SHROUD CARTRIDGE HAVING A CERAMIC MATRIX COMPOSITE SEAL SEGMENT

• US 20160348527A1
• Filed: 05/26/2015
• Published: 12/01/2016
• Est. Priority Date: 05/26/2015
• Status: Active Grant

• Current Assignee: Rolls-Royce Corporation (Rolls-Royce Holdings Plc), Rolls-Royce High Temperature Composites, Inc. (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce High Temperature Composites, Inc. (Rolls-Royce Holdings Plc)
• Inventors: Vetters, Daniel Kent, Thomas, David J., Freeman, Ted, Dierksmeier, Douglas David, Shi, Jun, Engel, Todd
• Granted Patent: US 10,087,770 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01D 11/08 for sealing space between rotor blade tips and stator specially-shaped blade tips therefor F01D5/20
• CPC Class Codes: F01D 25/005 Selecting particular materials
• CPC Class Codes: F01D 25/243 Flange connections; Bolting arrangements F01D25/265 takes precedence
• CPC Class Codes: F01D 25/246 Fastening of diaphragms or stator-rings
• CPC Class Codes: F01D 9/04 forming ring or sector
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2240/11 Shroud seal segments
• CPC Class Codes: F05D 2240/24 for turbines
• CPC Class Codes: F05D 2240/55 Seals
• CPC Class Codes: F05D 2300/6033 Ceramic matrix composites [CMC]

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.

Claims

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 a 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.

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 comprises a lateral cross-sectional dimension that varies along the length of said pin.

8. The shroud of claim 7 wherein said elongated pin comprises a circular cross-section having a minimum diameter proximate each end of said elongated pin and a maximum diameter proximate the longitudinal center of said pin.

9. The cartridge of claim 7 wherein said elongated pin comprises a circular lateral cross-section with a maximum diameter proximate each end of said pin and a minimum diameter proximate the longitudinal center of said pin.

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

11. 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.

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

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

14. The shroud of claim 13 wherein said seal segment bore comprises a lateral cross-sectional dimension of at least one half inch.

15. The shroud of claim 14 wherein said seal segment bore comprises a lateral cross-sectional dimension of at least five-eighths inches.

16. 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 a distance sufficient to define a bore comprising a lateral cross-sectional dimension large enough to receive one of said elongated pins therein, 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.

17. The cartridge of claim 16 wherein each of said elongated pins is received in only a single seal segment bore.

18. The cartridge of claim 16 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 a pair of opposing carrier bores,

wherein said CMC seal segment is carried by said carrier segment by extending each elongated pin through a pair of opposing carrier bores, a third carrier bore and a pair of axially aligned seal segment bores.

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

20. The cartridge of claim 16 comprising at least three pairs of opposing pin-receiving carrier bores and at least three seal segment bores.