| タイトル | The E3 combustors: Status and challenges |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810019557 |
| 著者（英） | Rohde, J. E.; Sokolowski, D. E. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1981-01-01 |
| 言語 | eng |
| 内容記述 | The design, fabrication, and initial testing of energy efficient engine combustors, developed for the next generation of turbofan engines for commercial aircraft, are described. The combustor designs utilize an annular configuration with two zone combustion for low emissions, advanced liners for improved durability, and short, curved-wall, dump prediffusers for compactness. Advanced cooling techniques and segmented construction characterize the advanced liners. Linear segments are made from castable, turbine-type materials. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N28095
E-904
NASA-TM-82684 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/168471 |
