A Call to LSE helped clear up some questions:
Q: Does the dual LSE system rely only on the primary sensor for timing so
that both sides would be sync'ed?
A: No, each side uses its' related sensor for timing. If a sensor
fails, the dual system will use the information from the remaining operating
sensor. Each side communicates with the other and that is how a timing
difference between the two can be displayed.
Q: I note that when I use the mag hole sensors, I have to correct the
displayed timing if I have, as suggested, retarded the timing by setting the
apparent TDC 5 degrees after the true TDC because of high compression. Why
not so with the crank sensor?
A: The Mag hole sensor is fixed at detecting 45 degrees before TDC and
TDC. Based on sensor position (and other factors), the BTDC timing is
computed and initiated at the correct moment. The system still
thinks true TDC is TDC, thus the displayed valued must be mentally
adjusted. If the engine base timing is 25 BTDC, the crank sensor magnets
are 45 degrees apart unless it is a high compression engine where the
lead magnets would be placed at 40 BTDC. In this case, the computed and
displayed timing is the true timing.
Q: Why is the display RPM so different than that shown by my VM system and
what should I do about it?
A: There seems to be an effect from the hookup to the digital VM RPM
back into the LSE unit, causing the analog display to be at a discrepancy.
Note that .01 V is 100 RPM on the LSE display. There is no effect on
the RPM used by the LSE unit to compute the timing. In a dual setup, one
could hook the VM to one unit and the LSE display to the other. The
VM RPM display should be accurate. (Note: at some future time, I
will take the digital RPM output from each LSE unit and run it through
a selector switch and then to the VM input.)
Q: Why was my initial timing display at 1000 RPM off by 1 degree
between left and right and, in flight at 2500 RPM it was off by 2.5
degrees.
A: Gear lash at the sensor/mag drive gears. Timing should be
verified at above 1600 RPM to eliminate the gear lash for 4-cyl
engines at low RPM.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)
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