燃机的燃料系统设计  

Design of Fuel System for a Industrial Gas Rurbine

作　　者：张丽桃[1] 王伟 蓝天霞 林成 

机构地区：[1]北华航天工业学院材料工程系,河北廊坊065000 [2]中航黎明发动机集团有限公司,辽宁沈阳110043

出　　处：《北华航天工业学院学报》2011年第5期6-9,共4页Journal of North China Institute of Aerospace Engineering

摘　　要：某型燃机是由航空发动机改进而成的,其设计及应用拓宽了航空发动机的使用范围,开辟了新的市场空间。燃机的主要设计思想是保持航空发动机总体布局不变,只对局部做了较大改进,这样不仅降低燃机的研制成本,缩短燃机的研制周期,而且能及时满足市场需求。燃机使用的燃料为天然气,因此设计了燃机的燃气系统,并对主燃烧室进行了改制,以适应燃气系统的装配。A gas turbine is derived from an aero engine,which design and application expanded the using range of an aero engine using opening the new market.The basic design idea of gas turbine is that makes local changes other than remains the overall layout of aero engine unchanged which not only reducing the development cost of gas turbine and shortening the development periods of the Gas turbine,but also it can meet the market requirement in time.The fuel used by gas turbine is natral gas,therefore the gas system had been designed and the main combustor was improved for the purpose of assembly of gas system.

关 键 词：燃机 燃料系统 设计 

分 类 号：V233[航空宇航科学与技术—航空宇航推进理论与工程]