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液体火箭发动机涡轮泵技术的发展
引用本文:颜子初.液体火箭发动机涡轮泵技术的发展[J].推进技术,1991,12(6):23-30,68.
作者姓名:颜子初
作者单位:航空航天部11所
摘    要:阐述了涡轮泵的技术发展水平在液体火箭发动机研制中的重要地位;分级燃烧循环系统发动机涡轮泵的设计特色;苏联涡轮泵总体设计的特点;并对预压泵、轴向力平衡活塞、两相流诱导轮、正反旋涡轮等涡轮泵新技术的设计原理进行了概述.

关 键 词:液体推进剂  火箭发动机  涡轮泵

THE DEVELOPMENT OF TURBOPUMP TECHNOLOGY FOR LIQUID ROCKET ENGINES
Yan Zichu.THE DEVELOPMENT OF TURBOPUMP TECHNOLOGY FOR LIQUID ROCKET ENGINES[J].Journal of Propulsion Technology,1991,12(6):23-30,68.
Authors:Yan Zichu
Institution:The 11th Research Institute
Abstract:The following contents are discussed in the paper, the essential position of turbopump technology in liquid rocket engine development,the design charateristics of turbopump for stage-combustion engines,and the general assembling design features of turbopumps in USSR.In addition,an overview on the design principles of turbopump technology-booster pumps,axial load balancing pistons,two-phase flow inducers,and counter-rotating turbines are also discussed
Keywords:Liquid propellant rocket engine  Rocket fuel system  Review  
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