Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor
Abstract
An injector for a gas turbine combustor including a catalyst coated surface forming a passage for feed gas flow and a channel for oxidant gas flow establishing an axial gas flow through a flow conditioner disposed at least partially within an inner wall of the injector. The flow conditioner includes a length with an interior passage opening into upstream and downstream ends for passage of the axial gas flow. An interior diameter of the interior passage smoothly reduces and then increases from upstream to downstream ends.
- Inventors:
- Issue Date:
- Research Org.:
- Solar Turbines Inc. (San Diego, CA)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1092904
- Patent Number(s):
- 8528334
- Application Number:
- 12/015,366
- Assignee:
- Solar Turbines Inc. (San Diego, CA)
- 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:
- FC26-05NT42647
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Dutta, Partha, Smith, Kenneth O., and Ritz, Frank J. Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor. United States: N. p., 2013.
Web.
Dutta, Partha, Smith, Kenneth O., & Ritz, Frank J. Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor. United States.
Dutta, Partha, Smith, Kenneth O., and Ritz, Frank J. Tue .
"Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor". United States. https://www.osti.gov/servlets/purl/1092904.
@article{osti_1092904,
title = {Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor},
author = {Dutta, Partha and Smith, Kenneth O. and Ritz, Frank J.},
abstractNote = {An injector for a gas turbine combustor including a catalyst coated surface forming a passage for feed gas flow and a channel for oxidant gas flow establishing an axial gas flow through a flow conditioner disposed at least partially within an inner wall of the injector. The flow conditioner includes a length with an interior passage opening into upstream and downstream ends for passage of the axial gas flow. An interior diameter of the interior passage smoothly reduces and then increases from upstream to downstream ends.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2013},
month = {9}
}
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Works referenced in this record:
Advanced Catalytic Pilot for Low NOx Industrial Gas Turbines
conference, February 2009
- Karim, Hasan; Lyle, Kent; Etemad, Shahrokh
- ASME Turbo Expo 2002: Power for Land, Sea, and Air, Volume 1: Turbo Expo 2002
Rich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas Turbines
conference, February 2009
- Smith, Lance L.; Karim, Hasan; Castaldi, Marco J.
- ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference, Volume 2: Turbo Expo 2003