风扇/压气机技术发展和对今后工作的建议
Development of Fan/Compressor Techniques and Suggestions on Further Researches
-
摘要: 风扇 /压气机是航空涡轮发动机的关键部件之一, 高推重比发动机对它们提出了更高的要求, 出现了一些新的技术问题需要加以研究解决。本文评述了风扇 /压气机的发展趋势, 对于提高其性能的主要措施如高叶片速度, 低展弦比, 高通流进口级, 掠形叶片技术, 大小叶片气动布局等都作了详尽程度不同的评述。风扇 /压气机内的非定常流动不仅影响气动性能, 而且影响可靠性, 如高周疲劳、失速和颤振等, 应加强研究。现代计算流体力学为我们提供了跨越式发展的可能性。本文对今后工作提出了建议。Abstract: Fan/compressor is one of the key components of turbo jet engines.As higher performance is demanded by the engines with higher thrust/weight ratio,some new techniques appeared and were needed to be further studied.The development trend of fan/compressor is described.The main measures for improving performance,such as high blade speed,low aspect ratio,high through flow inlet stage,swept blade,splittered vane rotor,are discussed.Unsteady flow in fan/compressor not only affects its gasdynamic performance,but also reliability,since high cycle fatigue,stall and flutter will cause serious machine damage.CFD provides possibility of fast development of our fan/compressor techniques.Further researches are proposed in this paper.
-
Key words:
- fan /
- compressors /
- blade /
- unsteady flow
点击查看大图
计量
- 文章访问数: 4360
- HTML浏览量: 4
- PDF量: 672
- 被引次数: 0