Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine
Abstract
A ducting arrangement (12) for a combustion turbine engine is provided. The arrangement includes a ceramic liner (22) defining a hot gas path throughout a length of the ducting arrangement. A cooling sleeve (24) is disposed circumferentially outwardly onto the ceramic liner along the length. A metallic support frame (26) is disposed circumferentially outwardly onto the cooling sleeve along the length. The cooling sleeve may be structured with structural features along the length for biasing against the ceramic liner and the metallic support frame to resiliently accept mechanical and thermal growth induced loading that develops between the ceramic liner and the metallic support frame during operating conditions of the combustion turbine engine.
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1524997
- Patent Number(s):
- 10215039
- Application Number:
- 15/207,716
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
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:
- FE0023955
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2016-07-12
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Schiavo, Anthony L. Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine. United States: N. p., 2019.
Web.
Schiavo, Anthony L. Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine. United States.
Schiavo, Anthony L. Tue .
"Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine". United States. https://www.osti.gov/servlets/purl/1524997.
@article{osti_1524997,
title = {Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine},
author = {Schiavo, Anthony L.},
abstractNote = {A ducting arrangement (12) for a combustion turbine engine is provided. The arrangement includes a ceramic liner (22) defining a hot gas path throughout a length of the ducting arrangement. A cooling sleeve (24) is disposed circumferentially outwardly onto the ceramic liner along the length. A metallic support frame (26) is disposed circumferentially outwardly onto the cooling sleeve along the length. The cooling sleeve may be structured with structural features along the length for biasing against the ceramic liner and the metallic support frame to resiliently accept mechanical and thermal growth induced loading that develops between the ceramic liner and the metallic support frame during operating conditions of the combustion turbine engine.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {2}
}
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