|Table of Contents|

Application of extrusion grinding technology in burr removal of solenoid valve spool(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年03期
Page:
93-98
Research Field:
工艺与材料
Publishing date:

Info

Title:
Application of extrusion grinding technology in burr removal of solenoid valve spool
Author(s):
LIU XiangCAO Feilong LI Xuguang LI Bo
(Xian Aerospace Engine Co.,Ltd., Xian 710100, China)
Keywords:
solenoid valve spool intersecting holes extrusion grinding burr removal prevention and control of surplus material
PACS:
V261
DOI:
-
Abstract:
In order to remove burrs at the intersecting small holes in the machined solenoid valve spool, so as to avoid the surplus material in the valve cavity after the burrs falling off from the base metal, it was proposed that using the extrusion grinding technology to remove burrs at the intersecting small holes after identifying the burr locations of the solenoid valve spool and learning the limitations of the conventional deburring methods.In addition, the prevention and control scheme of surplus material for extrusion grinding technology was proposed, and the orthogonal experiments was designed and carried out to obtain the optimal parameters in extrusion grinding technology that can effectively remove the burr at the intersecting hole and avoid the secondary generation of surplus material.By removing burrs at the intersecting small holes with the extrusion grinding technology after manufacturing the solenoid valve spool, the intersecting small holes of parts have the advantages of no burrs, no residual abrasives and good consistency of processing state.Compared with the conventional schemes, the deburring efficiency is improved by more than 60 with this method.The extrusion grinding technology can remove the burr at the intersecting small holes effectively and provide an engineering reference scheme for the burr removal at the intersection hole of the narrow inner cavity in other similar parts.

References:

[1] 朱宁昌.液体火箭发动机设计(上)[M].北京:宇航出版社,1994.
[2] 史秋明,谢荣华.电磁阀滑动副的设计参数灵敏度分析与可靠性研究[J].火箭推进,2013,39(3):72-78.
SHI Q M,XIE R H.Design sensitivity analysis and reliability research on sliding pairs of solenoid valve[J].Journal of Rocket Propulsion,2013,39(3):72-78.
[3] 牛书锋,张国悦.液氧/煤油发动机多余物自动检测技术[J].火箭推进,2019,45(4):69-73.
NIU S F,ZHANG G Y.Automatic detection technology of redundancy in LOX/kerosene engine[J].Journal of Rocket Propulsion,2019,45(4):69-73.
[4] 秦永涛,宋阳,苏红芳,等.火箭发动机试验管道多余物人机环境控制方法[J].火箭推进,2015,41(6):80-85.
QIN Y T,SONG Y,SU H F,et al.Method of man-machine-environment control over foreign object debris in pipelines used in rocket engine test[J].Journal of Rocket Propulsion,2015,41(6):80-85.
[5] 戴根林.磨料流技术去除交叉孔毛刺[J].航天制造技术,2002(1):25-28.
[6] 董志国.磨料流加工的切削机理及加工工艺的研究[D].太原:太原理工大学,2012.
[7] 陈曦,刘军.磨粒流技术在航天零件相贯孔去毛刺中的应用[J].金属加工(冷加工),2014(16):30-33.
[8] 高航,吴鸣宇,付有志,等.流体磨料光整加工理论与技术的发展[J].机械工程学报,2015,51(7):174-187.
[9] 赵奔,魏凯,刘超,等.高压开关液压机构零件热能法去毛刺工艺研究[J].高压电器,2013,49(3):134-138.
[10] 温从众,耿艳娟,李苹.液压腔体零件交接孔热能去毛刺工艺研究[J].机床与液压,2016,44(16):33-35.
[11] 中国航天科技集团公司7103厂.热能去毛刺工艺研究[J].航天制造技术,2002(1):14-15.
[12] 柏余杰.微小孔精密挤压研磨工艺与控制方法研究[D].上海:上海大学,2016.
[13] 李俊烨,许颖,杨立峰,等.非直线管零件的磨粒流加工实验研究[J].中国机械工程,2014,25(13):1729-1733.
[14] 郭成宇.微小孔磨粒流抛光机理及实验研究[D].长春:吉林大学,2016.
[15] 王忠,王凯,王鹏,等.挤压研磨对喷油器流量及雾化性能的影响[J].江苏大学学报(自然科学版),2019,40(5):497-503.
[16] 石岩,郭志,刘佳,等.SLM增材制造微流道内表面磨粒流抛光工艺与机理[J].表面技术,2021,50(9):361-369.
[17] 李俊烨,朱志宝,张心明,等.异形截面孔磨粒流精密加工质量分析[J].中国机械工程,2021,32(17):2063-2073.
[18] 段泽斌,轧刚,董志国,等.可控倒锥角微孔磨料流加工成形研究[J].机械设计与制造,2018(3):116-119.
[19] 刘月普.倒锥形微细喷孔磨料加工成型研究[D].太原:太原理工大学,2014.
[20] 闫波,张方东,黄铁军,等.基于磨料流加工技术叶片泵转子去毛刺试验研究[J].机床与液压,2020,48(4):67-70.

Memo

Memo:
-
Last Update: 1900-01-01