南疆天然气利民工程采用太阳能电源系统为阀室设备供电,太阳能电源系统电压等级为+24 V DC,经逆变器输出220 V AC为交流负载供电。投产初期设备带载时大部分阀室出现逆变器电路板烧毁现象,经对现场设备进行分析和测试,最终确认是220 V A...南疆天然气利民工程采用太阳能电源系统为阀室设备供电,太阳能电源系统电压等级为+24 V DC,经逆变器输出220 V AC为交流负载供电。投产初期设备带载时大部分阀室出现逆变器电路板烧毁现象,经对现场设备进行分析和测试,最终确认是220 V AC电压等级的音响功放系统在启动时瞬间冲击电流过大,导致逆变器损坏。为解决瞬间冲击电流过大导致设备损坏,最大程度节省改造费用,最小化影响阀室运行,经多方探讨和论证,决定在逆变器至功放电源的回路间增加一台功放软启动设备,以便减小音响功放启动瞬间对逆变器的电流冲击。本次提供的功放软启动设备经过在线使用三个月,运行情况良好。展开更多
In order to measure the instantaneous thrust of a certain attitude-control solid rocket motor, based on the analysis of the measurement principles, the difference between the instantaneous thrust and steady thrust mea...In order to measure the instantaneous thrust of a certain attitude-control solid rocket motor, based on the analysis of the measurement principles, the difference between the instantaneous thrust and steady thrust measurements is pointed out. According to the measurement characteristics, a dynamic digital filter compensation method is presented. Combined the identification-modeling, dynamic compensation and simulation, the system's dynamic mathematic model is established. And then, a compensation digital filter is also designed. Thus, the dynamic response of the system is improved and the instantaneous thrust measurement can be implemented. The measurement results for the rocket motor show that the digital filter compensation is effective in the instantaneous thrust measurement.展开更多
文摘南疆天然气利民工程采用太阳能电源系统为阀室设备供电,太阳能电源系统电压等级为+24 V DC,经逆变器输出220 V AC为交流负载供电。投产初期设备带载时大部分阀室出现逆变器电路板烧毁现象,经对现场设备进行分析和测试,最终确认是220 V AC电压等级的音响功放系统在启动时瞬间冲击电流过大,导致逆变器损坏。为解决瞬间冲击电流过大导致设备损坏,最大程度节省改造费用,最小化影响阀室运行,经多方探讨和论证,决定在逆变器至功放电源的回路间增加一台功放软启动设备,以便减小音响功放启动瞬间对逆变器的电流冲击。本次提供的功放软启动设备经过在线使用三个月,运行情况良好。
文摘In order to measure the instantaneous thrust of a certain attitude-control solid rocket motor, based on the analysis of the measurement principles, the difference between the instantaneous thrust and steady thrust measurements is pointed out. According to the measurement characteristics, a dynamic digital filter compensation method is presented. Combined the identification-modeling, dynamic compensation and simulation, the system's dynamic mathematic model is established. And then, a compensation digital filter is also designed. Thus, the dynamic response of the system is improved and the instantaneous thrust measurement can be implemented. The measurement results for the rocket motor show that the digital filter compensation is effective in the instantaneous thrust measurement.