprising the steps of
manufacturing a composite post including a body and a head coupled to the body, the head formed to include a space that forms a channel opening away from the body and extending through the head of the ceramic post,
manufacturing a first insert,
arranging the first insert into the space formed in the head,
depositing a first braze layer between the head and the first insert to bond the first insert to the head,
manufacturing a second insert,
arranging the second insert in the space formed in the head at a location spaced apart from the first insert, and
depositing a first braze layer between the head and the second insert to bond the second insert to the head.

16. The method of claim 15 , wherein manufacturing the first insert includes (i) preforming at least one ceramic fiber sheet into a predetermined shape and (ii) densifying the at least one ceramic fiber sheet.

Assignees

• Rolls Royce Corp
• Rolls Royce Nam Tech Inc

Inventors

• Loftus Peter
• Chamberlain Adam L
• Freeman Ted J

Classifications

• G01P15/18

  in two or more dimensions · CPC title

• F01D9/04

  forming ring or sector · CPC title

• E21B47/007 Primary

  Measuring stresses in a pipe string or casing (for locating blocked portions of pipes E21B47/09) · CPC title

• Y10T29/49337

  Composite blade · CPC title

• F01D5/3007 Primary

  of axial insertion type · CPC title