| タイトル | Emission Characteristics of A P and W Axially Staged Sector Combustor |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160010067 |
| 著者（英） | Kopp-Vaughan, Kristin; Cheung, Albert; Surgenor, Angela D.; He, Zhuohui J.; Lee, Chi Ming; Wey, Changlie; Chang, Clarence T. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2016-01-04 |
| 言語 | eng |
| 内容記述 | Emission characteristics of a three-cup P and W Axially Controlled Stoichiometry (ACS) sector combustor are reported in this article. Multiple injection points and fuel staging strategies are used in this combustor design. Pilot-stage injectors are located on the front dome plate of the combustor, and main-stage injectors are positioned on the top and bottom of the combustor liners downstream. Low power configuration uses only pilot-stage injectors. Main-stage injectors are added to high power configuration to help distribute fuel more evenly and achieve overall lean burn yielding very low NOx emissions. Combustion efficiencies at four ICAO LTO conditions were all above 99%. Three EINOx emissions correlation equations were developed based on the experimental data to describe the NOx emission trends of this combustor concept. For the 7% and 30% engine power conditions, NOx emissions are obtained with the low power configuration, and the EINOx values are 6.16 and 6.81. The high power configuration was used to assess 85% and 100% engine power NOx emissions, with measured EINOx values of 4.58 and 7.45, respectively. The overall landing-takeoff cycle NOx emissions are about 12% relative to ICAO CAEP/6 level. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | GRC-E-DAA-TN28388 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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