In a message dated 1/4/2008 6:56:41 P.M. Central Standard Time,
glcasey@adelphia.net writes:
The
possibility that Steve suggests below is probably real, but remember that the
electronic ignition will only advance when the manifold pressure - and hence
the cylinder pressure - is lower than the max (only at high altitude or part
throttle). And the electronic ignition will only advance 5 or so degrees
more than the mag anyway. In 5 or 10 degrees the cylinder pressure will
not rise much.
Gary,
Because I am running at a 9:1 CR, my base timing is 20 dBTDC. Light
Speed EI recommends that 20 dBTDC base timing for engines operating with
CRs greater than 8.7:1. At 80% to 110% my timing is less than 25
dBTDC. At 25**2 the timing is right around 25 dBTDC. At race power,
2750 RPM, 30" MAP, I typically see 21 or 22 d BTDC. At low power settings
enforced by high altitudes, thus reducing my WOT MAP, I see 28-30 dBTDC or
so. At idle power settings, say 10-12" MAP, 900-1100 RPM, I generally see
34+ dBTDC. It all works out very nicely. That means my timing span
is as much as 34 degrees, depending.
I did a great number of experiments with the LASAR ignition where I would
fail the EI in flight, reverting to the fixed timing mags and compare
the results. Too bad I didn't have any timing data on the EI
function. Also, note that I now use the LSE (Light Speed) EI system.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)
Pilot
not TSO'd, Certificated score only > 70%.
PS: Colyn, FYI see LSE timing data listed
above.