Advances in Aeroengine Cooling Hole Measurement: A Comprehensive Review

Author:

Yan Shuyan123,Shi Junkai1ORCID,Li Guannan1,Hao Can12,Wang Ying1,Yu Hao3,Zhou Weihu12

Affiliation:

1. Institute of Microelectronics of the Chinese Academy of Sciences, Beijing 100029, China

2. University of Chinese Academy of Sciences, Beijing 100049, China

3. China Aviation Planning and Design Institute (Group) Co., Ltd., Beijing 100120, China

Abstract

Film cooling technology is of great significance to enhance the performance of aero-engines and extend service life. With the increasing requirements for film cooling efficiency, researchers and engineers have carried out a lot of work on the precision and digital measurement of cooling holes. Based on the above, this paper outlines the importance and principles of film cooling technology and reviews the evolution of cooling holes. Also, this paper details the traditional measurement methods of the cooling hole used in current engineering scenarios with their limitations and categorizes digital measurement methods into five main types, including probing measurement technology, optical measurement technology, infrared imaging technology, computer tomography (CT) scanning technology, and composite measurement technology. The five types of methods and integrated automated measurement platforms are also analyzed. Finally, through a generalize and analysis of cooling hole measurement methods, this paper points out technical challenges and future trends, providing a reference and guidance for forward researches.

Funder

National Key Research and Development Program of China

Publisher

MDPI AG

Reference83 articles.

1. Han, J.C., Dutta, S., and Ekkad, S. (2012). Gas Turbine Heat Transfer and Cooling Technology, CRC Press. [2nd ed.].

2. Research Progress on Phosphor Thermometry Technology for Aero Engine Hot Section Components;Liu;J. Aerosp. Power,2023

3. Ding, S.T., Liu, C.K., Qiu, T., and Li, G. (2021). A Combined Cycle Method of Primary and Secondary Flows in Turbine Engines. (CN111237085B), Patent.

4. Review and Prospect of the Development of Casting Superalloys;Chen;J. Aeronaut. Mater.,2000

5. Cumpsty, N.A. (1997). Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines, Cambridge University Press.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3