摘要
介绍了QD-128燃气轮机燃烧室的设计要求,分析了某航空发动机主燃烧室改为燃气轮机燃烧室的可行性,简要介绍了QD-128燃气轮机燃烧室主要部件的设计特点,并对装配和试运转提出要求。
The design target of QD-128 industrial gas turbine combustor is presented in this paper. The feasibility is analyzed of deriving the industrial gas turbine combustor from an aeroengine combustor. Design features of the main components of the combustor are briefly described and some requirements for assembly and test run are provided.
出处
《航空发动机》
2002年第3期1-4,共4页
Aeroengine
关键词
设计分析
燃烧室
航空发动机
燃气轮机
aeroderivative industrial gas turbine
combustor design
aeroengine
