How is alternating current distributed on an aircraft?

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need more than one line answer

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AC power distribution on large aircraft is very complex. Below is a link to a simple block diagram.

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Generators are driven by the engines, and generator control units monitor these for correct power output and to synchronize the phases of multiple generators for more power. Large relays connect this power to the aircraft busses where it is distributed throughout the aircraft as needed. Generators create 115VAC 400Hz three-phase power, which can be converted to 26VAC via transformers or into 28VDC thru Transformer-Rectifier Units. These power types have their own regulators and relays to connect them to thier power busses.

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If I remember A/C electrical systems, its not AC, its DC.

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By
electrical
wires

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that is three lines this one makes 4

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An aircraft uses 26v and 115v 400Hz. The use of AC is the most efficient means (smaller cables = less weight) of getting electrical energy from source to load. The use of three phase or single phase is dictated by the size of the aircraft and the systems being supplied. You will find that in most cases only single phase supplies are used (these may well be from a three phase supply).

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Just like in your home. With copper wiring. Large A/C need AC for the kitchens and other uses too.

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voltage regulator.

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wires
bus
circuit breakers
generators
conductors...etc...
AIRCRAFT USE BOTH A/C and D/C!

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while the aircraft is running, through either the engine or APU generators, on the ground, electrical power. 120 volts, at 400 hertz

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It is provided using ground support equipment at 200v line voltage. this is 3 phase voltage meaning it is about 115 volts per phase. the frequency is 400 hz + or - 2 % tolerance. this means the aircraft may allow 392min -408 hz max depending on aircraft sensitivity. A socket connected will have 6 pins. :3 phases, 1 neutral, 2 interlock. the interlock prevents power at socket without it being connected. this is 28v dc provided by aircraft on civilian jets and provided by generator on military jets.

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A/C current is distributed from the Engine/APU generators to the main circuit panels called Buses. Then to individual circuits thru circuit breakers, relays, switches via wires usually made of copper. A/C current is almost always 115 Volts and 400 Hz (cycles).
While on the ground it usually will have a large cord plugged into the the nose area supplying power when the engines/APU are shut down. This power also goes to the Buses.

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There are several real good answers about power distribution here from the gens to line contactors (big relays) to transformer recifiers on to AC/DC busses then on to various subsystems.

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Stricly speaking about AC it will come straight off the generator usually in three phases A,B, and C from there it is routed using fairly heavy gauge wire through some times through current monitors for which detect differences in current between the phases then on to a generator controlo unit GCU which will check for various faults in the supply such as under/over voltage or overfrequency and so on. If a fault is detected the GCU can take the gen off-line to prevent damage to the whole system.
From the GCu it woulod go to a line contactor which is like a big relay then on to 115 busses for running three phase motors such as fuel pumps and other 115 VAC devices. It would also go to a transformer rectifier to be converted to DC then on to DC busses and components.

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Through cabling. A single cable for single phase and 3 cores for 3 phase. Generator cabling also has an exciter cable. The circuit is completed by bonding it down to the airframe (earth return) to avoid the need to run return cables back to the power source. Incidentally, auto-electrics utilise the same system of earth return(most modern cars are negative earth).
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