If you fly recips, what leaning procedure do you use? Chances are that almost everything your CFI told you about using the red knob — and most of what you've read and heard since then — is just plain hogwash! We suggest you forget everything you thought you knew about the subject, and let AVweb's John Deakin show you how to optimize engine efficiency and longevity through enlightened mixture management.
June 14, 1999
|About the Author ...
John Deakin is a 35,000-hour pilot who worked his way up the aviation food chain
via charter, corporate, and cargo flying; spent five years in Southeast Asia
with Air America; 33 years with Japan Airlines, mostly as a 747 captain; and
now flies the Gulfstream IV for a West Coast operator.
He also flies his own
V35 Bonanza (N1BE) and is very active in the warbird and vintage aircraft
scene, flying the C-46, M-404, DC-3, F8F Bearcat, Constellation, B-29, and
others. He is also a National Designated Pilot Examiner (NDPER), able to give
type ratings and check rides on 43 different aircraft types.
There are few things in airplanes as
misunderstood and misused as the mixture control. Old Wives' Tales (OWTs) abound, many of
them spread by POHs, the FAA, and even the engine manufacturers! Not much of what you've
read and heard about mixture management makes sense much of it is out of context, and
most of the good stuff is so dry, dull and boring that it's tough to get through it
without falling asleep.
I have flown with pilots who say, "Oh, I never lean, it's just too complicated,
and fuel is cheaper than an engine overhaul, anyway." What really annoys me is
that some of them even make TBO that way! What they don't think about is how many problems
they have enroute to TBO fouled plugs, burned valves, cracked cylinder heads, etc.
and how much money they waste on fuel. Even worse, they don't think about how much time
they waste making unnecessary fuel stops. Yeah, yeah, I know, your bladder range is more
limited than your fuel range. I've heard that before, but it sure sounds like a cop-out,
Ever make an extra stop for "cheap fuel?" Do you feel
smug when you buy fuel for ten cents a gallon less than usual? Why, then, do so many
pilots fail to learn a little about their engines and save 20% or more on fuel used?
That's just like getting forty cents off per gallon, these days! What am I missing
Others will tell me, "I lean to 50° F rich of peak, just like the POH says,"
not realizing that this can be and often is the very worst possible setting they can
Still others will decide on some arbitrary power setting with no particular logic in
mind. 65% is a very common level. They'll carefully set the MP and RPM to the book values
for 65% and figure that's all they have to do to attain that power setting. Wrong, it also
takes a very careful mixture setting, as well!
Don't be afraid of that red knob. Learn to use it! With a few pretty obvious exceptions
there is nothing you can do with the mixture control over a short period of time that will
hurt you or the engine. Used properly, you'll save a lot of fuel, your engine will run
cooler, cleaner, smoother, and longer, with less maintenance expense and downtime along
the way to TBO.
There! Now that I've gotten all that off my chest, lets see if we can make a little
sense of all this. If you haven't read my previous columns on manifold
pressure and props, this would be a good time to do so, as
this is the third in a series and builds on those earlier efforts.
I'd like to first discuss some things about the fuel we use, then go rather deeply into
the operation of a "perfect" engine. After that, I'll offer a little history of
why and how our engines are not perfect, and what we can do about it.
If you've been to the movies, or watched TV in the last 30 years, you've undoubtedly
seen the shot where someone pours a long trail of gasoline on the ground, then strikes a
match and lights it off. If you watch closely enough, the flame is a fairly gentle one,
and the flame front moves fairly slowly until it reaches whatever is going to explode, and
then blows up violently. A favorite shot is the car gas tank. While Hollywood plays
tricks with physics now and then, this particular one doesn't need much fakery: it's quite
But why does the fuel burn so slowly as the fire snakes across the ground, and
why does it blow up so violently when it reaches its intended destination? The short
answer is "mixture."
By itself, gasoline won't even burn. Try dropping a lighted match on the tarmac and
then pouring some liquid gasoline onto the flame: You'll put the fire out. This is the
"too rich to burn" case.
Returning to that movie scene, the trail of gasoline across the ground only burns
because the gas is evaporating, changing into a vapor, and at some point above the surface
the mixture will support combustion. That little bit of vapor burns, lighting off the next
few molecules, which light off the next batch, and so on.
