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Old 30th Aug 2019, 10:55
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barrichello72
 
Join Date: Sep 2005
Location: italy
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Cessna 172 electrical system

Hi guys
just a couple of questions about the electrical system of the C172.
i dont know how to post the schematic but i am confident that those of you able to provide me with an accurate answer are familiar with the layout.
as far as i understand when you flip the BAT side of the MASTER switch on, you ground the battery contactor, energizing the coil, driving the plunger down, completing the circuit and allowing battery power to be fed from the battery to the primary bus via the starter contactor and the ammeter. As the key is turned to the START position the the coil of the starter contactor is grounded, driving the plunger down, completing the circuit and allowing battery power to be fed to the starter motor, cranking the engine up.
as the ALT side of the MASTER switch is set to ON, the magic starts: the alternator is brought on line and power from the B terminal of the alternator is fed to the primary bus with a portion of it being fed via the alternator field cb and the alternator switch to the INPUT side of the ACU Alternator Control Unit, which in turn modulates the field charge fed to the F Field terminal of the alternator based on the positive sense input from the B terminal and on the negative sense input from the G terminal to vary the strength of the field current and thus the magnitude of the electromagnet so as to regulate the voltage output as the engine RPM’s and or the load vary.
Is the latter a correct statemennt?
now were does the current for the initial excitation of the field come from? I assume from the battery but the schematic does not show any wire going from the battery to the ACU and i am having a hard time figuring out the path.
as the alternator voltage exceeds the battery outpt, the current is fed from the bus via the starter and the battery contactors, to the battery keeping it charged.
Also, as far as i understand if the output of the generator exceeds a preset limit due to a failure of the ACU, the alternator field cb will trip, cutting off the field current to the alternator, causing the electromagnetic field to collapse and thus the alternator output to drop to zero - the cb can be reset switching the ALT side off and back on, flshing the field back, while should the draw from the bus exceed a preset limit, possibly due to an excessive draw from the bus, the ALT cb will trip isolating the bus from the alternator: if this is the case would not an excessive current draw from the bus result in the alternator field cb to trip as well as the altrnator will be coaxed to overwork?

Many thanks for your help



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