baobab72
10th Aug 2013, 07:37
Hi folks
I downloaded the r22 poh from the robinson website and while browsing through the system section i came across the electrical system diaghram which to say the least it looks pretty complicated!
A few questions that stem right off the bat and that hopefully the furus outthere will be able to answer:
1 Power from the battery is made available to the battery relay which has three posts - one input, one from the battery switch and one going to the starter relay - the input is self explainatory, the output to the starter as well since one of the functions of the battery is to power the starter to crank the engine up and then bring the alternator on line, while the output going to the BATT MASTER switch, does that control the ground to the relay, completing the circuit when flipping the switch to ON, what does it do exactly?
2 power from the start relay goes to the STARTER ON light, to the starter motor and then to the alternator control unit which i guess is the voltage regulator controlling the trickle charge to the electromagnetic field of the rotor of the alternator going to the F2 input on the alternator itself. The A+ output i guess is the output from the alternator to the bus. What about the ALT switch, what does it control? Because as far as i can see there is a wire going from the alternator control unti to the bus through the switch, is it the same as the A+? It looks like they are two distinguished wires! Another post is going from the starter relay to the master radio relay and from there to a number of avionics and instrumentation.
3 from the battery there is another wire going to what looks like the clutch actuator and the clock and from there to the dual tach which is also supplied from the radio master relay, is that correct?
4 are the overvoltage relay and the rectifier - i guess consisting of a number of solid state diodes - in the alternator control unit? Cos it is not shown on the schematic?
5 what are other funtions of the alternator control unit - Vr, apart from controlling the trickle charge to the rotor? Does it provide some kind of over-undervoltage or overload protection?
6 is the system single wire negative grounded, using the fuselage as a ground return to complete the circuit?
Many thanks and sorry if i have abused of your patience and willingness but i do believe that the elctrical system puzzles a lot of people outthere and i like to have a solid knowledge of the systems and not merely flipping switches while ignoring what they really do!
Baobab72
I downloaded the r22 poh from the robinson website and while browsing through the system section i came across the electrical system diaghram which to say the least it looks pretty complicated!
A few questions that stem right off the bat and that hopefully the furus outthere will be able to answer:
1 Power from the battery is made available to the battery relay which has three posts - one input, one from the battery switch and one going to the starter relay - the input is self explainatory, the output to the starter as well since one of the functions of the battery is to power the starter to crank the engine up and then bring the alternator on line, while the output going to the BATT MASTER switch, does that control the ground to the relay, completing the circuit when flipping the switch to ON, what does it do exactly?
2 power from the start relay goes to the STARTER ON light, to the starter motor and then to the alternator control unit which i guess is the voltage regulator controlling the trickle charge to the electromagnetic field of the rotor of the alternator going to the F2 input on the alternator itself. The A+ output i guess is the output from the alternator to the bus. What about the ALT switch, what does it control? Because as far as i can see there is a wire going from the alternator control unti to the bus through the switch, is it the same as the A+? It looks like they are two distinguished wires! Another post is going from the starter relay to the master radio relay and from there to a number of avionics and instrumentation.
3 from the battery there is another wire going to what looks like the clutch actuator and the clock and from there to the dual tach which is also supplied from the radio master relay, is that correct?
4 are the overvoltage relay and the rectifier - i guess consisting of a number of solid state diodes - in the alternator control unit? Cos it is not shown on the schematic?
5 what are other funtions of the alternator control unit - Vr, apart from controlling the trickle charge to the rotor? Does it provide some kind of over-undervoltage or overload protection?
6 is the system single wire negative grounded, using the fuselage as a ground return to complete the circuit?
Many thanks and sorry if i have abused of your patience and willingness but i do believe that the elctrical system puzzles a lot of people outthere and i like to have a solid knowledge of the systems and not merely flipping switches while ignoring what they really do!
Baobab72