首页> 外国专利> METHOD FOR DETERMINING COEFFICIENT OF CONVERTING CURRENT FLOWING VIA ELEMENTS OF EXTERNAL SPACE VEHICLE SURFACE TO VOLTAGE OF ELECTROMAGNETIC PICKUP IN FRAGMENTS OF AIRBORNE CABLE NETWORK AND DEVICE FOR ITS IMPLEMENTATION

METHOD FOR DETERMINING COEFFICIENT OF CONVERTING CURRENT FLOWING VIA ELEMENTS OF EXTERNAL SPACE VEHICLE SURFACE TO VOLTAGE OF ELECTROMAGNETIC PICKUP IN FRAGMENTS OF AIRBORNE CABLE NETWORK AND DEVICE FOR ITS IMPLEMENTATION

机译:通过航空电缆网段中外部空间车辆表面对电磁拾取电压的转换系数确定电流流动的方法及其实现方法

摘要

FIELD: measurement equipment.;SUBSTANCE: invention is intended for measuring the coefficient converting the current flowing via elements of external space vehicle surface to voltage of pickup in fragments of airborne cable network, which are routed along those elements. In method of determining coefficient converting the current flowing via elements of external space vehicle surface to voltage of electromagnetic pickup in fragments of airborne cable network (ACN), the tested cable is arranged on the device imitating the element of external space vehicle surface, tested fragment of airborne cable network loaded on both sides to the resistances imitating actual operating load, pulse current is generated and its pulse parametres correspond to actual parametres of electrostatic charges on space vehicle surface, pulse current with peak value I is passed via the device imitating the element of external space vehicle surface, voltage of electromagnetic pickup U is measured in tested fragment of airborne cable network, and there determined is value of coefficient converting current Kconv flowing via the device imitating the element of external space vehicle surface, L long, to voltage of electromagnetic pickup in tested fragment of airborne cable network from the ratio. There also proposed is device for method implementation.;EFFECT: improving fidelity and accuracy of determining electromagnetic pickups in fragments of airborne cable network, which are routed along external space vehicle surface.;3 cl, 1 dwg
机译:技术领域:本发明旨在测量将流经外部空间飞行器表面的元件的电流转换为沿着这些元件布线的机载电缆网络的片段中的拾取电压的系数。在确定将通过外部空间飞行器表面元件流动的电流转换为机载电缆网络(ACN)片段中的电磁感应电压的系数的方法中,将被测电缆布置在模仿外部空间飞行器表面元件,被测片段的装置上负载在两侧的空中电缆网络模拟实际运行负载的电阻,产生脉冲电流,其脉冲参数与航天器表面静电电荷的实际参数相对应,峰值电流I的脉冲电流通过模拟元件的装置传递在太空飞行器表面的表面上,测量机载电缆网络中被测片段的电磁拾波器U的电压,并确定流过模拟太空飞行器元件的装置中流过的系数转换电流K conv 的值表面,长L,相对于机载电缆测试段中的电磁感应电压n从比例开始。还提出了一种用于该方法实施的装置;效果:提高了确定沿外太空飞行器表面布线的机载电缆网络片段中的电磁拾波器的保真度和准确性。3 cl,1 dwg

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号