节点文献
一种后掠式离心压气机的研制
A Report on Designing, Manufacturing and Testing a Backswept Bladed Centrifugal Compressor Impeller with Controlled Exit
【摘要】 本文叙述了一种新型后掠式离心压气机的设计、制造和试验,并与普通径疏式离心压气机作了对比:绝热效率可提高4%、有效流量范围在额定转数时扩大了11.4%、高效率区扩大42%。文中对喘振原理的解释及喘振工况的预测可供研究具有无叶扩压器的离心压气机时参考。
【Abstract】 In this paper, the designing principle, manufacturing technology and testing result of a backswept bladed compressor impeller with controlled exit are described and analysed. As compared with the ordinary radial bladed compressor impeller, its adiabatic efficiency increases by 4%, its effective flow range at rated speed widens by 11.4% and its max. efficiency zone enlarges by 42%.The principle and boundary of surge of centrifugal compressor with certain vaneless diffuser are interpreted and predicted, and confirmed by this experiment as well.
- 【文献出处】 内燃机工程 ,Chinese Internal Combustion Engine Engineering , 编辑部邮箱 ,1981年03期
- 【被引频次】1
- 【下载频次】70