高温高压蒸发型燃烧加热器的设计  

Design of vapourization type combustion heater with high temperature and pressure

作　　者：黎明[1] 吴二平[1] 唐明[1] 

机构地区：[1]西北工业大学动力与能源学院,西安710072

出　　处：《航空动力学报》2009年第7期1443-1448,共6页Journal of Aerospace Power

摘　　要：为某热风洞试验台设计了一种高温、高压蒸发型煤油燃烧加热器,根据热风洞试验台对加热器的性能要求,设计了加热器的主要部件,采用流阻法和一元流法,对加热器的空气流量分配及流程参数进行了计算.试验结果表明,所设计的加热器在结构方案、主要部件和总体性能方面基本满足设计要求,具有一定的适用性和工程实用价值.A vapourization type heater fueled by kerosene with high temperature and pressure was designed for the certain thermal wind tunnel platform.According to performance requirements of the heater,the main components were designed,the air flow distribution and flowage parameters were calculated by the methods of flow resistance and one dimension flow.The experimental results show that the designed heater meets the demand for structural project,main components and overall performance and is valuable for engineeri...

关 键 词：热风洞 高温高压 蒸发型 加热器 

分 类 号：V231[航空宇航科学与技术—航空宇航推进理论与工程]