Catalog excerpts
Lightning Tests: Avionics Test System 1 Avionics Test System Lightning Tests Brief Overview of Phenomena. . . . . . . . . . . . . . . . 2 Applicable Standards . . . . . . . . . . . . . . . . . . . 3 Test System Overview. . . . . . . . . . . . . . . . . . . 4 Generator Specifi cations. . . . . . . . . . . . . . . . . 10 Accessories and Options. . . . . . . . . . . . . . . . . 12 Software . . . . . . . . . . . . . . . . . . . . . . . 18 EMC PARTNER’s Product Range . . . . . . . . . . . . . . 19
Open the catalog to page 12 Lightning Tests: Avionics Test System Studies by the Federal Aviation Administration (FAA) reveal that the average civil aircraft is struck by lightning every 1000 fl ight hours. It is therefore imperative that all aircraft should be tested to withstand the effects of lightning. Lightning events differ mainly in current amplitude, in the transferred charge and in the impulse shape of the lightning current. Two lightning events need to be simulated: - the direct strike (current and voltage) and - the induced currents and voltages within an aircraft resulting from a direct strike. Induced...
Open the catalog to page 2Lightning Tests: Avionics Test System 3 Applicable Standards Radio Technical Commission for Aeronautics (RTCA) DO-160 : Environmental Conditions and Test Procedure for Airborne Equipment. - Section 17: Voltage Spike. - Section 19: Induced Signal Susceptibility. - Section 22: Lightning Induced Transient Susceptibility. - Section 25: Electrostatic Discharge (ESD). European Organisation for Civil Aviation Equipment (EUROCAE) EUROCAE / ED-84 (1997): Aircraft Lightning Environment and related Test Waveforms. Report of EUROCAE WG-31 and SAE Committee AE4L. - Induced Signal Susceptibility These...
Open the catalog to page 34 Lightning Tests: Avionics Test System Test System Features - Full level 5 capability for all waveforms - Clean reproducible waveforms - Modular construction allows for future expansion - Simple operation - Parameter change during operation (+/-) - Internal program memory - Electronic polarity change - Compact designs - Fulfi lls ALL transient requirements - Remote control and software upgrade through standard interface - Full range of accessories - 2 year warranty User Benefi ts The technical excellence and many unique features of EMC PARTNER avionics generators translate directly into...
Open the catalog to page 4Lightning Tests: Avionics Test System 5 Remote control of EMC PARTNER avionics test systems is possible using the EMC PARTNER TEMA software package. This is greatly enhanced by the free to download DATABASE software which provides additional hints and contains predefi ned generator setup fi les. EMC PARTNER has test equipment to simulate four component tests on complete aircraft. For further information please contact EMC PARTNER directly. ESD3000 MIG2000-6 MIG-OS-MB-EXT MIG-OS-MB - MIG-OS-MB Waveforms WF2 & WF3 (1MHz & 10MHz). Used for WF2 multiple stroke and WF3 multiple burst tests on...
Open the catalog to page 56 Lightning Tests: Avionics Test System Single Stroke MIG0600SS DATABASE on EMCP Website easy use, no test programming, just carry out tests EUT TEMA TEST MANAGER customized solution DSO Option control TEK DSO NW-MS-LEVEL 1 MIG0618SS CN-GI-CI I-PROBE-MS DN-LISN160-32 Single Stroke (SS) Immunity EUT Power Multiple Stroke Z:\VK\Verkaufsinstrumente\Brochures\Lightning\Aircraft\MIG0600-MS.flo NW April29. 2008 MIG0600MS DATABASE on EMCP Website easy use, no test programming, just carry out tests EUT TEMA TEST MANAGER customized solution DSO Option control TEK DSO NW-MS-LEVEL 1 CN-GI-CI-V...
