Design Methodology and Development of Pressure Swirl Atomizer for Micro Gas Turbine Combustion Chamber

Digvijay B. Kulshreshtha; Saurabh B. Dikshit; S. A. Channiwala

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Design Methodology and Development of Pressure Swirl Atomizer for Micro Gas Turbine Combustion Chamber

机译：微型燃气轮机燃烧室压力旋流雾化器的设计方法与开发

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A method to design a pressure swirl atomizer is presented considering the ideal flow and viscous flow. The basic design dimensions of atomizers are presented in the form of theoretical and empirical approach. The designed methodology of combining the theoretical and empirical approach is presented and from that the pressure swirl atomizes with spray cone angles of 60°, 90°, and 120° are developed for application in tubular type combustion chamber of micro gas turbine.

机译：提出了一种考虑理想流量和粘性流量的压力旋流雾化器的设计方法。雾化器的基本设计尺寸以理论和经验方法的形式给出。提出了将理论方法与经验方法相结合的设计方法，并由此开发了以60°，90°和120°的喷射锥角雾化压力旋流的方法，用于微型燃气轮机的管状燃烧室。

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《International Journal of Applied Engineering Research》 |2009年第10期|共9页
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Digvijay B. Kulshreshtha; Saurabh B. Dikshit; S. A. Channiwala;
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中图分类工程基础科学;
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1. Design Methodology and Development of Pressure Swirl Atomizer for Micro Gas Turbine Combustion Chamber [J] . Digvijay B. Kulshreshtha, Saurabh B. Dikshit, S. A. Channiwala International Journal of Applied Engineering Research . 2009,第10期

机译：微型燃气轮机燃烧室压力旋流雾化器的设计方法与开发
2. Factors Affecting Spray Cone Angle of Pressure Swirl Atomizer for Gas Turbine Combustion Chamber: Theoretical and Experimental Analysis [J] . S. B. Dikshit, Digvijay Kulshreshta, S. A. Channiwala Indian Journal of Science and Technology . 2018,第8期

机译：燃气轮机燃烧室压力旋流雾化器喷雾锥角的影响因素：理论与实验分析
3. Factors Affecting Spray Cone Angle of Pressure Swirl Atomizer for Gas Turbine Combustion Chamber: Theoretical and Experimental Analysis [J] . S. B. Dikshit, Digvijay Kulshreshta, S. A. Channiwala Indian Journal of Science and Technology . 2018,第8期

机译：燃气轮机燃烧室压力旋流雾化器喷雾锥角的影响因素：理论与实验分析
4. FLOW IN ATOMIZERS: INFLUENCE OF DIFFERENT PARAMETERS ON THE PERFORMANCE CHARACTERISTICS OF PLAIN ORIFICE ATOMIZER AND PRESSURE SWIRL ATOMIZER OF A FUEL INJECTION SYSTEM OF GAS TURBINE COMBUSTOR [C] . Digvijay B Kulshreshtha, S A Channiwala ASME(American Society of Mechanical Engineers) Fluids Engineering Division Summer Conference(FEDSM2005) vol.1 pt.B; 20050619-23; Houston,TX(US) . 2005

机译：原子流量：不同参数对燃气轮机燃烧器燃料喷射系统的平原有机物雾化器和旋流式雾化器性能的影响
5. Development of a design tool for modern gas turbine combustors and commissioning of a gas turbine combustion research laboratory. [D] . Capurro, Michele. 2008

机译：开发用于现代燃气轮机燃烧器的设计工具，并调试燃气轮机燃烧研究实验室。
6. Investigation of the Pressure Gain Characteristics and Cycle Performance in Gas Turbines Based on Interstage Bleeding Rotating Detonation Combustion [O] . Lei Qi, Zhitao Wang, Ningbo Zhao, 2019

机译：基于间隙旋转爆轰燃烧的燃气轮机压力增益特性及循环性能研究
7. A swirler stabilized combustion chamber for a micro-gas turbine fuelled with natural gas [O] . Krieger, Guenther C., Campos, André P. V. de, Sacomano Filho, Fernando L., 2012

机译：用于天然气供气的微型燃气轮机的旋流器稳定燃烧室

Design Methodology and Development of Pressure Swirl Atomizer for Micro Gas Turbine Combustion Chamber

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