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涡轴(涡桨)/涡扇(涡喷)发动机通用核心机技术
引用本文:尹泽勇,曾源江,石建成,罗安阳.涡轴(涡桨)/涡扇(涡喷)发动机通用核心机技术[J].航空动力学报,2008,23(11):2088-2094.
作者姓名:尹泽勇  曾源江  石建成  罗安阳
作者单位:中国航空动力机械研究所;
摘    要:通用核心机技术不仅可增加所发展发动机的通用零件数,缩短研制周期,还可使所发展的各类发动机性能均较先进.不同流量的通用核心机可相应发展不同功率/推力范围的各类发动机,通用核心机的设计需考虑强度与气动性能的折衷,其部件应有宽广的高效与稳定工作范围,且通用前提下也允许核心机后续发展时有小的变动.文中最后讨论了某中小型通用核心机方案设计中涡轮级数和压气机形式的选择问题.

关 键 词:通用核心机  涡轴发动机  涡桨发动机  涡扇发动机  涡喷发动机
收稿时间:2007/10/23 0:00:00
修稿时间:2008/5/11 0:00:00

Versatile core engine technology for turboshaft(turboprop)/turbofan(turbojet) engines
YIN Ze-yong,ZENG Yuan-jiang,SHI Jian-cheng and LUO An-yang.Versatile core engine technology for turboshaft(turboprop)/turbofan(turbojet) engines[J].Journal of Aerospace Power,2008,23(11):2088-2094.
Authors:YIN Ze-yong  ZENG Yuan-jiang  SHI Jian-cheng and LUO An-yang
Institution:YIN Ze-yong,ZENG Yuan-jiang,SHI Jian-cheng,LUO An-yang (China Aviation Powerplant Research Institute,Zhuzhou 412002,China)
Abstract:The development of aero-engine technology makes it necessary to study the versatile core engine technology.Versatile core engine technology not only increases the number of the common parts of the developed engines,reduces its research and development periods,but also improves the performances of all the types of the developed engines.Aero-engines of different kinds with a certain power/thrust class could be derived from the corresponding versatile core engine with a certain mass flow amount.The design of v...
Keywords:versatile core engine  turboshaft  turboprop  turbofan  turbojet  
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