Shroud cartridge having a ceramic matrix composite seal segment

Patent metadata

Field	Value
Publication number	US-10087770-B2
Application number	US-201514721620-A
Country	US
Kind code	B2
Filing date	May 26, 2015
Priority date	May 26, 2015
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

A shroud for radially encasing a turbine in a gas turbine engine is provided. The shroud comprises a carrier which defines a pin-receiving carrier bore, and a ceramic matrix composite (CMC) seal segment comprising an arcuate flange with a surface facing the turbine and a part that defines a pin-receiving seal segment bore. The seal segment bore is radially spaced from the arcuate flange by a spacing flange which extends radially outward from the arcuate flange to effect receipt within the seal segment bore of an elongated pin. The elongated pin extends through the carrier bore and the seal segment bore, and the elongated pin has a lateral cross-sectional dimension of at least three-eighths of an inch.

First claim

What is claimed is:

1. A segmented turbine shroud for radially encasing a turbine in a gas turbine engine, the shroud comprising:
a carrier comprising a portion defining a pin-receiving carrier bore;
a ceramic matrix composite (CMC) seal segment comprising an arcuate flange having a surface facing the turbine and a portion defining a pin-receiving seal segment bore;
an elongated pin extending through said carrier bore and said seal segment bore,
wherein said elongated pin comprises a lateral cross-sectional dimension of at least three-eighths inches; and
wherein said CMC seal segment portion defining the pin-receiving seal segment bore is radially spaced from said arcuate flange by a spacing flange extending radially outward from said arcuate flange to thereby effect receipt within the seal segment bore of said elongated pin, said spacing flange having an axial dimension and a circumferential dimension, wherein said axial dimension is greater than said circumferential dimension of said spacing flange.

2. The shroud of claim 1 wherein said elongated pin comprises a lateral cross-sectional dimension of at least one half inch.

3. The shroud of claim 2 wherein said elongated pin comprises a lateral cross-sectional dimension of at least five-eighths inches.

4. The shroud of claim 1 wherein said elongated pin comprises a minimum lateral cross-sectional dimension of at least three-eighths inches.

5. The shroud of claim 1 wherein said elongated pin comprises a circular lateral cross-section.

6. The shroud of claim 1 wherein said elongated pin is hollow.

7. The shroud of claim 1 wherein said elongated pin is formed as a spiral rolled pin.

8. The shroud of claim 1 wherein said carrier comprises a plurality of carrier segments, each carrier segment carrying a single CMC seal segment by one or more elongated pins to form a shroud cartridge.

9. The shroud of claim 1 wherein said seal segment bore comprises a lateral cross-sectional dimension that varies along the axial length of said bore.

10. The shroud of claim 1 wherein said seal segment bore comprises a lateral cross-sectional dimension of at least three-eighths inches.

11. The shroud of claim 10 wherein said seal segment bore comprises a lateral cross-sectional dimension of at least one half inch.

12. The shroud of claim 11 wherein said seal segment bore comprises a lateral cross-sectional dimension of at least five-eighths inches.

13. A segmented turbine shroud for radially encasing a turbine in a gas turbine engine, said shroud comprising a plurality of cartridges, one or more of said cartridges comprising:
a carrier segment comprising an axial flange and opposing lateral flanges extending radially inward from said axial flange, each lateral flange being generally planar and perpendicular to the rotational axis of the turbine, the opposing flanges defining a plurality of pairs of opposing pin-receiving carrier bores;
a ceramic matrix composite (CMC) seal segment comprising an arcuate flange having a surface facing the turbine and a plurality of radial flanges extending radially outward from said arcuate flange, each of said radial flanges defining a pin-receiving seal segment bore at the distal end thereof; and
a plurality of elongated pins having a lateral cross-sectional dimension of at least three-eighths inches,
wherein said seal segment bores are radially spaced from said arcuate flange by a spacing flange to a distance sufficient to define a bore comprising a lateral cross-sectional dimension large enough to receive one of said elongated pins therein, and said spacing flange extending radially outward from said arcuate flange to thereby effect receipt within the seal segment bore of said elongated pin, said spacing flange having an axial dimension and a circumferential dimension, wherein said axial dimension is greater than said circumferential dimension of said spacing flange, and
wherein said CMC seal segment is carried by said carrier segment by extending each of said elongated pins through a pair of opposing carrier bores and at least one of said seal segment bores.

14. The cartridge of claim 13 wherein each of said elongated pins is received in only a single seal segment bore.

15. The cartridge of claim 13 wherein said carrier segment further comprises a third lateral flange extending radially inward from said axial flange, said third lateral flange being generally planar and perpendicular to the rotational axis of the turbine and positioned intermediate said opposing lateral flanges, said third lateral flange defining a plurality of pin-receiving third carrier bores, each of said third carrier bores being axially aligned with the pair of opposing carrier bores,
wherein said CMC seal segment is carried by said carrier segment by extending each elongated pin through the pair of opposing carrier bores, a third carrier bore and a pair of axially aligned seal segment bores.

16. The cartridge of claim 13 wherein said elongated pins are hollow.

17. The cartridge of claim 13 comprising at least three pairs of opposing pin-receiving carrier bores and at least three seal segment bores.

18. The shroud of claim 1 wherein said elongated pin is formed as a spiral rolled pin.

Assignees

• Rolls Royce Corp
• Rolls Royce Nam Tech Inc
• Rolls Royce High Temperature Composites Inc

Inventors

• Vetters Daniel Kent
• Thomas David J
• Freeman Ted
• Dierksmeier Douglas David
• Shi Jun
• Engel Todd

Classifications

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• F01D9/04 Primary

  forming ring or sector · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/24

  for turbines · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title