摘要
本文通过对某项目6F.03燃气轮机进气道的设计,阐述了实验用燃气轮机进气系统的作用、组成、设计依据、计算过程与考评标准等。通过3D建模和流场分析进行模拟评估,在设计过程中发现影响计算结果的主要因素并针对其进行调整,最终达到进气系统的设计要求。
Through the design process of a 6F. 03 gas turbine intake system, the function, composition, design basis, calculation process and evaluation standard of the experimental gas turbine system are described. Through the 3D modeling and flow field analysis to simulate the evaluation, in the design process we found that the main factors affecting the calculation results and for the adjustment, and ultimately to the intake system can meet design requirements.
作者
薛晶
XUE Jing(Nanjing Turbine and Electric Machinery （Group） Co. , Ltd. , Nanjing 210037, China)
出处
《燃气轮机技术》
2017年第3期46-51,共6页
Gas Turbine Technology
