中国航空学报(英文版)2024,Vol.37Issue(8) :513-526.DOI:10.1016/j.cja.2023.12.001

Core shift limitation in investment casting process of hollow turbine blade

Kang CUI Lin JING Ruisong JIANG Longnv YU Xiao GAO
中国航空学报(英文版)2024,Vol.37Issue(8) :513-526.DOI:10.1016/j.cja.2023.12.001

Core shift limitation in investment casting process of hollow turbine blade

Kang CUI 1Lin JING 2Ruisong JIANG 3Longnv YU 2Xiao GAO2
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作者信息

  • 1. Automation and Software Engineering,Shanxi University,Taiyuan 030006,China;Key Laboratory of High Performance Manufacturing for Aero Engine,Ministry of Industry and Information Technology,School of Mechanical Engineering,Northwestern Polytechnical University,Xi'an 710072,China
  • 2. Automation and Software Engineering,Shanxi University,Taiyuan 030006,China
  • 3. School of Mechanical Engineering,Sichuan University,Chengdu 610065,China
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Abstract

The deviation in wall thickness caused by core shift during the investment casting process significantly impacts the strength and service life of hollow turbine blades.To address this issue,a core shift limitation method is developed in this study.Firstly,a shift model is established based on computational fluid dynamics and motion simulation to predict the movement of the ceramic core in investment casting process.Subsequently,utilizing this model,an optimization method for fixtur-ing layout inside the refractory ceramic shell is devised for the ceramic core.The casting experiment demonstrates that by utilizing the optimized fixture layout,not only can core shift during the invest-ment casting pouring process be effectively controlled,but also the maximum wall thickness error of the blade can be reduced by 42.02%.In addition,the core shift prediction is also validated,with a prediction error of less than 26.9%.

Key words

Hollow turbine blade/Wall thickness/Ceramic core/Shift prediction/Fixturing layout optimization

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基金项目

National Natural Science Foundation of China(52005311)

Scientific and the National Science and Technology Major Project(J2019-VⅡ-0013-0153)

Shanxi Scholarship Council of China(2023-003)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量3
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