The scope of this report will document the various voltage levels and provide a rational for each level as discussed and agreed to in the AE-7 committee. Future aircraft programs will become more electric, with possibly hybrid or electrical propulsion, resulting in higher electrical loads. This will require other voltage ranges. New candidate supply voltages could be 0 to 270 VDC, ±135 VDC, ±270 VDC, 0 to 540 VDC, or even higher. This report shall set forth the voltage level definitions as discussed and agreed to in the AE-7 committee.


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    Title :

    Aircraft Electrical Voltage Level Definitions


    Publication date :

    2021-01-27



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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