六分力测试静态性能标定方法

林涛; 彭澎; 司欣格; 李大海; 张永建; 狄长安

doi:10.13224/j.cnki.jasp.20230335

六分力测试静态性能标定方法

doi: 10.13224/j.cnki.jasp.20230335

南京理工大学机械工程学院，南京 210000

详细信息

作者简介:
林涛（1995-），男，博士生，主要从事仪器科学与技术方面的研究

中图分类号: V216
计量
- 文章访问数: 567
- HTML浏览量: 344
- PDF量: 45
- 被引次数: 0
出版历程
- 收稿日期: 2023-05-20
- 网络出版日期: 2024-07-23

Static performance calibration method for six-component force testing

School of Mechanical Engineering，Nanjing University of Science and Technology，Nanjing 210000，China

摘要

摘要:
为准确地获取某型发动机偏航、俯仰、主推力等工作性能，在前人研究的基础之上，研制出一种发动机四支点六分量测试台架，该台架集发动机推力测试和静态性能标定于一体，实现了对某型发动机的推力测量。介绍了测量系统和静态性能标定方法，并进行了测力单元静态标定试验。试验结果表明所设计的动态六分力测试台测量精度较高，总体相对误差为0.31%。
- 四支点六分量 /
- 发动机推力 /
- 测力方法 /
- 静态标定 /
- 六分力
Abstract:
In order to accurately obtain the yaw, pitch and main thrust performance of an engine, a four-fulcrum and six-component engine testing platform was developed on the basis of previous studies. This platform integrated thrust test and static performance calibration of an engine, and realized thrust measurement of a certain engine. The measuring system and static performance calibration method were introduced, and the static calibration test of force measuring unit was carried out. The test results showed that the designed dynamic six-component force tester had high measuring accuracy, with the overall relative error of 0.31%.
- four-fulcrum six-components /
- engine thrust /
- force measurement method /
- static calibration /
- six-component force

HTML

图 1 六分力测试台架结构图

Figure 1. Structural diagram of the six-component force testing platform

下载: 全尺寸图片幻灯片

图 2 四支点六分量测试平台力传感器布置示意图

Figure 2. Schematic diagram of force sensor arrangement on four-point six-component testing platform

下载: 全尺寸图片幻灯片

图 3 标定单元结构组成

Figure 3. Composition of calibration unit structure

下载: 全尺寸图片幻灯片

图 4 X向数据拟合图

Figure 4. Data fitting graph in the X-direction

下载: 全尺寸图片幻灯片

图 5 Y向数据拟合图

Figure 5. Data fitting graph in the Y-direction

下载: 全尺寸图片幻灯片

图 6 Z向数据拟合图

Figure 6. Data fitting graph in the Z-direction

下载: 全尺寸图片幻灯片

表 1 X轴正向标定测试

Table 1. X direction positive calibration test

输入载荷/N	电压输出/V	相对误差/%	线性度/%
0	0	0	0
805.52	0.40	−0.05	−0.01
1313.01	0.65	−0.20	−0.05
1769.19	0.88	−0.28	−0.10
2251.68	1.11	−1.01	−0.46
2826.10	1.39	−0.96	−0.55
3223.49	1.59	−0.38	−0.25
3753.18	1.85	−0.48	−0.37
4176.16	2.06	−0.42	−0.36
4654.24	2.30	−0.41	−0.39

下载: 导出CSV

参考文献(24)

