|Table of Contents|

Isolated solenoid valve current measurement circuit in rocket engine test(PDF)

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

Issue:
2020年05期
Page:
102-108
Research Field:
测控与试验
Publishing date:

Info

Title:
Isolated solenoid valve current measurement circuit in rocket engine test
Author(s):
LING SiruiDING Boshen
(Beijing Institute of Aerospace Testing Technology, Beijing 100074,China)
Keywords:
current measurement solenoid valves isolation inverse voltage suppression temperature drift
PACS:
V433,TM933.1
DOI:
-
Abstract:
In the ground test of rocket engine, a large number of solenoid valves in the engine and test process system were needed to be controlled and record state.The solenoid current measurement system was required to have high static accuracy and dynamic performance.Aiming at the problems in traditional application, an integrated current measurement circuit was realized.The DC-DC modules and TPS717 were used for isolated power supply.Voltage on the 10 mΩ shunt resistor was amplified by an INA240 and was isolated by an AMC1311.An INA826 was used for gain adjustment and output.In error analysis, test and calibration prove that the total uncorrectable error of the circuit is 0.144 9%.The calibrated accuracy is better than 0.025%.The -3 dB bandwidth of full output range is 110 kHz.This circuit can be widely used in the driving of various applications of current measurement such as in rocket engine tests.

References:

[1] 张卫东, 李力, 张茂森, 等.基于虚拟仪器和PXI总线的电磁阀控制系统研制[J].火箭推进, 2015, 41(1): 112-116.
ZHANG W D, LI L, ZHANG M S, et al.Development of solenoid valve control system based on virtual instrument and PXI bus[J].Journal of Rocket Propulsion, 2015, 41(1): 112-116.
[2] 郝贵欣, 周吉, 张华.一种电磁阀智能测试系统[J].火箭推进, 2013, 39(5): 92-97.
HAO G X, ZHOU J, ZHANG H.Intelligent testing system for solenoid valve[J].Journal of Rocket Propulsion, 2013, 39(5): 92-97.
[3] 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(2): 114-117.
LIU W L, NIU X N, LI Q L, et al.Design of a ground test control system for attitude and orbital control engine[J].Journal of Rocket Propulsion, 2015, 41(2): 114-117.
[4] 孙新新, 常莹.电磁阀电流曲线测试电路的设计[J].计量技术, 2019(4): 3-5.
[5] 王明迪, 李建勋.霍尔电流传感器在阀门电流测试中的应用[J].微型电脑应用, 2009, 25(11): 17-19.
[6] 赵闻达, 苏永清.电磁阀驱动电源电流检测系统的精度分析[J].测控技术, 2017, 36(2): 153-156.
[7] Analog Devices.LT3042 20V、200mA、超低噪声、超高 PSRR RF 线性稳压器数据手册 [EB/OL].[2020-02-22].https://www.analog.com/media/cn/technical-documentation/data-sheets/3042f_chs.pdf.
[8] Texas Instruments.INA240具有增强型PWM抑制功能的高侧和低侧双向零漂移电流检测放大器数据表(Rev.B)[EB/OL].[2020-02-22].http://www.ti.com/cn/lit/ds/symlink/ina240.pdf.
[9] 沈福东.浅谈直流感性负载消除反电动势电路设计[J].科技创新导报, 2012, 9(15): 55.
[10] 余力凡, 马红梅.运载火箭控制系统电磁继电器消反峰电路分析与MULTISIM仿真[J].计算机测量与控制, 2017, 25(11): 55-57.
[11] 弭艳, 张红霞, 马兵兵, 等.基于双向TVS的电磁阀加速释放电路研究[J].计算机测量与控制, 2019, 27(8): 182-187.
[12] 林时放, 王建新, 陈洲, 等.一种基于AD215模块的低压电器通断试验电压测量装置[J].科技创新与应用, 2016(30): 50.
[13] 张亚维, 史强强, 姚锋刚.机载高速多通道隔离放大器设计[J].国外电子测量技术, 2018, 37(4): 107-112.
[14] 孙建军, 于克泳.隔离型Σ-Δ调制器技术在电机控制电流采样中的应用[J].电子产品世界, 2018, 25(12): 56-58.
[15] 郑荟民.一种非标测试行业的隔离精密电压采集模块[J].通信电源技术, 2019, 36(11): 82-83.
[16] 王博, 仲维彬.基于HCNR201线性光耦的飞机高压信号隔离电路设计[J].中国科技信息, 2019(24): 28-29.
[17] 叶克江.线性光电耦合器的进一步线性化[J].压电与声光, 2019, 41(5): 760-764.
[18] 张红勇, 方军.ISO124P器件为核心的隔离电路设计浅析[J].机电工程技术, 2013, 42(9): 103-106.
[19] Texas Instruments.AMC1311x高阻抗2V输入增强型隔离放大器数据表(Rev.A)[EB/OL].[2020-02-22].http://www.ti.com/cn/lit/ds/symlink/amc1311.pdf.
[20] Texas Instruments.INA826具有轨到轨输出的高精度、200μA电源电流、3V至 36V电源仪表放大器数据表(Rev.F)[EB/OL].[2020-02-22].http://www.ti.com/cn/lit/ds/symlink/ina826.pdf.

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Last Update: 2020-10-20