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In a message dated 6/21/2005 3:31:29 P.M. Central Standard Time,
walter@advancedpilot.com writes:
OK, here
are some facts.
Those that have carbureted engines (O 320/360) and
turn on carb heat see a much greater rise in inlet air temp since the air
is heated by the exhaust pipe.
That is not correct.
They will see a much smaller IAT rise in temp than 100 degrees. Try
it. I have. In my carbed engine, full carb heat will
result in a 50dF rise--maybe. That's not close to 100 degrees
and one should remember that the effects of IAT are not linear on
detonation margin. What is the large margin that has been reduced
a little? How is it related to Compression Ratio? We need
facts, not generalizations.
If you are interested in facts, then it
should be measured, not guessed at. If those of you doing this have
not taken an engine to a computerized test stand to accomplish this, then
you are guessing. There are several factors in detonation
margin. If we remove the fuel factors, we are left with IAT,
compression ratio, and CHT as major players. Using higher CR AND
higher IAT are both going the wrong way. There is a neat little
graph of this in Taylor you can look up. It is pretty impressive how
quickly the changes occur.
Walter,
The only facts here are that your engine sees a 50F rise in carb heat temp,
I will measure my heater air temp and lower cowl exiting air temp and get back
to you on that one. The other is that we all know the fact that
higher CR and higher IAT gets one closer to detonation. Please don't tell
me that a 8:1 CR IO 360 with a turbocharger that raised the inlet temp
100F is going to detonate running ROP. How about a supercharger that
delivers 40" MAP to a 7.5:1 Lyc IO 520? With no intercooler doesn't
the inlet temp rise 100F or more?
Who is Taylor?
Scott Krueger
AKA Grayhawk Lancair N92EX IO320 SB 89/96 Aurora, IL
(KARR)
Run Rich, Run
Fast.
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