本文已被：浏览 470次 下载 394次
中文摘要: 燃烧调整是发电领域燃气轮机检修服务中的重点工作之一，也是中国“十三五”期间“两机重大专 项”研究内容的一部分。燃烧调整问题可视为多目标最优化问题，存在可控参数与边界参数、边界参数与总 体稳定裕度的二级平衡关系，确定相关变量的相互关系从而保证各级参数的平衡和稳定是进行精细化燃烧 调整的关键。不同燃气轮机的燃烧调整方法因燃烧室结构和燃烧原理不同而产生差异，文章总结了三菱公 司M701F燃气轮机和GE公司DLN1.0燃烧器燃烧调整方法，对我国燃烧调整发展方向进行了展望。
Abstract:Combustion tuning is one of the key tasks in the maintenance service of gas turbines in the field of power generation，and it
is also part of the research on the “two major special projects” in China dring the “13th Five-Year Plan” period. The combustion
adjustment problem can be regarded as a multi-objective optimization problem. There is a two-level equilibrium relationship between
controllable parameters and boundary parameters, and boundary parameters and overall stability margin, determining the interrelationship of related variables to ensure the balance and stability of various parameters is the key to carry out refined combustion
tuning. The combustion tuning methods of different gas turbines are different due to the different combustion chamber structures and
combustion principles. The article summarizes the combustion tuning methods of Mitsubishi M701F gas turbine and GE company
DLN1.0 combustion, and prospects the development direction of China＇s combustion tuning.
文章编号： 中图分类号：TK477 文献标志码：
基金项目:
引用文本：
作者.题名[J].刊名,出版年份,卷号(期号):起止页码.
[2]KIM K M, PARK J S, DONG H L, et al. Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages[J]. Engineering Failure Analysis, 2011, 18(4):1212-1222.
作者.题名[J].刊名,出版年份,卷号(期号):起止页码.
[2]KIM K M, PARK J S, DONG H L, et al. Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages[J]. Engineering Failure Analysis, 2011, 18(4):1212-1222.