| タイトル | Reduction of aircraft gas turbine engine pollutant emissions - A status report |
| 著者（英） | Diehl, L. A. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1978-06-01 |
| 言語 | eng |
| 内容記述 | In mid-1971, NASA began a major program in emission reduction technology, which would consist of a continuing in-house effort on low emission combustor concepts and of contracted research programs with the major aircraft engine manufacturers. A description is presented of the design approaches taken by the manufacturers involved in the contracted programs. Current results are compared with EPA standards, and some of the engine related factors are briefly considered. In addition, some results from fundamental technology programs which indicate the emission levels which may be approached by advanced low emission combustors of the future are also discussed. It is found that special engine design features represent at least a partial solution to reducing aircraft emissions for engines of the future. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78A45429 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/431741 |
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