航天推进技术研究院主办
[1]朱子环,耿卫国,管 理,等.某型号大推力火箭发动机试验推力测量不确定度评定[J].火箭推进,2012,38(05):81-85.
ZHU Zi-huan,GENG Wei-guo,GUAN Li,et al.Assessment of thrust measurement uncertainty for test of large thrust rocket engine[J].Journal of Rocket Propulsion,2012,38(05):81-85.
点击复制
ZHU Zi-huan,GENG Wei-guo,GUAN Li,et al.Assessment of thrust measurement uncertainty for test of large thrust rocket engine[J].Journal of Rocket Propulsion,2012,38(05):81-85.
某型号大推力火箭发动机试验推力测量不确定度评定
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年05期
页码:
81-85
栏目:
测控与试验
出版日期:
2012-10-15
- Title:
- Assessment of thrust measurement uncertainty for test of large thrust rocket engine
- 文章编号:
- 1672-9374(2012)05-0081-05
- Keywords:
- rocket engine; thrust measurement; measurement uncertainty
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 根据某型号大推力火箭发动机试验推力测量系统的工作原理和组成、计量标准量值传递关系和系统低温调试结果，确定推力测量系统的不确定度来源，通过进一步的误差分析并应用误差计算理论对系统不确定度进行评定，得出该系统测量不确定度作为推力测量准确性依据。
- Abstract:
- The uncertainty source of the thrust measure system was determined on the basis of the working principle, composition, metrological standard value transitive relation and low temperature debugging result of thrust measurement system for a large thrust rocket engine. The test uncertainty of the thrust measurement system was assessed by error analysis and theory of error calculation. The test uncertainty of the system was obtained, which is taken as an evidence for accuracy of thrust measurement. The method can be taken as a reference for thrust measurement assessment for other types of rocket engines.
参考文献/References:
[1]杨生发, 樊丁, 李元业. 发动机推力测量新型校准装置的研制[J]. 西北工业大学学报, 1997 (3): 18-22.
[2]谢显奇. 液氢－液氧发动机的推力测量[J]. 导弹与航天运载技术, 1997 (2): 61-64.
[3]费业泰. 误差理论与数据处理[M]. 北京: 机械工业出版社, 2004.
[4]荆凤林, 陶汉铭. 某型固体火箭发动机推力测量不确定度评定[J]. 推进技术, 1998 (2): 101-105.
[5]杜鹤龄. 航空发动机推力的测量和确定方法[J]. 航空动力学报, 1997 (4): 54-57.
[6]马云华, 蒋光林. 推力架测试系统误差的研究[J]. 宇航计测技术, 2005 (2): 23-26.
[7]刘伟亮, 吴建军. 机电一体化推力测量系统的研制及应用[J]. 火箭推进, 2004, 30(6): 50-54.
[8]郭昕, 刘涛, 文刚. 航空发动机试车台附加阻力修正方法[J]. 航空动力学报, 2003 (6):129-134.
相似文献/References:
[1]朱舒扬.全尺寸超燃冲压发动机推力测量台架研制[J].火箭推进,2015,41(05):106.
ZHU Shuyang.Development of thrust measurement platform
for full-scale scramjet[J].Journal of Rocket Propulsion,2015,41(05):106.
[2]霍世慧,袁军社,徐学军,等.双推力室机架快速优化设计方法研究[J].火箭推进,2015,41(04):55.
HUO Shihui,YUAN Junshe,XU Xuejun,et al.A rapid optimization design method for frame structure
of double thrust chambers[J].Journal of Rocket Propulsion,2015,41(05):55.
[3]沈继彬,曾晓军,曹庆红.泵前管道波纹管对推力测量的影响分析[J].火箭推进,2015,41(04):95.
SHEN Jibin,ZENG Xiaojun,CAO Qinghong.Analysis of effects of bellows in front of
pump on thrust measurement[J].Journal of Rocket Propulsion,2015,41(05):95.
[4]沈传兵,苏 杭,朱子勇.基于PLC和WinCC的火箭发动机热真空试验控制系统[J].火箭推进,2015,41(03):93.
SHEN Chuan-bing,SU Hang,ZHU Zi-yong.Control system for liquid rocket engine heat-vacuum
test based on PLC and WinCC[J].Journal of Rocket Propulsion,2015,41(05):93.
[5]刘万龙,牛向楠,李全令,等.一种姿轨控发动机地面试验控制系统设计[J].火箭推进,2015,41(02):114.
LIU Wan-long,NIU Xiang-nan,LI Quan-ling,et al.Design of a ground test control system for attitude
and orbital control engine[J].Journal of Rocket Propulsion,2015,41(05):114.
[6]段文浩,于 涛,杨 莹.辐射式热流测量系统及其应用[J].火箭推进,2014,40(01):85.
DUAN Wen-hao,YU Tao,YANG Ying.Radiant heat flux measuring system and its application[J].Journal of Rocket Propulsion,2014,40(05):85.
[7]黄子惟,田松岩,商圣飞.基于双光束干涉原理的微小推力测量系统实验研究[J].火箭推进,2014,40(05):80.
HUANG Zi-wei,TIAN Song-yan,SHANG Sheng-fei.Experimental investigation on micro-thrust measurement system based on double-beam interference principle[J].Journal of Rocket Propulsion,2014,40(05):80.
[8]周奎,吴伟亮,张玫宝.火箭发动机喷雾均匀性数值分析[J].火箭推进,2010,36(02):26.
Zhou Kui,Wu Weiliang,Zhang Meibao.Numerical analysis on uniformity of spray in rocket engines[J].Journal of Rocket Propulsion,2010,36(05):26.
[9]朱子环.液体火箭发动机试验推力测量传感器并联影响研究[J].火箭推进,2010,36(02):59.
Zhu Zihuan.Investigation of parallel connection of thrust sensors on measurement precision in liquid rocket engine tests[J].Journal of Rocket Propulsion,2010,36(05):59.
[10]张涛,唐虎,周江平,等.可贮存推进剂泵压式液体火箭发动机多次起动系统研究[J].火箭推进,2010,36(03):15.
Study on the multi-start system of turbopump-fed rocket engine with storable propellants[J].Journal of Rocket Propulsion,2010,36(05):15.
备注/Memo
收稿日期：2011-09-16；修回日期：2012-08-28
基金项目：国家863项目（2008AA702303)
作者简介：朱子环（1977—），女，高级工程师，研究领域为液体火箭发动机试验推力测量技术及仿真
更新日期/Last Update:
1900-01-01