| contributor author | G. Leonard | |
| contributor author | J. Stegmaier | |
| date accessioned | 2017-05-08T23:44:06Z | |
| date available | 2017-05-08T23:44:06Z | |
| date copyright | July, 1994 | |
| date issued | 1994 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26729#542_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/113540 | |
| description abstract | This paper gives the development status of GE’s new aeroderivative premixed combustion system. This system consists of a new fuel staged annular combustor, compressor rear frame, first-stage turbine nozzle, electronic staging controller, and fuel delivery system. Component test results along with a description of the combustion system are presented. This new system will reduce NOx emissions by 90 percent relative to the original aircraft engine combustion system while maintaining low emissions of CO and UHCs. Tests of a LM6000 gas turbine equipped with the new system are planned for early 1994. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System | |
| type | Journal Paper | |
| journal volume | 116 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906853 | |
| journal fristpage | 542 | |
| journal lastpage | 546 | |
| identifier eissn | 0742-4795 | |
| keywords | Combustion systems | |
| keywords | Gas turbines | |
| keywords | Emissions | |
| keywords | Fuel delivery systems | |
| keywords | Nozzles | |
| keywords | Turbines | |
| keywords | Aircraft engines | |
| keywords | Control equipment | |
| keywords | Fuels | |
| keywords | Compressors | |
| keywords | Structural frames AND Combustion chambers | |
| tree | Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003 | |
| contenttype | Fulltext | |
