I have a question about electronic CDI ignitions:
The CDI units designed for model aircraft typically have a hall effect sensor activated by a magnet attached to the crankshaft.
This makes perfect sense for a two stroke. When the piston hits TDC the magnet passes the sensor which gives a spark- good.
If the magnet is on the crankshaft and we have a 4 stroke we only want a spark every *second* time the magnet passes the sensor. Not only that, but the spark has to be generated on the right pass. ie- TDC before the power stroke, not TDC before the intake stroke.
How does this happen?
I see conversions of 4 stroke engines (E.g. Saito's) where the sensor/magnet is apparently on the crankshaft. I understand the electronics could do a divide by 2 easily enough, but how do you get the spark on the right stroke?
Am I missing something?
Thanks,
Jason H.
The CDI units designed for model aircraft typically have a hall effect sensor activated by a magnet attached to the crankshaft.
This makes perfect sense for a two stroke. When the piston hits TDC the magnet passes the sensor which gives a spark- good.
If the magnet is on the crankshaft and we have a 4 stroke we only want a spark every *second* time the magnet passes the sensor. Not only that, but the spark has to be generated on the right pass. ie- TDC before the power stroke, not TDC before the intake stroke.
How does this happen?
I see conversions of 4 stroke engines (E.g. Saito's) where the sensor/magnet is apparently on the crankshaft. I understand the electronics could do a divide by 2 easily enough, but how do you get the spark on the right stroke?
Am I missing something?
Thanks,
Jason H.