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试论联合循环中使用的汽轮机及暖机操作
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作者 王新力 张有瑞 《经济技术协作信息》 2014年第9期107-107,共1页
随着电网的结构调整,对电网中机组响应负荷能力提出了更高的要求,这就要求机组各关键设备具备快速启动的性能。近年来汽轮机组的快速启动越来越多的被研究。文章探讨了联合循环中使用的汽轮机及暖机操作。
关键词 汽轮 暖机操作
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某电厂联合循环汽轮机启动过程优化 被引量:29
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作者 丁阳俊 盛德仁 +3 位作者 陈坚红 洪雷 顾正皓 林成 《中国电机工程学报》 EI CSCD 北大核心 2013年第2期9-15,5,共7页
燃气/蒸汽联合循环机组中汽轮机启动时间较长,导致联合循环机组不能及时响应电网调峰需求。为此,通过数值实验和现场启动试验相结合的方法研究了汽轮机的启动过程。建立汽轮机转子二维轴对称有限元模型,确定非线性边界条件,通过数值模... 燃气/蒸汽联合循环机组中汽轮机启动时间较长,导致联合循环机组不能及时响应电网调峰需求。为此,通过数值实验和现场启动试验相结合的方法研究了汽轮机的启动过程。建立汽轮机转子二维轴对称有限元模型,确定非线性边界条件,通过数值模拟研究启动过程各暖机操作对转子应力的影响。基于数值实验分析结果,结合试验机组结构、运行特点,制定优化后的启动过程。温态启动时汽轮机转子最大应力降低11 MPa,启动时间缩短36 min,低周疲劳寿命损耗减少0.0008%;冷态启动时转子最大应力降低261MPa,启动时间缩短32min,低周疲劳寿命损耗减少0.0197%。 展开更多
关键词 联合循环 汽轮启动过程 暖机操作 转子应力 低周疲劳寿命损耗
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Numerical Tools for the Control of the Unsteady Heating of an Airfoil
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作者 Franqoise Masson Francisco Chinesta +4 位作者 Adrien Leygue Chady Ghnatios Elias Cueto Laurent Dala Craig Law 《Journal of Mechanics Engineering and Automation》 2013年第6期339-351,共13页
This paper concerns the real time control of the boundary layer on an aircraft wing. This new approach consists in heating the surface in an unsteady regime using electrically resistant strips embedded in the wing ski... This paper concerns the real time control of the boundary layer on an aircraft wing. This new approach consists in heating the surface in an unsteady regime using electrically resistant strips embedded in the wing skin. The control of the boundary layer's separation and transition point will provide a reduction in friction drag, and hence a reduction in fuel consumption. This new method consists in applying the required thermal power in the different strips in order to ensure the desired temperatures on the aircraft wing. We also have to determine the optimum size of these strips (length, width and distance between two strips). This implies finding the best mathematical model corresponding to the physics enabling us to facilitate the calculation for any type of material used for the wings. Secondly, the heating being unsteady, and, as during a flight the flow conditions or the ambient temperatures vary, the thermal power needed changes and must be chosen as fast as possible in order to ensure optimal operating conditions. 展开更多
关键词 Model reduction PGD (proper generalized decomposition) heating of an airfoil boundary layers laminar-turbulenttransition and separation point friction drag unsteady heating.
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