[1]	刘万龙,王得志,刘硕,等. 几种国外火箭发动机推力矢量测量装置概述[J]. 火箭推进,2021,47(4): 6-12. LIU Wanlong,WANG Dezhi,LIU Shuo,et al. Several foreign rocket engine thrust vector measuring devices[J]. Journal of Rocket Propulsion,2021,47(4): 6-12. (in Chinese LIU Wanlong, WANG Dezhi, LIU Shuo, et al. Several foreign rocket engine thrust vector measuring devices[J]. Journal of Rocket Propulsion, 2021, 47(4): 6-12. (in Chinese)
[2]	解亮,李庆林,张驰,等. 三轴承推力矢量喷管推力性能试验研究[J]. 航空发动机,2021,47(5): 26-33. XIE Liang,LI Qinglin,ZHANG Chi,et al. Test study on thrust performance of 3-bearing swivel duct nozzle[J]. Aeroengine,2021,47(5): 26-33. (in Chinese XIE Liang, LI Qinglin, ZHANG Chi, et al. Test study on thrust performance of 3-bearing swivel duct nozzle[J]. Aeroengine, 2021, 47(5): 26-33. (in Chinese)
[3]	罗华云,赖传兴,王月贵,等. 喷管模型试验器六分量天平校准技术[J]. 航空动力学报,2013,28(1): 67-73. LUO Huayun,LAI Chuanxing,WANG Yuegui,et al. Six-component balance calibration technology for nozzle model testing facility[J]. Journal of Aerospace Power,2013,28(1): 67-73. (in Chinese LUO Huayun, LAI Chuanxing, WANG Yuegui, et al. Six-component balance calibration technology for nozzle model testing facility[J]. Journal of Aerospace Power, 2013, 28(1): 67-73. (in Chinese)
[4]	李贝. 发动机推力试车台推力测量分析及其特性仿真研究[D]. 哈尔滨: 哈尔滨工业大学,2017. LI Bei. Research on measurement and simulation of engine thrust test stand[D]. Harbin: Harbin Institute of Technology,2017. (in Chinese LI Bei. Research on measurement and simulation of engine thrust test stand[D]. Harbin: Harbin Institute of Technology, 2017. (in Chinese)
[5]	WRIGHT A M,WRIGHT A B,BORN T,et al. A six degree-of-freedom thrust sensor for a labscale hybrid rocket[J]. Measurement Science and Technology,2013,24(12): 125104. doi: 10.1088/0957-0233/24/12/125104
[6]	COOK M,GRUET L. Characterization of space shuttle reusable solid rocket motor static test stand thrust measurements[R]. AIAA 2003-280,2003.
[7]	KIRK D,BRIMHALL Z,DIVITOTAWELA N,et al. Design and validation of a six degree of freedom rocket motor thrust stand[R]. AIAA 2008-5051,2008.
[8]	BURKE R F,REZZAG T,RODRIGUEZ A,et al. Development of an automatic-calibrating small-scale thrust stand for rotating detonation rocket engines[R]. AIAA 2022-2370,2022.
[9]	李琳,翟江源,程建彬,等. 固体火箭发动机磁悬浮试验台架承载力分析[C]// 2007系统仿真技术及其应用学术会议论文集. 合肥:中国科技大学出版社,2007: 716-720. LI Lin,ZHAI Jiangyuan,CHENG Jianbin,et al. Analysis of bearing capacity of solid rocket motor magnetic suspension test bench[C]//2007 Proceedings of the Academic Conference on System Simulation Technology and Its Application. Hefei:China University of Science and Technology Press,2007: 716-720. (in Chinese LI Lin, ZHAI Jiangyuan, CHENG Jianbin, et al. Analysis of bearing capacity of solid rocket motor magnetic suspension test bench[C]//2007 Proceedings of the Academic Conference on System Simulation Technology and Its Application. Hefei: China University of Science and Technology Press, 2007: 716-720. (in Chinese)
[10]	郑健,周长省,刘锐. 固体火箭发动机六分力试验台应用综述[J]. 江苏航空,2010(增刊): 5-8. ZHENG Jian,ZHOU Changxing,LIU Rui. Application review of solid rocket engine six-component test bench[J]. Jiangsu Airlines,2010(Suppl.): 5-8. (in Chinese ZHENG Jian, ZHOU Changxing, LIU Rui. Application review of solid rocket engine six-component test bench[J]. Jiangsu Airlines, 2010(Suppl.): 5-8. (in Chinese)
[11]	庄杰,李建勋. 490 N长喷管发动机轴向推力测量系统精度分析[J]. 微型电脑应用,2010,26(1): 51-53,6. ZHUANG Jie,LI Jianxun. The precise analyse of 490 N long nozzle engineaxial thrust measuring system[J]. Microcomputer Applications,2010,26(1): 51-53,6. (in Chinese ZHUANG Jie, LI Jianxun. The precise analyse of 490 N long nozzle engineaxial thrust measuring system[J]. Microcomputer Applications, 2010, 26(1): 51-53, 6. (in Chinese)
[12]	MILOŠ P,DAVIDOVIC N,JOJIC B,et al. A novel 6 DOF thrust vector control test stand[J]. Tehnicki Vjesnik,2015,22(5): 1247-1254. DOI: 10.17559/TV-20140621064603.
[13]	SESSIONS S D. A 6-degree of freedom static-thrust stand developed for RC-scale jet engines[D]. Logan,US:Utah State University,2011.
