Preliminary tests of vulnerability of typical aircraft electronics to lightning-induced voltages
National Aeronautics and Space Administration, 1974 - Technology & Engineering - 44 pages
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28 volts AIDS Amplifier aircraft electronics equipment Aircraft Passenger Address alumel amplifier circuits Amplifier Showing AMPLIFIRR analog and digital analog pointer Announcement Reproducer Input audio Block Diagram Boeing Company Chromel circuitry Comparator Amplifier Gate connected Connector Jl digital indicators diodes electrical error signal Figure l4 function Gas Temperature Indicator Gate and AIDS impedance Indication Pointer Reset Indicator Functional Induced Voltages Applied injected voltage waveform instrument operation interference or damage Lightning-Induced Voltages Applied malfunction Maximum Indication Pointer microsecond noted none noted partial breakdown Partial Wiring Diagram Passenger Address Amplifier photo switch Pin Numbers Pins l4 Pointer Reset Coil printed circuit boards servomechanism shown on Figure Simulated Induced Voltages Simulated Lightning-Induced Voltages solid state electronics susceptibility Tektronix Test Circuit test voltage TGT indicator TGT instrument thermocouple input circuit torque amplifier transient analyzer transient voltage Transistor turbine gas temperature us/div v/div Voltage Injection Tests voltage transients volts peak vulnerability levels waveshape Wedge Lights