燃气轮机燃烧室中藻类替代燃料混合物的 污染物排放和性能

在一个单头部燃气轮机燃烧室中,针对与传统航空煤油(RP-3)混合的藻类替代燃料,本文进行了实验研究。实验中使用的基于藻类的替代燃料由几种烷烃混合而成,用以模拟微型藻类的碳分布。本实验研究了各种混合物的排放性能、贫油熄火极限和喷雾特性。在实验中测试了六种燃料,包括纯航空煤油和五种替代燃料混合物。在慢车状态下进行实验,进口空气压力为460 kPa,温度为511 K,流量为0.498 kg/s。实验结果表明,各种混合物的喷雾角度随替代燃料比例的增大而略有下降。当替代燃料的质量分数达到10%时,观察到燃烧性能的显著变化,这些性能包括燃烧效率、贫油熄火极限和污染物排放。     

Effects of probe support on the flow field of a low-speed axial compressor

This paper presents an investigation on the effect of probe support on the flow field of an axial compressor.The experiment is carried out in a large-scale low-speed research compressor.A cylindrical probe support intruding to 50% blade span was installed at 50% chord upstream from the rotor leading edge.The region from 5° to 32° off the probe support in the direction of rotation at the rotor outlet was measured with a 5-hole probe and a high-response total pressure probe.The experiment is performed at both near-design and near-stall points.The measuring results of 5-hole probe and high-response total pressure probe indicate that the probe blockage effect is different at different blade spans.The wake of the probe support weakens the leakage vortex intensity at the tip region,leading to greater total pressure rise.At near-design condition,the presence of probe support has a negative effect on the region from 75% to 92% span,while improves the flow field below 75% span.At near stall condition,the probe support has a negative effect on the region from 70% to 90% span,and almost has no influence on the flow field below 70% span.