Gas-path leakage seal for a gas turbine

• US 5,657,998 A
• Filed: 12/14/1995
• Issued: 08/19/1997
• Est. Priority Date: 09/19/1994
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Maynard, James Robert, Bagepalli, Bharat Sumpathkumar, Dinc, Osman Saim, Cromer, Robert Harold
• Primary Examiner(s): Cummings, Scott
• Application Number:
  US08/572,355
• Time in Patent Office: 614 Days
• Field of Search: 277/230, 277/229, 277/215, 277/217, 277/232, 277/233, 277/236, 415/139, 415/191, 285/336
• US Class Current: 277/653
• CPC Class Codes: F01D 11/005 Sealing means between non relatively rotating elements
• CPC Class Codes: F16J 15/022 characterised by structure or material
• CPC Class Codes: F16J 15/0812 with a braided or knitted body
• CPC Class Codes: F16J 15/104 characterised by structure
• CPC Class Codes: F16J 15/121 with metal reinforcement
• CPC Class Codes: Y10S 277/916 Seal including vibration dampening feature
• CPC Class Codes: Y10S 277/937 Glass particles or filament

Abstract

A gas-path leakage seal for generally sealing a gas-path leakage-gap between spaced-apart first and second members of a gas turbine (such as first and second segments of a gas turbine combustor casing). The seal includes a generally imperforate foil-layer assemblage which is generally impervious to gas, is located in the leakage-gap, is spaced apart from the first member, and has a first foil layer. The seal also includes a cloth-layer assemblage contacting the first member and having a first cloth layer generally enclosing and generally enclosingly-contacting the foil-layer assemblage. The first foil layer is made from a metal, ceramic, and/or polymer. The first cloth layer is made from metal, ceramic, and/or polymer fibers. The foil assemblage provides for sealing and flexibility, and the cloth assemblage provides for wear resistance and flexibility. The seal accommodates different surface shapes, assembly misalignment, vibration, and differential thermal growth of the gas turbine members.

Claims

1. A gas-path leakage seal for generally sealing a gas-path leakage-gap between spaced-apart first and second members of a gas turbine, said seal comprising:

a) a generally imperforate foil-layer assemblage consisting essentially of material selected from the group consisting of metals, ceramics, and polymers, generally impervious to gas, disposed in said gas-path leakage-gap, spaced apart from said first member, having a foil-assemblage edge and generally opposing first and second foil-assemblage outer surfaces extending to said foil-assemblage edge, and having a first foil layer wherein said first foil layer has a lengthwise direction and wherein a cross section of said first foil layer normal to said lengthwise direction does not itself completely enclose other structure; and

b) a woven, non-impregnated, cloth-layer assemblage generally pervious to gas, contacting said first member, and having a first cloth layer covering and contacting generally the entire first foil-assemblage outer surface, and covering and contacting generally the entire second foil-assemblage outer surface, wherein said foil-layer assemblage consists essentially of material selected from the group consisting of metals, ceramics, and polymers, and wherein said first cloth layer covers generally the entire foil-assembly edge.

2. The seal of claim 1, wherein said cloth-layer assemblage includes a cloth-assemblage edge and two generally opposing cloth-assemblage outer surfaces joined at said cloth-assemblage edge, and wherein said two generally opposing cloth-assemblage outer surfaces contact said first member proximate said cloth-assemblage edge.

3. The seal of claim 1, wherein said cloth-layer assemblage includes a cloth-assemblage edge and two generally opposing cloth-assemblage outer surfaces joined at said cloth-assemblage edge, and wherein said cloth-assemblage edge contacts said first member.

4. The seal of claim 1, wherein said foil-layer assemblage is spaced apart from said second member, and wherein said cloth-layer assemblage contacts said second member.

5. The seal of claim 1, wherein said cloth-layer assemblage includes a second cloth layer generally enclosing and generally enclosingly-contacting said first cloth layer of said cloth-layer assemblage.

6. The seal of claim 1, wherein said foil-layer assemblage includes a second foil layer which is generally identical to and generally superimposed on and generally entirely contacts said first foil layer.

7. The seal of claim 6, wherein said first and second foil layers each have slots, wherein said slots of said second foil layer are spaced apart from said slots of said first foil layer.

8. The seal of claim 1, wherein said first and second member are members of a gas turbine combustor.

9. The seal of claim 8, wherein said first and second members are members of a gas turbine combustor casing.

10. The seal of claim 1, wherein said foil-layer assemblage consists essentially of metal.

11. The seal of claim 1, wherein said foil-layer assemblage has a thickness of generally between five and ten thousandths of an inch.

12. The seal of claim 11, wherein said cloth-layer assemblage has a thickness of generally between ten and twenty-five thousandths of an inch.