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Core shift limitation in investment casting process of hollow turbine blade

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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%.

Hollow turbine bladeWall thicknessCeramic coreShift predictionFixturing layout optimization

Kang CUI、Lin JING、Ruisong JIANG、Longnv YU、Xiao GAO

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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

School of Mechanical Engineering,Sichuan University,Chengdu 610065,China

National Natural Science Foundation of ChinaScientific and the National Science and Technology Major ProjectShanxi Scholarship Council of China

52005311J2019-VⅡ-0013-01532023-003

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
年,卷(期):2024.37(8)
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