Mailing List flyrotary@lancaironline.net Message #52376
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: SAG from Paducah
Date: Fri, 1 Oct 2010 10:40:23 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Charlie, I agree with your assessment.

Certainly is possible to have pre-ignition without detonation.  Pre-ignition simply means something is firing the combustible mixture before its intended ignition point - most of the time this is caused by some element (carbon, metal) retaining sufficient heat and temperature from the last combustion event to prematurely fire the next combustion event.

Pre-ignition generally results in higher combustion chamber pressure and heat as frequently the combustion event is started long before its intended and may occur as the piston/rotor is coming up on its compression stroke.  The piston trying to compress this burning mixture adds to the pressure and heat load.   Continued pre-ignition continues to build up the heat load until seals, sparkplugs, etc start to deteriorate - if continued it  frequently leads to detonation which can quickly lead to destruction of the engine (at least in piston engines).   So pre-ignition can raise indeed raise coolant temps due to this increased heat load.  When the combination of heat load and pressure reaches a certain point the combustible mixture can explode rather than burn - detonation has begun.

Detonation does not necessarily add greatly to the heat load above that already caused by pre-ignition - but since detonation is essentially a situation where the combustible mixture is no longer burning but actually exploding.  The combination of elevated heat/temperature  and shock of this exploding (rather than burning) mixture can in short order destroy an engine.

 Now our rotary engines appear to be less prone to detonation and the quenching effect of its less efficient combustion chamber shape may be to our advantage in this case.   I have experience SAG a number of times and I never got the impression the engine was under stress (same can not be said for me), in fact if anything the lesser rpm and EGT always let me to believe it was producing less power and therefore under less stress.  In otherwords, my impression was the problem was the engine was failing to light off the combustible mixture and therefore was producing less power (and thereby less stress on the engine).  So while something to be concerned about, I had not felt SAG was dangerous (other than to seat cushions).

I have had detonation completely destroy my spark plugs in very short order - but, it took extreme missetting of my static  ignition point to do this.  I have never detected any damage (even to the plugs) through the normal SAG event.  So in our case, I guess its possible that pre-ignition in the rotary is not as conducive to detonation - or perhaps we are not getting pre-ignition?

It's always great to understand what is happening to our engines - but, regardless of the ultimate cause of SAG, we do know that replacing the plugs does provide a fix (if only temporarily {:>)) and a fairly inexpensive one.  I am awaiting Steve's experiment with colder plugs - even extending the my current SAG interval from 25- 50 hours would be worthwhile

That's my take on it.

Ed

--------------------------------------------------
From: "Charlie England" <ceengland@bellsouth.net>
Sent: Friday, October 01, 2010 9:59 AM
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Subject: [FlyRotary] Re: SAG from Paducah

>
> I've only been scanning this series of emails, but it looks like both
> terms pre-ignition & detonation have been applied to the SAG symptom.
> Isn't it possible to have pre-ignition (causing elevated water temps,
> etc and declining EGT) without detonation, and the resulting destruction
> of plugs, seals, etc?
>
> Charlie
>
> --
> Homepage:  http://www.flyrotary.com/
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