摘要
为了获得正弯静叶在动态压气机中的性能特点,分别对采用带根部间隙的直静叶和正弯静叶的重复级低速轴流压气机在不同流量工况下的静叶出口流场进行了实验测量,结果表明,正弯静叶对气流的扩压能力在设计工况和近喘工况下强于直静叶,在最大流量工况下弱于后者。设计工况下,流道内存在的两个主要旋涡结构,分别为上通道涡和刮削涡,且刮削涡在正弯静叶流道内的尺度要远小于直静叶流道中;最大流量工况下直静叶流道中的刮削涡明显增大而正弯静叶中则基本保持不变;近喘工况下分离严重,旋涡随之消失。考查出口气流角可以发现,正弯静叶对气流的折转能力在整个流量工况下都弱于直静叶,但沿叶高的分布更为均匀。
Experimental investigation was performed in a double stages low speed axial compressor.The traverse flow field at the exit of second stator was measured in details at different working condition for both straight and positive bowed stator passages.The results show that the pressure diffusion ability in positive bowed stator passage is stronger than in straight stator at design condition and near stall condition but weaker in near maximum flow condition.There are two main vortexes in stator passage at design...
出处
《推进技术》
EI
CAS
CSCD
北大核心
2009年第5期581-587,共7页
Journal of Propulsion Technology
基金
国家自然科学基金(50236020)
教育部博士点基金(20060213007)
关键词
压气机
正弯静叶+
旋涡结构+
实验研究
Compressor
Positive bowed stator+
Vortex structure+
Experimental investigation