航天推进技术研究院主办
[1]张雪梅,朱佳春.动力系统大气垫容积启动充填仿真及试验研究[J].火箭推进,2012,38(06):1-4.
ZHANG Xue-mei,ZHU Jia-chun.Filling simulation and test research of power system with large ullage volume[J].Journal of Rocket Propulsion,2012,38(06):1-4.
点击复制
ZHANG Xue-mei,ZHU Jia-chun.Filling simulation and test research of power system with large ullage volume[J].Journal of Rocket Propulsion,2012,38(06):1-4.
动力系统大气垫容积启动充填仿真及试验研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年06期
页码:
1-4
栏目:
研究与设计
出版日期:
2012-12-15
- Title:
- Filling simulation and test research of power system with large ullage volume
- 文章编号:
- 1672-9374(2012)06-0001-04
- Keywords:
- filling of systemsimulationtestAMESim
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 应用AMESim系统建模和仿真软件并考虑减压阀出口不同节流孔板孔径节流能力，建立了贮箱加注仅为满载加注量40％条件下的系统启动充填过程仿真模型。计算了电爆阀打开后贮箱出口压力变化曲线，获得系统初始充填时间。依据仿真结果结合系统实际情况完成系统冷试验证试验，试验结果与仿真计算数据基本一致。
- Abstract:
- According to throttle ability of different orifice plate at exit of pressure reducing valve, the simulation model of start-up and filling process under the condition of 40% full-load filling quantity was built with the software AMESim. The curves of pressure history at the tank’s exit were calculated after electric explosion valve was opened, and time of the start-up and filling process was obtained. Depending on the simulated results and actual condition of the system, cold test of the system was completed. The test results are coincident with the simulation results.
参考文献/References:
[1]付永领, 祁晓野． AMESim系统建模和仿真: 从入门到精通[M]． 北京: 北京航空航天大学出版社, 2006.
[2]白晓瑞． 液体火箭推进系统动态特性仿真研究[D]． 长沙:国防科技大学, 2008.
[3]张金荣，汪亮. 液体火箭发动机启动过程的动态仿真计算[J]. 低温工程, 2008 (2): 22-27.
[4]晋晓伟, 孙亮, 马健, 等. 推进剂供应系统增压过程仿真[J]. 火箭推进, 2009, 35(3): 30-34.
[5]王定军. 贮箱充填过程仿真和分析[J]. 火箭推进, 2008, 34(1): 23-25.
[6]杨晶, 杨凯, 黄敏超. 空间发动机启动过程的仿真[J]. 动力学与控制学报, 2006, 4(2): 187-192.
[7]张小平, 丁丰年. 富氧补燃循环发动机启动过程[J]. 推进技术, 2004, 25(1): 83-86.
[8]刘洪坤, 王维斌. 发动机启动燃气返腔仿真与影响分析[J]. 火箭推进, 2011, 37(2): 30-38.
[9]高明, 胡茑庆, 秦国军. 面对对象的推进剂加注系统建模与故障仿真[J]. 机床与液压, 2009, 37(9): 223-226.
[10]李锦江. 一种低温发动机系统动态仿真的快捷方法[J]. 导弹与航天运载技术, 2012 (1): 13-17.
[11]汪小卫, 金平, 张国舟, 等. 全流量补燃循环试验发动机启动过程[J]. 推进技术, 2008, 29(4): 407-411.
[12]汪小卫, 金平, 俞南嘉, 等. 富氧预燃室试验启动过程研究[J]. 航空动力学报, 2007, 22(12): 2119-2123.
[13]张育林, 刘昆, 程谋森.液体火箭发动机动力学理论与应用[M]. 北京: 科学出版社, 2005.
[14]刘红军, 张恩昭, 董锡鉴. 补燃循环发动机启动特性仿真研究[J]. 推进技术, 1999, 20(3): 5-9.
[15]刘昆, 张育林, 程谋森. 液体火箭发动机系统瞬变过程模块化建模与仿真[J]. 推进技术, 2003, 24(5): 18-22.
相似文献/References:
[1]刘海娃,汤建华.浮动断接器热控设计与仿真[J].火箭推进,2015,41(01):23.
LIU Hai-wa,TANG Jian-hua.Design and simulation of thermal control for floating coupling[J].Journal of Rocket Propulsion,2015,41(06):23.
[2]李 莹,潘宏亮,秦 飞,等.基于EASY5的液发系统建模与仿真可行性研究[J].火箭推进,2015,41(01):70.
LI Ying,PAN Hong-liang,QIN Fei,et al.Feasibility study on EASY5-based modeling and
simulation of liquid rocket engine[J].Journal of Rocket Propulsion,2015,41(06):70.
[3]窦 唯,胡长喜.液体火箭发动机水击特性仿真及试验研究[J].火箭推进,2013,39(02):40.
DOU Wei,HU Chang-xi.Simulation and testing research for water hammer characteristic of liquid rocket engine[J].Journal of Rocket Propulsion,2013,39(06):40.
[4]胡长喜.反向卸荷式减压阀动态建模与仿真[J].火箭推进,2014,40(01):60.
HU Chang-xi.Dynamic modeling and simulation for
converse unloading pressure reducing valve[J].Journal of Rocket Propulsion,2014,40(06):60.
[5]宋会玲,王春民,王云岩,等.集成控制双绕组高速电磁阀的设计与仿真分析[J].火箭推进,2012,38(06):16.
SONG Hui-ling,WANG Chun-min,WANG Yun-yan,et al.Design and simulation analysis of bi-coil high-speed solenoid valve with integrated control[J].Journal of Rocket Propulsion,2012,38(06):16.
[6]晋晓伟,孙亮,马键,等.推进剂供应系统增压过程仿真[J].火箭推进,2009,35(03):30.
Jin Xiaowei,Sun Liang,Ma Jian,et al.Simulation of the pressurizing process
of propellant feed system[J].Journal of Rocket Propulsion,2009,35(06):30.
[7]王定军,袁洪滨,董苑.贮箱充填过程仿真和分析[J].火箭推进,2008,34(01):23.
Wang Dingjun,Yuan Hongbin,Dong Yuan.Simulation and analysis of the tank filling process[J].Journal of Rocket Propulsion,2008,34(06):23.
[8]戴佳,黄敏超,余勇,等.电磁阀动态响应特性仿真研究[J].火箭推进,2007,33(01):40.
Dai Jia,Huang Minchao,Yu Yong,et al.Simulation on the dynamic response characteristics of solenoid valve[J].Journal of Rocket Propulsion,2007,33(06):40.
[9]汪洪波,王振国,孙明波,等.预燃室低频不稳定燃烧仿真研究[J].火箭推进,2007,33(05):22.
Wang Hongbo,Wang Zhenguo,Sun Mingbo.Simulation investigations of low frequency combustion instability of precombustion chamber[J].Journal of Rocket Propulsion,2007,33(06):22.
[10]马红宇,段小龙,刘红军,等.落压式供应发生器试验系统动态仿真[J].火箭推进,2007,33(05):55.
Ma Hongyu,Duan Xiaolong,Liu Hongjun.Dynamic simulation for a blow down feed test system of a gas generator[J].Journal of Rocket Propulsion,2007,33(06):55.
备注/Memo
收稿日期：2011-09-28；修回日期：2012-10-11
基金项目：国家863项目（2008AA702303）
作者简介：张雪梅（1979—），女，高级工程师，研究领域为姿轨控发动机系统
更新日期/Last Update:
1900-01-01