摘要
介绍了新型氢氧火箭发动机试验系统的液氢主管道用DN250直流式截止阀的结构特点和性能参数,提出了低温阀门、漏热、阀颈长度和密封等技术问题的处理方法。
The paper introduces structure characteristics and performance parameters of DN250 oblique type liquid hydrogen globe valve used for liquid hydrogen main pipelines in the test system of new type hydrogen-oxy rocket engine, proposes handling methods for some technical problems, such as for low temperature valves, leakage of heat, the length of valve neck, sealing and so on.
出处
《阀门》
2008年第5期5-7,40,共4页
VALVE MAGAZINE
关键词
截止阀
液氢
低温
漏热
密封
globe valve
liquid hydrogen
cryogenic
leakage heat
sealing