| タイトル | Aircraft Engine Sump Fire Mitigation, Phase 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790009048 |
| 著者（英） | Rosenlieb, J. W. |
| 著者所属（英） | SKF Industries, Inc. |
| 発行日 | 1978-04-01 |
| 言語 | eng |
| 内容記述 | The effect of changes in the input parameters (air leakage flow rate and temperature and lubricating oil inlet flow rate and temperature) over a specified range on the flammability conditions within an aircraft engine bearing sump was investigated. An analytical study was performed to determine the effect of various parameters on the generation rate of oil vapor from oil droplets in a hot air stream flowing in a cylindrical tube. The ignition of the vapor-air mixture by an ignition source was considered. The experimental investigation demonstrated that fires would be ignited by a spark ignitor over the full range of air and oil flow rates and air temperatures evaluated. However, no fires could be ignited when the oil inlet temperature was maintained below 41.7 K (290 F). The severity of the fires ignited were found to be directly proportional to the hot air flow rate. Reasonably good correlation was found between the mixture temperature in the sump at the ignitor location and the flammability limits as defined by flammability theory; thus a fairly reliable experimental method of determining flammable conditions within a sump was demonstrated. The computerized mathematical model shows that oil droplet size and air temperature have the greatest influence on the generation rate of oil vapor. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 79N17219
NASA-CR-135379
AL78T007 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176508 |
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