The Design of The Space Engine Fan Blade Cooling System Based on Cooling Strategy

Main Article Content

Deyong Li
Haixia Yao
Yong Zhan
Hongyan Zou
Hang Yang

Abstract

The fan blades in the subsonic intake of jet aero engines have an important impact on the efficiency of the aircraft, whether the engine is working normally, and the size of the thrust. In view of the current problems in the design of jet aero engine blades, this paper carries out the design of the shape and number of engine blades. First of all, some of the current problems with heat dissipation in the engine blades are analyzed. Secondly, based on how to improve the cooling effect of the air intake fan blade of the jet aircraft engine, the design of the fan blade in the engine air intake was carried out. Finally, the 3D modeling software has been used to improve the engine air intake fan blades. The design results show that the desired effect is achieved for increasing the number of blades of the fan blade and improving its shape, and the cooling effect on the engine is improved.

Article Details

How to Cite
Li, D., Yao, H., Zhan, Y., Zou, H., & Yang, H. (2022). The Design of The Space Engine Fan Blade Cooling System Based on Cooling Strategy. Journal of Research in Multidisciplinary Methods and Applications, 1(1), 01220101003. Retrieved from http://www.satursonpublishing.com/jrmma/article/view/a01220101003
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Articles

References

LI Jing, TIAN Qingzheng, ZHOU Qitao. Design and verification of turbine blade cooling scheme based on pipe network calculation. Gas Turbine Technology, 2022, 35(01): 30-34.

LÜ Song, WU Fayong, WANG Hongbin, GE Hongzhi. Interaction effect analysis and experimental study of influencing factors of turbine blade cooling effect. Propulsion Technology, 2022, 43(05):278-289.]

LIU Guangdong, LIU Xianglan. Research on processing method of thin-walled integral centrifugal impeller in precision inner cavity of aerospace engine. Mechanical Engineer, 2021(12): 162-164.

WANG Jiao, WANG Junli, YANG Yongle, JIANG Peng, LI Yanqing. Development and application of a high-performance oxygen pressure reducer for aerospace engines. Mechanical Engineer, 2021(06):77-78+82.

QU Hongliang, SU Yunling, YAO Zhiqi, TIAN Hui, WANG Yongfei. Research on manufacturing process technology of gearbox for new generation aerospace engine. New Technologies and New Processes, 2021(05): 19-23

LI Yazhong, WEI Kuan, MIAO Hui. A brief analysis of turbine blade cooling structure design and test method. Aeronautical Dynamics, 2020(06): 59-61.

GUO Wen, WANG Pengfei. Analysis of turbine blade cooling technology. Aeronautical Power, 2020(06): 55-58.

XIA Kailong, GE Chao, WANG Qiutong, HE Zhen. Research progress on detection technology of cooling air film pores and coating defects of turbine blades. Aviation manufacturing technology:1-13.

JIA Kai, GUO Xinxin, CHENG Quanshi, LI Zhao, ZHAO Liping, HE Dingxuan. Analysis of the causes of corrosion of screws in aerospace engines. Electroplating and Finishing, 2020, 39(17): 1184-1186.

ZHOU Lingmin, WANG Bo, WEI Jiaming, ZHUANG Daming, LI Yiman. Gas turbine blade cooling test technology. Aeronautical Dynamics, 2020(04): 27-30.

LIU Qiang, XU Zhengyang. Design and experimental study of flow field for electrolytic processing of aerospace engine blades. Machinery Manufacturing and Automation, 2020, 49(02): 54-59

ZHANG Shihong, CHENG Ming, SONG Hongwu, XU Yong. Research progress on precision forming technology of aerospace complex surface components. Journal of Nanjing University of Aeronautics and Astronautics, 2020, 52(01):1-11.]

MA Chao, HUANG Minghai, ZANG Shusheng. Comparative analysis of the cooling performance of turbine blades under two cooling media: air and steam. Thermal Science and Technology, 2014, 13(02):169-175.]

Chi Zhongran. Mechanism of action and design optimization method of turbine cooling structure of gas turbine. Tsinghua University, 2014.]

SONG Hongwen, WU Wei. Application of special processing in aerospace manufacturing industry. Mechanical Design and Manufacturing, 2009(02): 266-268.

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