预燃级旋流数对中心分级燃烧室点火性能影响

刘岩; 惠鑫; 王建臣; 王欣尧; 韩猛

doi:10.13224/j.cnki.jasp.20220277

预燃级旋流数对中心分级燃烧室点火性能影响

doi: 10.13224/j.cnki.jasp.20220277

刘岩^1,,
惠鑫¹,
王建臣^1,*, ,,
王欣尧²,
韩猛¹

1.
北京航空航天大学航空发动机研究院，北京 100191
2.
北京航空航天大学能源与动力工程学院，北京 100191

详细信息

作者简介:
刘岩（1996-），男，硕士生，主要从事低排放燃烧室研究。E-mail：lyliuyan@buaa.edu.cn

通讯作者:
王建臣（1986-），男，助理研究员，博士，主要从事航空发动机低排放燃烧研究。E-mail：wangjianchen@buaa.edu.cn

中图分类号: V231.2
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- 被引次数: 0
出版历程
- 收稿日期: 2022-04-29
- 网络出版日期: 2022-09-07

Effect of swirl number of pilot stage on ignition performance of centrally-staged combustor

LIU Yan^1
,,
HUI Xin¹,
WANG Jianchen^{1,*
, ,},
WANG Xinyao²,
HAN Meng¹

1.
Research Institute of Aero-Engine，Beihang University，Beijing 100191，China
2.
School of Energy and Power Engineering，Beihang University，Beijing 100191，China

摘要

摘要:
为了研究预燃级旋流数对中心分级燃烧室点火性能的影响规律，对采用3种不同内外旋流强度预燃级的中心分级燃烧室进行了常温常压、常温低压的贫油点火试验，获得了贫油点火边界曲线。点火试验结果表明内弱旋流外强旋流预燃级点火性能最好，增大预燃级内旋流强度不利于点火。研究进一步采用米氏散射技术测量了3种方案预燃级出口的燃油空间分布特性，测量结果表明增大预燃级内旋流强度会使喷雾张角增大，降低预燃级外旋流强度可以减小喷雾张角，内弱旋外强旋流预燃级设计能够让油雾在燃烧室中心轴线和壁面点火嘴附近都有充足的分布，从而改善燃烧室点火性能。
- 点火性能 /
- 中心分级燃烧室 /
- 预燃级旋流数 /
- 油雾空间分布 /
- 喷雾张角
Abstract:
In order to investigate the influence of pilot stage swirl intensity on ignition performance, ignition tests using a centrally-staged combustor equipped with three different pilot stages with different inner/outer swirl numbers were carried out at atmospheric temperature and sub-and atmospheric pressures, and the ignition boundaries were obtained. The ignition test results showed that the ignition performance of inner weak swirl and outer strong swirl pilot stage had the best ignition performance, and increasing the inner swirl intensity was not conducive to ignition. The spatial distributions of the fuel spray at the outlet of the three configurations of pilot stage were measured by using the Mie scattering technology. The measurement results showed that increasing the inner swirl intensity can increase the spray angle, and reducing the outer swirl intensity can reduce the spray angle. The pilot stage with inner weak swirl and outer strong swirl led to proper fuel distribution near the central axis of the combustor and near the ignitor, thereby improving the ignition performance. The results are useful for improving ignition performance of centrally-staged combustors.
- ignition performance /
- centrally-staged combustor /
- swirl number of pilot stage /
- fuel distribution /
- spray angle

HTML

图 1 单环腔火焰筒试验件

Figure 1. Single annular combustor

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图 2 头部方案结构

Figure 2. Dome configuration

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图 3 常压点火系统简图

Figure 3. Schematic of atmospheric ignition system

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图 4 PMie测量系统简图

Figure 4. Schematic of PMie measurement system

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图 5 常压点火边界曲线

Figure 5. Atmospheric ignition boundary

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图 6 常温低压点火边界曲线

Figure 6. Ambient temperature and low pressure ignition boundary

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图 7 2%压降下油气比为0.022的3种方案油雾场分布

Figure 7. Fuel distributions of three configurations at fuel/air-ratio of 0.022 and 2% pressure drop

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图 8 3%压降下油气比为0.018的3种方案油雾场分布

Figure 8. Fuel distributions of three configurations at fuel/air-ratio of 0.018 and 3% pressure drop

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图 9 3%压降下油气比为0.03的3种方案油雾场分布

Figure 9. Fuel distributions of three configurations at fuel/air-ratio of 0.03 and 3% pressure drop

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表 1 预燃级方案设计参数

Table 1. Design parameters of pilot stage scheme

方案内旋流数外旋流数类型

A 0.4 0.8 内弱旋外强旋
B 0.6 0.8 内中旋外强旋
C 0.8 0.6 内强旋外中旋

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