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DL_Mech wrote:Each seat should have its own power supply, so you would only take out your own seat row. I believe this is done to minimize wire size/ amount of wires with 120v.
kalvado wrote:DL_Mech wrote:Each seat should have its own power supply, so you would only take out your own seat row. I believe this is done to minimize wire size/ amount of wires with 120v.
What is the power system voltage generally? 28 V or something else?
I remember it used to be 400 Hz to reduce transformer size and weight, probably not a big deal anymore with all DC-DC converters today
DL_Mech wrote:kalvado wrote:DL_Mech wrote:Each seat should have its own power supply, so you would only take out your own seat row. I believe this is done to minimize wire size/ amount of wires with 120v.
What is the power system voltage generally? 28 V or something else?
I remember it used to be 400 Hz to reduce transformer size and weight, probably not a big deal anymore with all DC-DC converters today
Traditional airplanes have 28v dc and 115v ac 400 hz (for smaller wire size). However, newer planes such as the A220 have mostly dc wiring running throughout with dc-ac conversion taking place inside the black boxes. I don’t know the reason for this new convention. Ideas?