Ceramic gas turbine shroud
Abstract
An example gas turbine engine shroud includes a first annular ceramic wall having an inner side for resisting high temperature turbine engine gasses and an outer side with a plurality of radial slots. A second annular metallic wall is positioned radially outwardly of and enclosing the first annular ceramic wall and has a plurality of tabs in communication with the slot of the first annular ceramic wall. The tabs of the second annular metallic wall and slots of the first annular ceramic wall are in communication such that the first annular ceramic wall and second annular metallic wall are affixed.
- Inventors:
- Issue Date:
- Research Org.:
- Hamilton Sundstrand Corporation, Windsor Locks, CT (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1149909
- Patent Number(s):
- 8,784,052
- Application Number:
- 12/776,673
- Assignee:
- Hamilton Sundstrand Corporation (Windsor Locks, CT)
- DOE Contract Number:
- FC26-00CH11060
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2010 May 10
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Shi, Jun, and Green, Kevin E. Ceramic gas turbine shroud. United States: N. p., 2014.
Web.
Shi, Jun, & Green, Kevin E. Ceramic gas turbine shroud. United States.
Shi, Jun, and Green, Kevin E. Tue .
"Ceramic gas turbine shroud". United States. https://www.osti.gov/servlets/purl/1149909.
@article{osti_1149909,
title = {Ceramic gas turbine shroud},
author = {Shi, Jun and Green, Kevin E.},
abstractNote = {An example gas turbine engine shroud includes a first annular ceramic wall having an inner side for resisting high temperature turbine engine gasses and an outer side with a plurality of radial slots. A second annular metallic wall is positioned radially outwardly of and enclosing the first annular ceramic wall and has a plurality of tabs in communication with the slot of the first annular ceramic wall. The tabs of the second annular metallic wall and slots of the first annular ceramic wall are in communication such that the first annular ceramic wall and second annular metallic wall are affixed.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {7}
}
Save to My Library
You must Sign In or Create an Account in order to save documents to your library.
Works referenced in this record:
Composite ceramic/metal cylinder for gas turbine engine
patent, August 1983
- Hartel, Edward; Libertini, Zoltan; Manente, Joseph
- US Patent Document 4,398,866
Mechanical support of a ceramic gas turbine vane ring
patent-application, May 2008
- Shi, Jun; Green, Kevin E.; Mosher, Daniel A.
- US Patent Application 11/598450; 20080112803
Stator Damper Shim
patent-application, November 2008
- Ellis, Charles; Hollis, Terry; Medrano, David
- US Patent Application 11/744245; 20080273964
Gas turbine engine systems and methods involving blade outer air seals
patent-application, August 2009
- McCaffrey, Michael G.
- US Patent Application 12/032789; 20090208322