Rich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas TurbinesSource: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001::page 27Author:Lance L. Smith
,
Vivek Khanna
,
Kenneth O. Smith
,
Hasan Karim
,
Marco J. Castaldi
,
Shahrokh Etemad
,
William C. Pfefferle
DOI: 10.1115/1.1787510Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A new rich-catalytic lean-burn combustion concept (trademarked by PCI as RCL) was tested at industrial gas turbine conditions, in Solar Turbines’ high-pressure (17 atm) combustion rig and in a modified Solar Turbines engine, demonstrating ultralow emissions of NOx<2 ppm and CO<10 ppm for natural gas fuel. For the single-injector rig tests, an RCL catalytic reactor replaced a single swirler/injector. NOx<3 ppm and CO<10 ppm were achieved over a 110°C operating range in flame temperature, including NOx<1 ppm at about 1350°C flame temperature. Combustion noise was less than 0.15% peak to peak. Four RCL catalytic reactors were then installed in a modified (single can combustor) engine. NOx emissions averaged 2.1 ppm over the allowable operating range for this modified engine, with CO<10 ppm and without combustion noise (less than 0.15% peak to peak).
keyword(s): Temperature , Combustion , Fuels , Engines , Combustion chambers , Ejectors , Catalysts , Emissions , Gas turbines , Stress , Flow (Dynamics) , Air flow AND Flames ,
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| contributor author | Lance L. Smith | |
| contributor author | Vivek Khanna | |
| contributor author | Kenneth O. Smith | |
| contributor author | Hasan Karim | |
| contributor author | Marco J. Castaldi | |
| contributor author | Shahrokh Etemad | |
| contributor author | William C. Pfefferle | |
| date accessioned | 2017-05-09T00:16:13Z | |
| date available | 2017-05-09T00:16:13Z | |
| date copyright | January, 2005 | |
| date issued | 2005 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26854#27_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/131818 | |
| description abstract | A new rich-catalytic lean-burn combustion concept (trademarked by PCI as RCL) was tested at industrial gas turbine conditions, in Solar Turbines’ high-pressure (17 atm) combustion rig and in a modified Solar Turbines engine, demonstrating ultralow emissions of NOx<2 ppm and CO<10 ppm for natural gas fuel. For the single-injector rig tests, an RCL catalytic reactor replaced a single swirler/injector. NOx<3 ppm and CO<10 ppm were achieved over a 110°C operating range in flame temperature, including NOx<1 ppm at about 1350°C flame temperature. Combustion noise was less than 0.15% peak to peak. Four RCL catalytic reactors were then installed in a modified (single can combustor) engine. NOx emissions averaged 2.1 ppm over the allowable operating range for this modified engine, with CO<10 ppm and without combustion noise (less than 0.15% peak to peak). | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Rich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas Turbines | |
| type | Journal Paper | |
| journal volume | 127 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.1787510 | |
| journal fristpage | 27 | |
| journal lastpage | 35 | |
| identifier eissn | 0742-4795 | |
| keywords | Temperature | |
| keywords | Combustion | |
| keywords | Fuels | |
| keywords | Engines | |
| keywords | Combustion chambers | |
| keywords | Ejectors | |
| keywords | Catalysts | |
| keywords | Emissions | |
| keywords | Gas turbines | |
| keywords | Stress | |
| keywords | Flow (Dynamics) | |
| keywords | Air flow AND Flames | |
| tree | Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001 | |
| contenttype | Fulltext |