QD—128航改燃机燃烧室设计分析 |
| |
引用本文: | 尚守堂.QD—128航改燃机燃烧室设计分析[J].航空发动机,2002(3):1-4. |
| |
作者姓名: | 尚守堂 |
| |
作者单位: | 中国航空工业沈阳发动机设计研究所,沈阳,110015 |
| |
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。
|
关 键 词: | 航改燃机 燃烧室设计 航空发动机 |
修稿时间: | 2002年6月12日 |
Design and Analysis of QD-128 Aeroderivative Industrial Gas Turbine combustor |
| |
Authors: | Shang Shoutang |
| |
Abstract: | 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. |
| |
Keywords: | aeroderivative industrial gas turbine combustor design aeroengine |
本文献已被 CNKI 维普 万方数据 等数据库收录! |