火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2012年
1期
68-71,75
,共5页
脉宽调制%推挽方式%高压发生电路%绝缘电阻测试
脈寬調製%推輓方式%高壓髮生電路%絕緣電阻測試
맥관조제%추만방식%고압발생전로%절연전조측시
PWM%push-pull mode%high-voltage generating circuit%insulation resistance test
以TL494为控制核心的脉宽调制推挽式高压发生电路采用脉冲宽度调制和电压反馈推挽技术,可通过调整振荡器频率和采样电阻值,输出多种状态恒定直流高压。本电路结构简单可靠,稳定性高。试验验证表明,满足液体火箭发动机控制电路系统绝缘电阻测试要求。
以TL494為控製覈心的脈寬調製推輓式高壓髮生電路採用脈遲寬度調製和電壓反饋推輓技術,可通過調整振盪器頻率和採樣電阻值,輸齣多種狀態恆定直流高壓。本電路結構簡單可靠,穩定性高。試驗驗證錶明,滿足液體火箭髮動機控製電路繫統絕緣電阻測試要求。
이TL494위공제핵심적맥관조제추만식고압발생전로채용맥충관도조제화전압반궤추만기술,가통과조정진탕기빈솔화채양전조치,수출다충상태항정직류고압。본전로결구간단가고,은정성고。시험험증표명,만족액체화전발동궤공제전로계통절연전조측시요구。
A push-pull high-voltage generating circuit is introduced, which takes TL494 as a con- trol core, and adopts pulse-width modulation (PWM) and voltage feedback push-pull technologies. It can output a variety of constant DC high-voltage current by adjusting the oscillator frequency and the sampling resistance. The circuit is simple and reliable, and has high stability. The test validation result shows that the circuit can meet the test requirements of insulation resistance in control circuitry of liquid rocket engines