| タイトル | Ignition and combustion: Low compression ratio, high output diesel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830007038 |
| 著者所属（英） | Michigan Univ. |
| 発行日 | 1981-07-01 |
| 言語 | eng |
| 内容記述 | The feasibility of converting a spark ignition aircraft engine GTSI0-520 to compression ignition without increasing the peak combustion pressure of 1100 lbs/sq.in. was determined. The final contemplated utilized intake air heating at idle and light load and a compression ratio of about 10:1 with a small amount of fumigation (the addition of about 15% fuel into the combustion air before the cylinder). The engine used was a modification of a Continental-Teledyne gasoline engine cylinder from the GTSI0-520 supercharged aircraft engine. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N15309
NASA-CR-169742
NAS 1.26:169742 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163906 |