If we could closely examine what's going on, the surface of the liquid fuel would not
be burning at all, there would be a thin layer of very rich vapor just above it, also too
rich to burn. At the point above the surface where combustion does take place, the fire
burns "up," and all the combustible mixture above that point also burns. Blow a
gentle breeze across this process ("fan the flames"), injecting more air into
the process (leaning it out) and you'll see a much more vigorous flame, and a much faster
flame front. Blow even more air, and there will be too much air (too lean), and the fire
will slow down again, and ultimately go out.
Now, what happens when the burning trail of gasoline reaches its destination? If the
fire hits a full gas tank, the fire will simply go out! The liquid is again too
rich to burn. But if the tank is partially empty, there will be a nice volume of
combustible gasoline vapor at just the right mixture in the upper part of the tank. The
smallest spark is more than enough to light that off, and the flame front will expand
rapidly in all directions. The rapidly expanding gasses will blow up the tank, scattering
the liquid fuel, nicely mixing it with air, and creating an even larger volume of highly
combustible fuel/air mixture. Technically, this is not an explosion: It's still just
burning. But it takes place so quickly that it appears to explode.
Another example. Propane (or acetylene, or any flammable gas), right out of the tank,
makes a rather lazy, sooty yellow flame that really isn't very hot, only a few hundred
degrees. Add air to that mix, push it out that pipe under some pressure, and it turns into
a hissing blue jet of flame at several thousand degrees. Your gas stove is cleverly
designed so that the rising heat sucks air into the gas stream, making a mixture that
burns with a nice hot blue flame. But mix too much air with that gas, and the flame
becomes weaker, weaker, and finally dies out the fire is burning so slowly it simply
can't leap from molecule to molecule. Well, at least that's the way I like to think of it!
All this is a very good thing, because if any of these substances could burn on their
own, the fire would run right back down the supply line to the tank, and burn it all
How does this translate into the gasoline-powered, spark-fired, internal combustion
engines found in our airplanes (and also in tractors, lawn mowers, and cars)? For purposes
of this article, I'll limit my discussion to normally-aspirated engines, leaving
turbocharged ones for a future column.
In the engine that powers my Bonanza (a TCM IO-550), if I flip the boost pump to high
with the mixture rich, I can literally "flood" the engine and kill it, even at
takeoff or climb power settings. (Update Oct. 2005: This column was written in 1999, when I believed that to be true. Alas, it is not completely so. At low power settings, it is true, and illustrates the principle nicely. But most of these engines -- including mine -- tolerate the boost pump very well at high power settings. Indeed, the boost pump can be your friend if taking off with hot fuel in the tanks, or if you climb rapidly, as with the Turbo'd aircraft.)
Any malfunction that pumps "too much" fuel into
the combustion chamber (relative to the air) will do the same thing. The fuel is flowing,
the spark is sparking, and the airspeed is still turning the prop, but there's just too
much fuel and not enough air. Flip the boost to "Low" or "Off" or lean
it out with the mixture control and the engine will run again. Given the correct fuel
flow, air flow and spark, it must start and run.
An aside here. Two people report that when they have run a tank dry as I described in another column, they have
had a minor problem re-starting. This may be a possible explanation if they shoved the
mixture in and flipped the boost pump on at high altitude. The engine goes quickly from
"no fuel" to "too rich to run" and can't start. If you run into this
problem, don't change anything but the fuel selector, and maybe flip the boost on
momentarily, just to get the fuel started again to the engine-driven pump, then turn it
off again. That engine will start. After all, it is FAA-certified to do so!
At the other end of the spectrum, pulling the big red knob all the way back cuts off
all fuel to the engine, making the mixture "too lean" and also causing the
engine to quit. We do this to shut down the engine on most airplanes, so this is more
familiar territory to most.
Somewhere in between those two extremes of "too rich to run" and "too
lean to run," there is a small range of mixture settings that will allow the
engine to run. At each end of that small range, the engine doesn't really run very well,
but things get better in the middle of the range. It is this range of
"burnable" mixture we need to understand. So, read on.
