To realize multiple starts of LOX/CH4 rocket engines, a fuel rich torch igniter fed with gaseous oxygen and gaseous methane is designed, in which methane is used as film cooling refrigerant. Through CFD simulation and CFD simulation, comparative study on the ignition reliability and thermal protective effect is conducted with three types of igniters. It is found that ignition mixture ratio affects the ignition success rate and thermal protective effect directly, and relative distances between methane injectors and oxygen injectors is an important parameter which would affect the working characteristics of the ignitors. The selected ignitor with double rows of CH4 injectors can ignite reliably while the mixture ratio is between 0.6 and 1.3. During the second round test in which the flow rate is 25~50 g/s while the mixture rate is 0.6~1.0, the ignitor ignited successfully 11 times in a row and no structure burned damage is found. The reliability of the film-cooling igniter and multiple starts is verified. With simulation results, it is showed that the relative distance between the injectors has an important influence on the thermal protective effect of film cooling. Using multi-rows of methane injectors is an optimized scheme consideration to ignition reliability and thermal protective effect.
| 科 Family | 属数 Number of genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) | 属 Genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) |
|---|---|---|---|---|---|---|
| 鹅膏菌科Amanitaceae | 2 | 11 | 5.26 | 鹅膏菌属 Amanita | 10 | 4.78 |
| 小菇科 Mycenaceae | 2 | 12 | 5.74 | 丝盖伞属 Inocybe | 5 | 2.39 |
| 多孔菌科 Polyporaceae | 8 | 14 | 6.70 | 蜡蘑属 Laccaria | 5 | 2.39 |
| 红菇科 Russulaceae | 3 | 23 | 11.00 | 小皮伞属 Marasmius | 6 | 2.87 |
| 小菇属 Mycena | 11 | 5.26 | ||||
| 光柄菇属 Pluteus | 5 | 2.39 | ||||
| 红菇属 Russula | 17 | 8.13 | ||||
| 栓菌属 Trametes | 5 | 2.39 |