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.
Failure modes and effects analysis
High voltage systems
Also known as: SAE AIR 7502
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