(This picture, and several others in this column comes from the superb Pratt &
Whitney "The Aircraft Engine and its Operation", February 1955 edition. I have
arranged to have this publication duplicated, copies available for $60. 150 B&W pages,
38 in color. If you want a copy, drop me an e-note at email@example.com.)
The chart above depicts only the lower end of the mixture range, from "no
fuel" to about 20% fuel, by weight. Obviously, any mixture greater than 20% fuel is
also "too rich to burn."
Note also that only a very narrow part of this will actually support combustion at all,
from roughly 5% to about 12.5%. Remember we're talking here about weight of both
air and fuel. At 20:1 by weight, the mix is 20 pounds of air, and 1 pound of
fuel. By volume, that's about 11,700 gallons of air for each gallon of fuel.
Let's do a little thought experiment here. Assume you are in cruise at 10,000 feet,
with wide-open throttle and the prop control set to2,300 RPM. Now cut the mixture,
shutting the engine down. The prop governor will attempt to maintain that 2,300 RPM, and
for the purposes of this exercise, let's assume it can, and does. Thus, even with the fuel
cut off, the engine is still turning, the pistons are still pumping air, and you'll still
have the same manifold pressure (about 20 inches). All engine instruments will remain
normal, except CHT and EGT which will drop pretty quickly. You establish a nice power-off
descent with enough speed to keep the prop windmilling within the governing range. (This
is a learning exercise, and not an engine-out drill, where you'd reduce to
For most normally-aspirated engines, as you get down around 8,000 or 9,000 msl, the
resulting manifold pressure and RPM will be approximately correct for the classic
65% power setting. How much power are we getting? None, of course, or 0%. My point
is that MP and RPM alone do not determine power output. Obviously, mixture plays a major
part in the power equation, too!
Continuing our thought experiment, you're at the extreme left end of this chart, all
air and no fuel ("too lean to burn"). Now, start easing the mixture control in
(moving to the right on the chart). At some point, that will begin to allow fuel into the
air, but still, nothing happens until that "mix" gets to the 5% point. At about
that point, the engine will start rather abruptly. If you look closely at that chart, the
power curve rises just about vertically to around 30% of power, and only a tiny bit more
fuel will bring it to 50% power. After that, it takes larger and larger increases in fuel
to get to 100% of available power. Note there's a fairly wide "flat spot" on top
of that curve, where power stays pretty constant. Note also that if you enrich even
further, power drops off again ultimately, to zero ("flooded out").
Adjusting the mixture level (by weight) to about 8% fuel will get the absolute maximum
horsepower out of that fuel and air mixture, so we call that "Best Power
Mixture." No matter how you play with the mixture, that's the best you can do for
sheer, raw power. This setting is useful for maximum speed, maximum climb, and for
converting gas into noise. This is "Maximum Power for the Fuel and Air
Most of the cruise performance charts in General Aviation aircraft POHs either don't
mention it all, or there is a tiny note somewhere that the chart numbers are valid only
with a mixture setting at "Best Power" (at the top of our power/mixture curve).
This is often a marketing ploy, as faster airplanes sell better.
Now here's a slippery concept for many (well, at least I had trouble with it). If we
re-lean the mixture a bit, say 10% (moving back to the left on the chart), the power
doesn't drop very much, perhaps only 5%. Hmm, think about that. 10% less fuel, 5% less
power. This seems more efficient and it is. We're not getting the maximum horsepower,
we're getting a little less, but for a lot less fuel. (There are many things
in aviation that work this way. Give a little here, get a lot there.) Tests have shown
that at about 6.25% of fuel (by weight) we won't get as much power (it'll be roughly 80%),
but we will get the most power per gallon, and we call this "Best Economy".
To look at it another way, by running at "Best Power," we are wasting a
little fuel to increase the power.
In this context, when we speak of "power," we're speaking of the power
available from a particular amount of air and fuel, and not some percentage of
"rated power" from the engine. In other words, this mixture diagram applies
whether we have half throttle and 1500 RPM, or any other setting. For any given
setting of throttle and manifold pressure, this chart of combustible mixtures applies.
