航天推进技术研究院主办
HAN Lei,HE Wei-dong.Digitization process technology of cooling grooves on nozzle of liquid-propellant rocket engine[J].Journal of Rocket Propulsion,2014,40(04):57-61.
液体火箭发动机喷管冷却槽数字化加工技术
- Title:
- Digitization process technology of cooling grooves on nozzle of liquid-propellant rocket engine
- 分类号:
- V434.2-33
- 文献标志码:
- A
- 摘要:
- 主要针对现有液体火箭发动机喷管冷却槽数字化加工方法与工艺技术存在的精度保证与效率提升难题,在已开发的加工工艺和加工系统的基础上,重点研究了局部光亮面蓝油处理技术,在喷管光亮面均匀涂抹蓝油以降低局部反光程度,局部光亮区域经蓝油处理后的激光测量精度得到改善。激光传感器可靠校准技术,借助于三角形辅助支架安装激光传感器在滑枕端部,保证传感器安装后的位置是固定不变。自动清根加工技术是利用软件生成程序,执行清根程序,人工调整角度分度。在某喷管产品上对上述关键加工革新技术进行了工艺试验验证。通过验证试验,加工后的喷管槽深及壁厚尺寸误差均控制公差范围以内,较好地满足了喷管尺寸精度要求。应用于实际生产中,自动化加工比例提升,零件合格率提升,加工效率提高了30%。
- Abstract:
- To solve the problems that the accuracy can not be guaranteed and the efficiency is difficult to improve, which exist in digitization processing method and technology of the cooling grooves on nozzle liquid rocket engine, the technology of local bright surface treatment with blue oil is proposed on the basis of the developed processing technology and system. The degree of partial reflection can be reduced by painting blue oil evenly on the bright surface of the nozzle. The laser measurement accuracy was improved with the local bright surface treatment with blue oil. By means of triangle auxiliary bracket mounted on the end portion of the ram, the reliable calibration technology of laser sensors can ensure that the position of laser sensors is fixed. The proposed software is utilized in the automatic root clearing technology nozzle products. The experimental results show the errors of the groove depth and wall thickness were controlled within the tolerance range and met the requirements of dimensional accuracy of the nozzle. With the technologies, the proportion of automatic processing in actual production was increased, the qualified rate of the parts was improved and the processing efficiency was increased by 30%.
参考文献/References:
[1]谭永华. 中国重型火箭动力系统研究[J].火箭推进, 2011, 37(1): 1-6.
[2]SUTTON G P. History of liquid-propellant rocket engines in Russia, formerly the Soviet Union[J]. Journal of Propul- sion and Power, 2003, 19(6): 1008-1037.
[3]卢杰持, 胡力耘, 杨金奎, 等. 火箭大喷管数控仿形铣槽控制系统[J]. 大连理工大学学报, 1998, 38(3): 296-299.
[4]靳惠敏, 薛引慧. 数控仿形铣槽机床仿形系统的设计与改造[J]. 航天制造技术, 2007 (5): 16-19.
[5]吕明云, 祝明, 王焕, 等. 复杂曲面FSS加工系统研究[J].航空学报, 2005, 26(4): 26-32.
[6]王永青, 卢杰持, 王春, 等. 大型航天火箭喷管铣槽加工系统 [J]. 组合机床与自动化技术, 2000 (10): 25-27.
[7]大连理工大学. 液体火箭发动机喷管直槽冷却通道立式加工方法: 中国, 200810229225.9[P]. 2009-04-22.
相似文献/References:
[1]郑 伟,李护林,陈新红.激光快速成形技术在液体动力领域的应用前景[J].火箭推进,2015,41(06):1.
ZHENG Wei,LI Hulin,CHEN Xinhong.Application prospect of laser rapid prototyping
technology in the field of liquid power[J].Journal of Rocket Propulsion,2015,41(04):1.
[2]郭 敬,宋晶晶,孔凡超.发动机推进剂增压输送系统建模仿真技术综述[J].火箭推进,2015,41(05):1.
GUO Jing,SONG Jingjing,KONG Fanchao.Overview of modeling and simulation technology
for propellant pressurization feed system
of liquid rocket engine[J].Journal of Rocket Propulsion,2015,41(04):1.
[3]徐学文,牟俊林,任建存,等.固体火箭发动机喷管瞬态流场特性分析[J].火箭推进,2015,41(05):49.
XU Xuewen,MU Junlin,REN Jiancun,et al.The analyses of transient flow-field
characteristics in the nozzle of SRM[J].Journal of Rocket Propulsion,2015,41(04):49.
[4]于 康,谢荣华,陈晓江.表面张力贮箱电子束焊接工艺研究[J].火箭推进,2015,41(05):89.
YU Kang,XIE Ronghua,CHEN Xiaojiang.Study on electron beam welding process
for surface tension tank[J].Journal of Rocket Propulsion,2015,41(04):89.
[5]刘中华,苏 晨,汪军安,等.气路膜片设计研究[J].火箭推进,2015,41(05):95.
LIU Zhonghua,SU Chen,WANG Junan,et al.Design and study of pneumatic diaphragm in gas circuit[J].Journal of Rocket Propulsion,2015,41(04):95.
[6]梁俊龙,张贵田,秦艳平.基于高阶WENO格式的喷管动态特性仿真分析[J].火箭推进,2015,41(04):29.
LIANG Junlong,ZHANG Guitian,QIN Yanping.Simulated analysis on nozzle dynamic characteristics
based on high-order WENO scheme[J].Journal of Rocket Propulsion,2015,41(04):29.
[7]薛 薇,蔡震宇,曹红娟,等.基于可视化平台的液氢/液氧火箭发动机核心部件质量计算[J].火箭推进,2015,41(04):61.
XUE wei,CAI Zhenyu,CAO Hongjuan,et al.Mass calculation of key assembly units in
LH2/ LOX rocket engine based on visual interface[J].Journal of Rocket Propulsion,2015,41(04):61.
[8]穆朋刚,童 飞,蒲光荣,等.温度对贮箱增压系统的影响分析[J].火箭推进,2015,41(04):74.
MU Penggang,TONG Fei,PU Guangrong,et al.Influence of temperature on tank pressurization system[J].Journal of Rocket Propulsion,2015,41(04):74.
[9]高朝辉,刘 宇,肖 肖,等.垂直着陆重复使用运载火箭对动力技术的挑战[J].火箭推进,2015,41(03):1.
GAO Zhao-hui,LIU Yu,et al.Challenge to propulsion technology for vertical
landing reusable launch vehicle[J].Journal of Rocket Propulsion,2015,41(04):1.
[10]申智帅,等.气动增压器技术及其在空间推进系统的应用[J].火箭推进,2015,41(03):15.
SHEN Zhi-shuai,RUAN Hai-jun,et al.Pneumopump technology and its application
in space propulsion system[J].Journal of Rocket Propulsion,2015,41(04):15.
[11]陈曦.喷管后段内壁铣槽加工工艺[J].火箭推进,2006,32(04):48.
Chen Xi.Milling groove machining of inner wall of nozzle extension[J].Journal of Rocket Propulsion,2006,32(04):48.
备注/Memo
收稿日期:2014-03-31;修回日期:2014-04-14 基金项目:中国航天科技集团公司支撑项目(2011JY13) 作者简介:韩磊(1971—),男,技师,研究领域为火箭发动机铣槽加工方法与工艺技术