Our Services

OUR SERVICES

Picture Name
Picture Name

Electromagnetic Environment Effects Test

    Electromagnetic environment refers to the sum of all electromagnetic phenomena existing in a given space, including natural electromagnetic environment and man-made electromagnetic environment, such as lightning, static electricity, etc. With more and more modern electronic equipment, the electromagnetic sensitivity is getting higher and higher, the electromagnetic environment is becoming more and more complicated, and the electromagnetic environment effect test is becoming more and more important. Safety Electromagnetic has established an electromagnetic environment effect laboratory, equipped with a lightning test system and a high-voltage electrostatic test system, which can meet the testing needs of various products such as aircraft, aircraft systems and components, ground systems, ordnance, and military systems.

 

Object Name Item/Parameter Testing Standard
Military aircraft and helicopter systems High voltage adhesion test
High current physical damage test
Transient induction test of external components
Whole machine indirect effect test
Fuel system current test
Fuel system voltage test

GJB 8848,GJB 1389A
GJB 3567

 

 Lightning induced transient sensitivity test of airborne equipment

GJB 8848,GJB1389A
 RTCA/DO-160G,RTCA/DO-160F
RTCA/DO-160E
Ground system and ordnance Indirect effect test caused by direct lightning strike
Pulse electromagnetic field effect test
Lightning conduction coupling injection test
Lightning direct effect test
Electrostatic discharge test

GJB 8848,GJB 1389A
Aircraft and parts Full-size component attachment point test
Direct effect test
Direct effect test of fuel vapor ignition
Direct effect test of corona and streamer
Indirect effect test of external electrical and electronic equipment

GJB 3567

 

 Initial pilot adhesion test
Sweep channel attachment test
High current physical damage test
Induction transient test of externally installed equipment
Conduction test of fuel tank and components

RTCA/DO-160E/F/G
SAE ARP5416/5416A
HB6167.25

 

 High-voltage lightning adhesion test of the model
Direct lightning strike test of fuel tank and components
Small gap voltage breakdown test of fuel system
Fuel system high pressure streamer test

SAE ARP5416/5416A

 

 Fuel system ignition source detection test

HB6167.25
SAE ARP5416/5416A
Onboard equipment Pin injection test
Cable bundle test

RTCA/DO-160E/F/G
HB6167.24
Wind blades and cables Initial pilot connection test
Sweep channel lightning test
Arc introduction test
Non-conductive surface test
Conduction current test

 IEC 61400-24

Previous Page

Calibration

Production Compliance Test

Next Page