Abstract:When the main components meet the performance requirements, weight reduction is of positive significance to increase the thrust-to-weight ratio of small turbojet engines. Analyzing the space structure of the small turbojet engine, choosing the integral impeller for lightweight design, and giving a preliminary hollow structure plan. Based on the additive–subtractive hybrid manufacturing, this paper designed the complete process and testing plan of the hollow centrifugal impeller, using Powermill software to verify the process and optimize the additive–subtractive hybrid manufacturing. The feasibility of the overall process is verified through the additive–subtractive hybrid manufacturing, and the machining accuracy of the hollow centrifugal impeller is inspected to verify the machining accuracy. The application of the additive–subtractive hybrid manufacturing has positive significance for the process design of complex structures.
高凯,王振忠,孔刘伟,孔洋波,侯亮. 基于增减材复合制造的中空离心叶轮工艺设计[J]. 航空制造技术, 2021, 64(12): 72-79/84.
GAO Kai, WANG Zhenzhong, KONG Liuwei, KONG Yangbo, HOU Liang. Process Design of Hollow Centrifugal Impeller Based on Additive–Subtractive Hybrid Manufacturing. Aeronautical Manufacturing Technology, 2021, 64(12): 72-79/84.