汤张喆,孙玉利,王利峰,朱力敏,柯泰龙,左敦稳. 伺服交叉孔零件磨粒流去毛刺仿真研究及试验验证[J]. 航空制造技术, 2023, 66(23/24): 86-93. TANG Zhangzhe, SUN Yuli, WANG Lifeng, ZHU Limin, KE Tailong, ZUO Dunwen. Simulation Research and Experimental Verification of Abrasive Flow Deburring for Servo Intersecting-Holes Parts[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24): 86-93.
TANG Zhangzhe, SUN Yuli, WANG Lifeng, et al. Simulation Research and Experimental Verification of Abrasive Flow Deburring for Servo Intersecting-Holes Parts[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24).
汤张喆,孙玉利,王利峰,朱力敏,柯泰龙,左敦稳. 伺服交叉孔零件磨粒流去毛刺仿真研究及试验验证[J]. 航空制造技术, 2023, 66(23/24): 86-93. TANG Zhangzhe, SUN Yuli, WANG Lifeng, ZHU Limin, KE Tailong, ZUO Dunwen. Simulation Research and Experimental Verification of Abrasive Flow Deburring for Servo Intersecting-Holes Parts[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24): 86-93. DOI: 10.16080/j.issn1671-833x.2023.23/24.086.
TANG Zhangzhe, SUN Yuli, WANG Lifeng, et al. Simulation Research and Experimental Verification of Abrasive Flow Deburring for Servo Intersecting-Holes Parts[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24). DOI: 10.16080/j.issn1671-833x.2023.23/24.086.
Simulation Research and Experimental Verification of Abrasive Flow Deburring for Servo Intersecting-Holes Parts
and poor consistency of the existing burr removal process for the intersecting-hole parts top shell in the servo mechanism
a suggestion of using the abrasive flow deburring process was proposed. Through the analysis of the internal structure of the workpiece and the planning of the deburring processing path
the runner simulation model of each processing path was established
and the flow field characteristics of the corresponding path of each inlet runner group were compared
analyzed and optimized for better process path. Deburring verification experiments were carried out on the top shell workpiece. The results show that the uneven distribution of the streamline inside the flow channel and the large difference in the streamline pressure can be effectively improved by increasing the drainage section structure at the exit of the large hole and extending the length of the flow channel. Finally
the problem of inconsistent burr removal effect during processing can be solved and the sharp edges at the entrance and exit can also be effectively protected. After the experiment
the internal burrs of the runner are removed
and the edges of the internal small holes are rounded
which improves the surface quality and performance of the workpiece.