In fact, sitting on the ground, idling at 1,000 RPM, you can see this. The prop is well
out of the governing range and at its flattest pitch. RPM is thus a direct indication of
power. Full rich, flip the boost pump on, and you may flood the engine out completely. But
quickly pull the mixture knob back to keep it running. With this setup, you can vary the
mixture, and watch the results on the tachometer. Too rich, the RPM will be low, the
exhaust will be sooty. Lean it, and you'll come to an RPM peak. Keep leaning further and
the RPM will drop again eventually to zero. It gets very sensitive at the extremes,
because of the steep slope of the curve on the combustion chart.
The mixture control is the most important "power control" we have! Using the
mixture alone, we can vary the power from zero (lean) to "full," and back to
zero (rich). We can't do that with the throttle (there's always some power at idle) or
with RPM (unless we can feather the engine.) Of course, for practical purposes, the real
range of power control through mixture adjustment is from about 30% on the lean side, to
100%, and back to 30% on the rich side.
For far too long, these engines have been run with no science at all. We simply haven't
had any decent instrumentation to tell us what's going on in the combustion chamber. If
you've read my previous columns on manifold
pressure (MP) and props (RPM),
you now realize that neither MP nor RPM is a very good indicator of power or what's
happening inside the engine. The story they tell is incomplete, because it ignores the
profound effects of mixture.
If your airplane has the old-style Cylinder Head Temperature (CHT) instrument, it
probably has a green arc (or line) to denote normal operating range, with a redline at the
upper end, and maybe even no numeric temperature markings at all. The CHT probe is often
not even on the hottest cylinder, or in a location that will yield useful information. The
early single-probe Exhaust Gas Temperature (EGT) systems were little more than a good
thought, because some only measured the EGT in a single cylinder, or an average of half
the cylinders, or maybe an average of all the cylinders (depending on the probe location).
What few realized is that because of a severe mixture maldistribution, these engines are
nothing more than a collection of four or six separate one-cylinder engines, flying along
in loose formation. A single EGT indication from one of them or even an average of all
of them is virtually meaningless, because the others are certainly doing something very
different from the one you're watching.
In the big old radials, where we can often watch the exhaust at night, we can see
directly what is happening. At full rich (takeoff and climb), the exhaust is a bright
yellow, with visible flames licking (slowly, relatively speaking) back along the cowling.
Lean it out, and the flame turns blue, becomes shorter, and burns more intensely
(quicker). Keep on leaning, and it turns white with a noticeable loss in power. If you
lean it far enough, the fire goes out and the engine quits. In the early days of the big
radials, it was easy enough to learn how to lean the engine by sight at night, develop a
"feel," and duplicate it closely enough in the daytime. The design of the big
radials also allowed a direct measurement of actual power being delivered to the prop, and
this led to some very scientific leaning methods indeed, based on actual power. This
"art" had become a real science towards the end of the heyday of the big radials
on DC-7s, Connies, and others both in the airline world and in the military. By any
accounting, there were several hundred million hours of accumulated experience on large
fleets, under highly controlled and monitored conditions, by professional crews who had to
operate in a very consistent and standard way, using some pretty sophisticated tools for
Another wonderful feature of the radial engine is that the intake pipes are all the
same size and shape, and they radiate from a central point. This gives a wonderfully even air
distribution to all cylinders. In many of the radials, there is also a gear-driven
supercharger at that central point, which is just a centrifugal impeller. The fuel is
often sprayed into the airflow just before it gets to that impeller, resulting in a nice,
even mixture. As a result, not only is the air distribution very good, but so is the fuel
We lost all that with the "flat fours" and "flat sixes" that power
most GA aircraft today. There is no practical way of measuring power directly, the exhaust
cannot normally be observed from the cockpit, and the mixture distribution is often
dreadful as the engine is delivered from the factory. Intake pipes of the "log
runner" type are of dramatically different lengths for different cylinders. Despite
this, the actual air distribution is pretty good in the big-bore TCM engines. Most
Lycoming engines, however, have a "plenum" type induction system that provides
somewhat unbalanced air distribution that changes with engine RPM.
Many of these engines have terrible fuel distribution. The carbureted engines are the
worst, but many fuel injected engines are not a lot better. (Fuel injection does have
other benefits, however.) Again, what we really have is six (or four) cylinders flying
along in loose formation, each doing their own thing with regard to mixture, while the
pilot has only one mixture control, a "master mixture" if you will, which simply
controls total fuel flow to all of them.
