OK, here's my effort:
The AVR (9) is powered from a DC source which is supplied by the stationary rectifier. (8)
DC from the AVR output is applied to F1 & F2 at the exciter field (stator) winding. (4)
3-phase AC is generated on the exciter rotor (3) and is rectified by a shaft-mounted rectifier (5) to feed DC to the main field. (2)
The rotation of the main field within the alternator stator (1) develops 3-phase AC on the main terminals of the alternator.
The interesting component here is the stationary rectifier (8) which is dual-fed from both a set of power CT's (7) on each phase of the alternator stator and from the alternator main terminals via a choke (6). The purpose of the choke is to decouple the inputs to the stationary rectifier from the alternator terminals, so the CT's aren't directly connected to the output of the alternator. The input to the stationary rectifier is therefore a factor of both the alternator terminal voltage and the alternator phase currents.
Under normal conditions stationary rectifier (8) is principally fed from the alternator terminals via choke (6), and the contribution from the power CT's (7) is negligible. Under fault conditions the alternator terminal voltage will collapse and the phase current will increase, with the result that the power CT's will feed into the rectifier making up for the shortfall due to the reduced terminal voltage during the fault, and ensuring that a source of power is available to the AVR during the fault.
The AVR (9) itself looks fairly standard, with single-phase voltage sensing between lines U-V and a quadrature droop CT (11) to aid reactive load sharing.
RF suppressor (10) shunts any high-frequency noise on the generator terminals to earth.
Hope this helps, if anyone spots any errors please feel free to correct me.
