Studying the Generation of Liquid Films on the Nozzle Vanes of a Turbine Stage in the Region of Low Humidity Values

A. N. Troitskii; R. V. Agapov

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Studying the Generation of Liquid Films on the Nozzle Vanes of a Turbine Stage in the Region of Low Humidity Values

机译：研究低湿度区域内涡轮级喷嘴叶片上液膜的产生

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Results from experiments on determining the thicknesses of liquid film generated on the surface of a turbine nozzle vane in the region of low steam humidity values are presented. The obtained results can be used to predict the locations at which liquid films may be generated and evaporated and, hence, to predict the regions in which corrosion processes may occur on the nozzle vane surfaces.

机译：给出了确定低蒸汽湿度值区域内在涡轮喷嘴叶片表面上产生的液膜厚度的实验结果。所获得的结果可用于预测液膜产生和蒸发的位置，从而预测喷嘴叶片表面上可能发生腐蚀过程的区域。

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《Thermal engineering》 |2010年第9期|p.779-785|共7页
作者
A. N. Troitskii; R. V. Agapov;
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Moscow Power Engineering Institute, ul. Krasnokaiarmennaya 14, Moscow, 111250 Russia;

Moscow Power Engineering Institute, ul. Krasnokaiarmennaya 14, Moscow, 111250 Russia;

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1. Numerical Study on the Secondary Air Performance of the Film Holes for the Combined Impingement and Film Cooled First Stage of High Pressure Gas Turbine Nozzle Guide Vane [J] . Pol ReddyKukutla, B.V.S.S.SPrasad International Journal of Turbo and Jet Engines . 2020,第3期

机译：高压燃气涡轮喷嘴导向叶片组合冲击和薄膜冷却第一阶段膜孔的二次空气性能的数值研究
2. Network analysis of a coolant flow performance for the combined impingement and film cooled first-stage of high pressure gas turbine nozzle guide vane [J] . Kukutla Pol Reddy, Prasad B. V. S. S. S. Proceedings of the Institution of Mechanical Engineers . 2019,第6期

机译：高压燃气轮机喷嘴导叶组合冲击和薄膜冷却的第一级冷却液流动性能的网络分析
3. Development of Procedure for and Results from Calculated Study of Thermal State of Turbine First-Stage Nozzle Vanes and Efficiency of Their Convective-Film Air Cooling [J] . K. D. Andreev, A. V. Lipin, V. G. Polishchuk, Thermal engineering . 2009,第7期

机译：涡轮第一级喷嘴叶片热态计算及对流膜风冷效率的计算方法和结果的发展
4. EFFECT OF INCIDENCE ANGLE ON GAS TURBINE FIRST-STAGE NOZZLE GUIDE VANE LEADING EDGE AND GILL REGION FILM COOLING [C] . Yang Zhang, Xin Yuan ASME turbo expo . 2012

机译：入射角对燃气轮机第一级导流叶片前缘和G区膜冷却的影响
5. Measurements in a gas turbine first stage nozzle guide vane cascade with film cooling and endwall contouring. [D] . Oke, Rohit Anand. 2001

机译：燃气轮机第一级喷嘴导流叶片中的测量随着薄膜冷却和端壁轮廓而级联。
6. Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane [O] . Haifen Du, Ziyue Mei, Jiayao Zou, 2019

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7. A Computational Validation of Turbine Nozzle Guide Vane Aerodynamic Experiments in an HP Turbine Stage [O] . Özhan H. Turgut, Cengiz Camcı 2011

机译：Hp涡轮级涡轮喷嘴导叶气动实验的计算验证

Studying the Generation of Liquid Films on the Nozzle Vanes of a Turbine Stage in the Region of Low Humidity Values

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