Method and system to facilitate sealing in gas turbines
Abstract
A method and system for sealing between components within a gas turbine is provided. A first recess defined in a first component receives a seal member. A second recess defined in a second component adjacent the first component also receives the seal member. The first and second recesses are located proximate a hot gas path defined through the gas turbine, and define circumferential paths about the turbine axis. The seal member includes a sealing face that extends in a direction substantially parallel to the turbine axis. The seal member also includes a plurality of seal layers, wherein at least one of the seal layers includes at least one stress relief region for facilitating flexing of the first seal member.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1390171
- Patent Number(s):
- 9759081
- Application Number:
- 14/049,020
- Assignee:
- General Electric Company
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2013 Oct 08
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Morgan, Victor John, Foster, Gregory Thomas, and Sarawate, Neelesh Nandkumar. Method and system to facilitate sealing in gas turbines. United States: N. p., 2017.
Web.
Morgan, Victor John, Foster, Gregory Thomas, & Sarawate, Neelesh Nandkumar. Method and system to facilitate sealing in gas turbines. United States.
Morgan, Victor John, Foster, Gregory Thomas, and Sarawate, Neelesh Nandkumar. Tue .
"Method and system to facilitate sealing in gas turbines". United States. https://www.osti.gov/servlets/purl/1390171.
@article{osti_1390171,
title = {Method and system to facilitate sealing in gas turbines},
author = {Morgan, Victor John and Foster, Gregory Thomas and Sarawate, Neelesh Nandkumar},
abstractNote = {A method and system for sealing between components within a gas turbine is provided. A first recess defined in a first component receives a seal member. A second recess defined in a second component adjacent the first component also receives the seal member. The first and second recesses are located proximate a hot gas path defined through the gas turbine, and define circumferential paths about the turbine axis. The seal member includes a sealing face that extends in a direction substantially parallel to the turbine axis. The seal member also includes a plurality of seal layers, wherein at least one of the seal layers includes at least one stress relief region for facilitating flexing of the first seal member.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {9}
}
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