[14]	钱鹏俊,陆正亮,廖文和. 微纳卫星固体火箭推进器推力矢量测量方法[J]. 系统工程与电子技术,2020,42(6): 1348-1357. QIAN Pengjun,LU Zhengliang,LIAO Wenhe. Thrust vector measurement method of micro-nano satellite solid rocket thruster[J]. Systems Engineering and Electronics,2020,42(6): 1348-1357. (in Chinese QIAN Pengjun, LU Zhengliang, LIAO Wenhe. Thrust vector measurement method of micro-nano satellite solid rocket thruster[J]. Systems Engineering and Electronics, 2020, 42(6): 1348-1357. (in Chinese)
[15]	金贺龙,王浩,林庆育,等. 斜切喷管固体火箭发动机喷管流场与推力特性研究[J]. 推进技术,2020,41(12): 2681-2690. JIN Helong,WANG Hao,LIN Qingyu,et al. Characteristics of nozzle flow field and thrust for a solid rocket motor with a structure of angle-cut nozzle[J]. Journal of Propulsion Technology,2020,41(12): 2681-2690. (in Chinese JIN Helong, WANG Hao, LIN Qingyu, et al. Characteristics of nozzle flow field and thrust for a solid rocket motor with a structure of angle-cut nozzle[J]. Journal of Propulsion Technology, 2020, 41(12): 2681-2690. (in Chinese)
[16]	邢勤. 姿控火箭发动机脉冲推力测试系统研究[D]. 大连: 大连理工大学,2011. XING Qin. Study of pulsed thrust measurement system of attitude-control rocket engine[D]. Dalian: Dalian University of Technology,2011. (in Chinese XING Qin. Study of pulsed thrust measurement system of attitude-control rocket engine[D]. Dalian: Dalian University of Technology, 2011. (in Chinese)
[17]	高博. 姿控火箭发动机脉冲推力测试研究[D]. 大连: 大连理工大学,2012. GAO Bo. Development of pulsating thrust measuring system of attitude-control rocket engine[D]. Dalian: Dalian University of Technology,2012. (in Chinese GAO Bo. Development of pulsating thrust measuring system of attitude-control rocket engine[D]. Dalian: Dalian University of Technology, 2012. (in Chinese)
[18]	李明昱. 立式大推力压电测试系统研究[D]. 大连: 大连理工大学,2018. LI Mingyu. Research on vertical large thrust piezoelectric test system[D]. Dalian: Dalian University of Technology,2018. (in Chinese LI Mingyu. Research on vertical large thrust piezoelectric test system[D]. Dalian: Dalian University of Technology, 2018. (in Chinese)
[19]	胡旭晓. 火箭发动机推力矢量测试系统的研制[D]. 大连: 大连理工大学,2006. HU Xuxiao. Research and development of the thrust vector measuring system for rocket motor[D]. Dalian: Dalian University of Technology,2006. (in Chinese HU Xuxiao. Research and development of the thrust vector measuring system for rocket motor[D]. Dalian: Dalian University of Technology, 2006. (in Chinese)
[20]	董洪强. 小推力液体火箭发动机试车台设计研究[D]. 长沙: 国防科学技术大学,2006. DONG Hongqiang. Research on the design of test bench for low thrust liquid rocket engine[D]. Changsha: National University of Defense Technology,2006. (in Chinese DONG Hongqiang. Research on the design of test bench for low thrust liquid rocket engine[D]. Changsha: National University of Defense Technology, 2006. (in Chinese)
[21]	吴雨,贾云飞,郝玉风,等. 大吨位火箭发动机传感器自动标定系统[J]. 固体火箭技术,2018,41(5): 664-670. WU Yu,JIA Yunfei,HAO Yufeng,et al. Automatic calibration system of sensors in large-tonnage rocket motor[J]. Journal of Solid Rocket Technology,2018,41(5): 664-670. (in Chinese WU Yu, JIA Yunfei, HAO Yufeng, et al. Automatic calibration system of sensors in large-tonnage rocket motor[J]. Journal of Solid Rocket Technology, 2018, 41(5): 664-670. (in Chinese)
[22]	段武斌. 大吨位六分力测量系统原位标定及数据处理方法研究[D]. 南京: 南京理工大学,2009. DUAN Wubin. Research on in-situ calibration and data processing method of large tonnage six-component measurement system[D]. Nanjing: Nanjing University of Science and Technology,2009. (in Chinese DUAN Wubin. Research on in-situ calibration and data processing method of large tonnage six-component measurement system[D]. Nanjing: Nanjing University of Science and Technology, 2009. (in Chinese)
[23]	王志勇. 火箭发动机推力矢量测试系统标定装置的研制[D]. 大连: 大连理工大学,2006. WANG Zhiyong. Research and development of calibration devices for rocket motor thrust vector measuring system[D]. Dalian: Dalian University of Technology,2006. (in Chinese WANG Zhiyong. Research and development of calibration devices for rocket motor thrust vector measuring system[D]. Dalian: Dalian University of Technology, 2006. (in Chinese)
[24]	宋鹏. 四支点压电测力仪的静态测试误差研究[D]. 大连: 大连理工大学,2018. SONG Peng. Research on the static test error of four-point piezoelectric dynamometer[D]. Dalian: Dalian University of Technology,2018. (in Chinese SONG Peng. Research on the static test error of four-point piezoelectric dynamometer[D]. Dalian: Dalian University of Technology, 2018. (in Chinese)