Here's what that looks like in a typical TCM IO-520 or 550, with stock injectors, and
all cylinders instrumented. Some engines are "better," others are
For simplicity, this chart shows only the six EGTs plotted against fuel flow. In this
chart (unlike the previous one), "richer" is to the left,
"leaner" to the right. If you start with "full rich" on the
left side, and lean slowly, you will see all EGTs rise together at first. At about 14.5
GPH, the #1cylinder peaks, and then starts cooling off on the lean side of peak. Very
shortly thereafter, #2 does the same. (#1 and #2 are the rearmost cylinders in the
big-bore TCM engines.) We continue leaning, and soon #3 and #4 (the middle cylinders) hit
peak EGT and start down, while #5 and #6 continue rising. Finally, at about 13.3 GPH, the
last cylinder peaks. But what has happened to number 1, the first cylinder to peak? It is
now 40 degrees lean of peak (LOP)!
That relationship between "Best Power" and "Best Economy" is but
one aspect of this subject. What is happening to the EGT while we lean? What is happening
to the CHT? What is happening to the fuel consumption, and the power? More importantly, what
is their relationship to each other?
TCM, like Pratt & Whitney and Wright before them, publishes a neat little chart
showing this. Some are surprised that the charts from these different engine manufacturers
all look just like each other! When you think about it, this is not really that strange,
because the principles are the same, the metallurgy is the same, the sparks occur at about
the same time and the geometry of the pistons, rods, and crankshafts are the same, whether
the engine is from a DC-7, a Bonanza, or a John Deere tractor. Here's one such
"relationship chart" from TCM:
Now, please stop right here. DO NOT just skip over that chart, it's important.
It looks a little complicated, because there are four parameters on one chart, and each
needs to be understood. If you are not prepared to understand that chart, I don't think
you can understand how to operate your engine properly, much less understand the rest of
this column. Please take the time, right now, to follow me through on this chart!
The entire chart represents data while running at 25.0 inches of manifold pressure and
2,500 RPM. Those are held constant only the mixture changes.
Please read the preceding paragraph again, it's VERY important.
The only variable is the fuel flow, plotted across the bottom of the chart, and all
four parameters are plotted against that fuel flow from 75 to 120 pounds per hour (PPH).
This gives a lovely picture of the relationships. Note that "Richer" is again to
the right on this chart (I could have swapped some of these charts left to right to
make them all the same, but preferred to stick to "authentic.")
The right side of the chart is not necessarily "Full Rich". For
whatever reasons, TCM chose to show just the range of fuel flows from 75 to 120 PPH on
this IO-550, while "full rich" at sea level is about 162 PPH
The top curve shows EGT, aligned with the numbers on the right side, from a low of
1,350° at 75 PPH (lean), peaking at about 1,520° F at 95 PPH, and dropping again to
1,380° F at 120 PPH (rich). This is a classic EGT curve, and many of you will be familiar
with it. There, now that's not so bad, is it? And you thought this chart was too
Below that is the CHT curve, with the scale at the left. About 310° F at 75 PPH
(lean), peaking at about 425° F at 105 PPH, dropping again to about 405° F at 120 PPH
(rich). Note the CHT peaks at a substantially richer mixture than EGT. (In fact, you'll
see that the hottest CHT occurs at the point where EGT is about 50° F rich of peak (ROP).
Hmmm, where have we heard that before?)
The third trace from the top is "brake horsepower" (BHP), which we can just
call "Power" as delivered to the shaft. The numbers for this trace are on the
right, and our trace shows 180 HP at 75 PPH (lean), peak at about 250 HP for fairly broad
range of fuel flows, and drops only slightly to about 245 HP at 120 PPH (rich). Note that
going all the way to "Full Rich" would produce a good deal more fuel flow and a
good deal less power.
Finally, the bottom curve depicts "Brake Specific Fuel Consumption" (BSFC).
This fancy-sounding engineering term is nothing more than the fuel required to produce one
horsepower (HP) for one hour.
A useful trick to help you understand this chart is to lay a clear plastic ruler
vertically on the chart. Keeping it vertically oriented, move it back and forth
horizontally. As one end of the ruler moves over the fuel flow scale at the bottom of the
page, the four curves will move up and down along the ruler's straightedge, just as those
parameters move up and down in the real world.
