北京航空航天大学 能源与动力工程学院,北京,100083
纸质出版:2007
移动端阅览
孟江涛, 黄勇, 郭志辉, 等. 带旋流杯的模型回流燃烧室主燃孔射流研究[J]. 航空动力学报, 2007,22(7).
MENG Jiang-tao, HUANG Yong, GUO Zhi-hui, et al. Research on primary jet of a reverse flow combustor model with swirl cup[J]. 2007, 22(7).
孟江涛, 黄勇, 郭志辉, 等. 带旋流杯的模型回流燃烧室主燃孔射流研究[J]. 航空动力学报, 2007,22(7). DOI:
MENG Jiang-tao, HUANG Yong, GUO Zhi-hui, et al. Research on primary jet of a reverse flow combustor model with swirl cup[J]. 2007, 22(7). DOI:
实验研究了带轴径向旋流杯、主燃孔和冷却气流的模型回流燃烧室在工作压力为300 kPa
燃烧室压力损失为2.5%时主燃孔射流的特点以及其对燃烧室流场的影响.结果表明
回流式燃烧室内外壁主燃孔射流进气方向与顺流式燃烧室不同
即内壁主燃孔射流向流动方向下游倾斜
外壁主燃孔射流向流动方向上游倾斜;主燃孔射流穿透深度很大
几乎能穿透到对面火焰筒壁;中心回流区长度明显缩短
其长度L与旋流杯出口直径D的比值(L/D)约为0.5
而常规的顺流式燃烧室的L/D约为1.3.
The characteristics of primary jets and its effects on the velocity field of reverse flow combustor model
which primarily comprising an axial-radial swirl cup and a primary hole with cooling air
was studied experimentally in the case of operating pressure of 300Kpa and pressure lose of combustor of 2.5%.The results show that
the air intake direction of primary jets into the reverse flow combustor differs from that of straight-flow combustors
namely
the inner jets inclined to downstream direction
and the outer jets inclined to upstream direction.The penetration of the primary jets is very deep to reach almost the opposite liner wall.And
the length of the recirculation zone is shortened remarkably
with L/D(length to diameter of swirl cup) about 0.5D
and L/D of typical straight-flow combustor about 1.3.
0
浏览量
441
下载量
CSCD
关联资源
相关文章
相关作者
相关机构