For the Corvair crowd, I think you'll find that they have a mechanical advance 
set up. While that's not ideal, and doesn't necessarily fit all situations, it 
works reasonably well. 

 Aircraft engines are typically configured to prevent detonation under the 
worst circumstances; hot engine, marginally lean mixture, hot day, and sea 
level/ high manifold pressure situations. That's why the O-200s have the timing 
set at 28 BTDC (24 BTDC with old style cylinders) or most Lycomings are set at 
25 BTDC.

 For both the Corvair mechanical advance and the fixed timing magnetos, they 
are configured to prevent detonation under the worst case scenario. Aircraft 
engines, whether they are Corvair, VW, Continental or Lycoming are essentially 
a one speed engine with the exception of starting and idle. With the Emags, 
Light Speed Ignition, and a few other aftermarket magneto replacements, the 
electronics sense both rpm and manifold pressure and use that to calculate 
timing advance on a timing curve. Emags are designed for the Lycoming engines 
and advance up to 38 BTDC with low manifold pressure (like under cruise 
conditions). Light Speed goes up to 41 BTDC with the right combination of RPM 
and MP. This may provide a marginal increase in power witha tiny bit more 
timing advance under full throttle conditions, but the beauty of them is the 
extra advance that kicks in when the manifold pressure drops, like in low 
throttle or high altitude cruise operation. Under those circumstances, the 
extra advance can save significant amounts of fuel as the extra timing advance 
gives a better burn without the danger of detonation under low power operation.

 -Jeff Scott
 Los Alamos, NM

----- Original Message -----
From: Craig Williams
Sent: 06/09/11 09:43 AM
To: KRnet
Subject: Re: KR> Combustion process

 Very good read! Does this mean we need is an advance/retard control in the 
cockpit in addition to the mixture control? Craig www.kr2seafury.com --- On 
Thu, 6/9/11, Paul & Karen Smith <pk.sm...@bigpond.net.au> wrote: > From: Paul & 
Karen Smith <pk.sm...@bigpond.net.au> > Subject: KR> Combustion process > To: 
"KRnet" <kr...@mylist.net> > Date: Thursday, June 9, 2011, 1:27 AM > A good 
read... > > http://www.innovatemotorsports.com/resources/myths.php > > Paul 
Smith > Brisbane, AUSTRALIA > pk.sm...@bigpond.net.au > 
http://kr2spacemodulator.blogspot.com/ > > > 
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