Application

The lightning stoke system for direct current test on aircraft comprises of three sets of impulse generators and one set DC power source, which can generate A, B, C, D four current components to meet the direct effect requirement on aircraft.

The test system has four control systems which can not only be operated separately but also can be synchronously controlled by one human interface if necessary.

The test system is also applicable for other research test such as OPGW in power system

Standard

IEC60060-1, IEC60060-2, IEC61312, Mil-Std-464C

System Configuration

• Switchgear Cubic for AC power system 400V, 50/60 Hz
• GIC200C Impulse Current Generator with Crowbar Unit (component A)
• GRIC20-5 Square Waveform Current Generator (component B)
• GZL-800L DC Power Source with Battery (Component C)
• GIC100C Impulse Current Generator with Crowbar Unit  (Component D)
• Accessories for the system, cables, tools, fuses, inductors, resistors…
• Calibration certificate of measuring system from XIHARI 

  Technical Specification

  Direct Lightning Current	Model No	Shapes	Peak Current	Remark
  Component A	GIC200C	10/350μs	200kA	Crowbar circuit
  		8/20μs	250 kA
  Component B	GRIC20-5	Td=2ms	5kA	Long duration
  Component C	GZL-800L	Direct current	800A
  Component D	GIC100C	10/350μs	100kA	Crowbar circuit
  		8/20μs	200kA