摘要
针对固体火箭发动机研制和生产中的性能检测需求,基于柔性试验架建立试验平台,采用虚拟仪器技术搭建测控平台,使用LabView7.1开发一套包含参数标定、数据测量、数据处理等模块的固体火箭发动机性能检测试验测控软件,构建了固体火箭发动机性能检测系统。通过对标准发动机进行测试,结果表明:该系统实现了发动机参数的现场方便标定、发动机数据的高速采集和实验数据的快速处理,测量精度达到0.3%的工程要求,并同步监测了整个发动机的工作过程,满足了发动机性能检测的高精度要求。
According to the performance detecting requirements in development and manufacture of solid rocket motor, a test platform has been set up based on flexible test stand, in which the measurement and control platform has been built using virtual instrument technology ; a set of solid rocket motor ground test performance detecting software including parameter calibration model, data measure model and data processing model have been developed based on the LabViewT. 1 ; and the solid rocket motor performance detecting system was built. The application results through testing normative solid rocket motor show that: this system could actualize parameter calibration expediently, experimental data collection and processing rapidly, even reach the measurement precision by 0.3% required in projects and could monitor the testing process of solid rocket motor simultaneously, which satisfied high-precision requirements of motor performance detection.
出处
《机械科学与技术》
CSCD
北大核心
2011年第10期1597-1601,共5页
Mechanical Science and Technology for Aerospace Engineering
基金
武器装备预研基金项目
关键词
固体火箭发动机
试验平台
虚拟仪器
测控平台
性能检测系统
solid rocket motor
test platform
virtual instrument
measurement and control platform
performancedetecting system