Open the catalog to page 6Lightning Tests: Avionics Test System 7 PIN Injection MIG0600SS Immunity DATABASE on EMCP Website easy use, no test programming, just carry out tests EUT TEMA TEST MANAGER customized solution DSO Option control TEK DSO NW-MS-LEVEL 1 Pin Injection (PIN) DN-LISN160-32 EUT Power System Flowcharts for WF2 and WF3 The following fl owcharts illustrate EMC PARTNER equipment confi gurations necessary to perform multiple burst, multiple stroke and PIN injection tests in accordance with DO160 section 22. - PIN Injection Waveform 3 is applied directly from the generator output using the CN-MIG-TT to...
Open the catalog to page 78 Lightning Tests: Avionics Test System Multiple Burst CN-MIG-BT1/ BT3 MIG-OS-MB Immunity DATABASE on EMCP Website easy use, no test programming, just carry out tests EUT TEMA TEST MANAGER customized solution DSO Option control TEK DSO I-PROBE-MB-P1 DN-LISN160-32 Multiple Burst (MB) EUT Power CN-MIG-BT Single Stroke and Multiple Stroke Z:\VK\Verkaufsinstrumente\Brochures\Lightning\Aircraft\MIG-OS-MB-MS-MB.flo MIG-OS-MB-EXT MIG-OS-MB NW April 29. 2008 Immunity DATABASE on EMCP Website easy use, no test programming, just carry out tests EUT DSO Option control TEK DSO DN-LISN160-32 Single...
Open the catalog to page 8Lightning Tests: Avionics Test System 9 Flowchart for Voltage Spike and Induced Susceptibility Tests The following EMC PARTNER equipment is used to perform tests in accordance with DO160 section 17 and 19. Z:\VK\Verkaufsinstrumente\Brochures\Lightning\Aircraft\MIG2000-6-avionics.flo NW April29. 2008 MIG2000-6 EUT TEMA TEST MANAGER customized solution Calibration Feature (VERI50 & VERI5) Plug-in DO160 Section 19 MIG2000-6 Plug-in Airbus AMD-24C Plug-in DO160 Section 17 Coupling: CN-MIG-BT & direct Coupling CN-MIG-BT4 GENECS-MIG ESD Test Equipment for DO160 section 25...
Open the catalog to page 910 Lightning Tests: Avionics Test System MIG0618SS (Level 4 and 5 Extension) DO160 Waveforms W1, W4 & W5A W1 - 6.4/70ìs 250A up to 4000A W4 - 6.4/70ìs PIN injection 125 up to 3200V W4 - 6.4/70ìs Ground injection 125 up to 3200V ( 6400A at 3200V) 1) W5A - 40/120ìs PIN injection 125 up to 3200V (3200A at 3200V) 1) W5A - 40/120ìs Ground injection 400A up to 6000A (10000A) 1) Generator Specifi cations MIG0600SS and MIG0600MS DO160 Waveforms W1, W4, W5A & W5B W1 - 6.4/70ìs 15A up to 1600A (3200A) 1) W4 - 6.4/70ìs 75V up to 1600V W5A - 40/120ìs 75A up to 2000A (10000A) 1) W5B - 50/500ìs 75A up to...
Open the catalog to page 10Lightning Tests: Avionics Test System 11 MIG2000-6 Fx-DO160-S17 DO160 Section 17 waveform Voltage Spikes Amplitude range 100 to 1100V Source Impedance 50ohm Risetime 1 to 2ìs Duration 10ìs ± 20% Repetition up to 2Hz Synchronisation 50/60/400Hz Coupling Serial injection using CN-MIG-BT Fx-DO160-S19 DO160 Section 19 waveform Induced Signal Susceptibility Amplitude range 100 to 1000V Spike duration 4ìs Burst duration 250ìs Coupling Serial using wire coil Fx-AMD24C ABD0100.1.8 waveform Voltage Spikes Test Supply Voltage 115V Risetime < 2ìs Source Impedance 50ohm Spike Duration 10ìs Amplitude...
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