Gas turbine premixer with internal cooling
Abstract
A system that includes a turbine fuel nozzle comprising an air-fuel premixer. The air-fuel premixed includes a swirl vane configured to swirl fuel and air in a downstream direction, wherein the swirl vane comprises an internal coolant path from a downstream end portion in an upstream direction through a substantial length of the swirl vane.
- Inventors:
- Issue Date:
- Research Org.:
- National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1082352
- Patent Number(s):
- 8333075
- Application Number:
- 12/425,293
- Assignee:
- General Electric Company (Schenectady, NY)
- 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
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, and Stevenson, Christian Xavier. Gas turbine premixer with internal cooling. United States: N. p., 2012.
Web.
York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, & Stevenson, Christian Xavier. Gas turbine premixer with internal cooling. United States.
York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, and Stevenson, Christian Xavier. Tue .
"Gas turbine premixer with internal cooling". United States. https://www.osti.gov/servlets/purl/1082352.
@article{osti_1082352,
title = {Gas turbine premixer with internal cooling},
author = {York, William David and Johnson, Thomas Edward and Lacy, Benjamin Paul and Stevenson, Christian Xavier},
abstractNote = {A system that includes a turbine fuel nozzle comprising an air-fuel premixer. The air-fuel premixed includes a swirl vane configured to swirl fuel and air in a downstream direction, wherein the swirl vane comprises an internal coolant path from a downstream end portion in an upstream direction through a substantial length of the swirl vane.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2012},
month = {12}
}
Works referenced in this record:
Burner Development and Operability Issues Associated with Steady Flowing Syngas Fired Combustors
journal, May 2008
- Lieuwen, Tim; McDonell, Vince; Santavicca, Domenic
- Combustion Science and Technology, Vol. 180, Issue 6