Liner assembly for gas turbine combustor

• US 4,413,477 A
• Filed: 12/29/1980
• Issued: 11/08/1983
• Est. Priority Date: 12/29/1980
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: White, Loren H., Dean, Gilbert J.
• Primary Examiner(s): Croyle, Carlton R.
• Assistant Examiner(s): Thorpe, Timothy S.
• Application Number:
  US06/220,272
• Time in Patent Office: 1,044 Days
• Field of Search: 60/322, 60/39.32, 60/752, 60/755, 60/756, 60/757, 431/352, 138/109, 138/178, 138/44
• US Class Current: 60/757
• CPC Class Codes: F23R 3/002 Wall structures F23R3/02 and F23R3/007 take precedence
• CPC Class Codes: F23R 3/42 characterised by the arrangement or form of the flame tubes or combustion chambers
• CPC Class Codes: F23R 3/60 Support structures; Attaching or mounting means

Abstract

A liner assembly for a combustor used in connection with a gas turbine is disclosed. The liner assembly comprises a double-wall structure including an outer structural shell and a separate throat insert coupled to and situated in the shell. The throat insert has a reduced throat section which divides the outer shell into upstream and downstream chambers. The upstream end of the throat insert is flexibly coupled in a stationary position to the outer shell by integral fingers and the downstream end is flexibly coupled to the outer shell, preferably by an air seal incorporating a plurality of flexible fingers located at the downstream end of the throat insert.

Claims

1. A liner assembly for a combustor used in connection with a gas turbine, said liner assembly comprising:

an outer structural shell;

a separate throat insert flexibly coupled to and situated in said outer shell;

said throat insert including a reduced throat section effective to divide said outer shell into an upstream chamber and a downstream chamber;

a plurality of upstream fingers defined by a plurality of slots in an upstream end of said throat insert;

means for connecting each of said upstream fingers to said outer shell; and

a plurality of downstream fingers on a downstream end of said throat insert, said downstream fingers including means for coupling said downstream end to said outer shell.

2. A liner assembly according to claim 1 wherein at least one of said upstream or said downstream fingers is rigidly connected to said outer shell.

3. A liner assembly according to claim 2 wherein the other of said upstream or downstream fingers includes slidable connection to said outer shell.

4. A liner assembly according to claim 1 wherein said upstream and downstream fingers are effective to flexibly couple said throat insert to said outer shell.

5. A liner assembly according to claim 1 wherein said means for coupling said downstream fingers includes slidable means for coupling to said outer shell.

6. A liner assembly according to claim 5 wherein said slidable means includes a pre-stressed condition in said downstream fingers effective to bias said downstream fingers outward against said outer shell.

7. A liner assembly according to claim 6 wherein all of said downstream fingers are integrally formed.

8. A liner assembly according to claim 7 wherein each of said downstream fingers is part of a continuous metal sheet.

9. A liner assembly according to claim 8 wherein each of said downstream fingers is defined by respective adjacent slots formed in said continuous metal sheet.

10. A liner assembly according to claim 9 wherein said continuous metal sheet is welded to said throat insert by a plurality of welds.

11. A liner assembly according to claim 10 wherein said slots are aligned with said welds such that a supply of cooling air can pass through said slots and over said welds.

12. A liner assembly according to claim 9 wherein a downstream end of said throat insert includes a plurality of convolutions formed therein and said metal sheet and said fingers cooperate with said convolutions to define a plurality of air flow metering passages.

13. A liner assembly according to claim 11 wherein said throat insert is effective to form a toroidal space between said throat insert and said outer shell and said slots in said continuous metal sheet are effective to pass cooling air from said toroidal space into said downstream chamber.

14. A liner assembly according to claim 12 wherein said throat insert is effective to form a toroidal space between said throat insert and said outer shell and said slots in said continuous metal sheet are effective to pass cooling air from said toroidal space into said downstream chamber via said air metering passages.

15. A liner assembly according to claim 1 wherein said throat insert is effective to form a toroidal space between said throat insert and said outer shell and said plurality of slots in said upstream end being effective to pass cooling air from said toroidal space to said upstream chamber.