Mailing List flyrotary@lancaironline.net Message #10095
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Turbo and the EC2
Date: Fri, 30 Jul 2004 16:05:31 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Message
Well, its generally accepted that retarding ignition timing as boost increases is one way to make certain you don't get into detonation situation.  I guess I would wonder about why the timing between leading and trailing would be critical.  It could be that since with boost you have higher combustion chamber pressure which supposedly leads to faster combustion propagation of the wave front - that the split could be a factor. 
 
It could be that   with faster combustion wave propagation that you would want the timing of the lead and trail closer in timing rather than further or possibly vice versa {:>). 
Ed Anderson
RV-6A N494BW Rotary Powered
Matthews, NC
----- Original Message -----
From: John Slade
Sent: Friday, July 30, 2004 3:11 PM
Subject: [FlyRotary] Re: Turbo and the EC2

 > From what perspective, John?? 
I'm hearing from Leon that the ignition timing in general, and specifically the timing split between leading and trailing is CRITICAL to turbo installations.  I "think" Tracy is retarding the ignition with boost, but I don't know how much.
 
I wish Tracy was back on the list and had time to read it. :(
John
 
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