Remember earlier, where I said we could lean a lot and only lose a little power? Well,
this curve gives us a visual idea of how that works. At 75 PPH (lean), it takes about
0.425 pounds to produce one HP for one hour. In the range 85 to 95 PPH, less fuel is
required: about 0.385 pounds of fuel. Enrich further to 120 PPH, and you'll be burning
about 0.480 pounds of fuel to produce one HP for one hour. In this case, "less is
better" if we're looking for economy. BSFC is a very useful term, as it is a direct
indication of an engine's efficiency. Modern automobile engines, contrary to popular
belief, are not very efficient, having BSFCs above 0.42 or so. They are designed to run
very clean, however, and sacrifice some efficiency as a result. TCM engines can achieve
BSFCs as low as 0.385 from the factory. With modifications, we're going to do better than
that. Not too shabby for "World War II technology," as so many call it!
Now, here's the crucial concept behind this chart: All four curves are carefully
plotted with reference to the fuel flow scale at the bottom, and this gives us a lovely
opportunity to look at the relationships between them! If you'd like to know what
is happening to CHT as you fiddle with EGT, the answer is here.
For example, let's say we've leveled off in cruise, allowed things to settle down and
it's time to lean, at whatever MP and RPM you choose. Starting from full rich (perhaps
well off the right side of this chart and due to the enrichment feature at full throttle),
we start leaning. According to the chart, the EGT and CHT will rise, and we know this to
be true from experience. The power rises only slightly. If you're going for absolute
maximum altitude or speed, that very flat "peak" in the BHP curve that occurs
around 105 to 110 PPH fuel flow will be helpful, and if you're making a high-altitude
takeoff, it will be very helpful. The BSFC is dropping as you lean, of course,
you're getting "more efficient."
So as the mixture is leaned, power peaks first, with CHT peaking at very close to the
same point. In practical terms, if we lean to max CHT, we'll have max power for that
MP/RPM setting. Doesn't that make sense, intuitively? Max power, max CHT? It's not precisely
true, but it's close enough.
Ok, so power peaks first, stays pretty flat, and then CHT peaks shortly thereafter.
With continued leaning, power and CHT drop together very gradually at first, then
progressively more steeply while BSFC continues to improve and EGT continues to rise.
Continue leaning, and EGT peaks and begins to fall, while BSFC continues to improve.
Sure, we're losing power, but fuel consumption is declining even faster, so our
"economy" (as measured by BSFC) is still getting better.
Finally, BSFC bottoms out (at "best economy mixture"), and stays pretty flat
between 85 and 90 PPH. If we disregard the small difference between 0.385 and 0.400, we
could even stretch the point a little, and say the BFSC curve is "kinda flat"
between 85 and 100 PPH. Look immediately above at the HP curve, and note that for a small
loss of fuel efficiency, we can pick up 25 to 30 HP? Isn't that interesting? We'll see
later how that affects airplane performance and efficiency, a very different
subject. But to make a long story short, if the power setting that results from optimizing
engine efficiency causes your airplane drop below the airspeed range that provides optimum
aerodynamic efficiency, you're not gaining anything! That's a whole 'nother can o' worms.
(I feel another column coming on.)
Let's say we have carefully set up a real 65% of rated power, using the required
MP/RPM, with the mixture leaned to Best Power.
What would happen to this if we increased the MP and/or RPM, keeping the mixture
constant at Best Power? More power to the shaft, right? Think about what this might do to
that chart. Since the power moves up, all the curves must move up. Since the peak EGT will
occur at a higher fuel flow, it must move to the right, and all the other traces will move
right, too, to preserve the interrelationships.
Here's what that looks like:
Note the left-right relationships don't change on this chart, because we've fiddled the
fuel flow scale at the bottom to keep them aligned.
Heads up, crucial concept coming! Assume that we increase MP to increase power output
to something substantially above 65% power. Now suppose we lean the mixture a bit, until
the actual power drops to exactly 65% power again?
Here's exactly what that looks like:
This is a real picture of a Cessna 414, previously trimmed up very carefully for
straight and level flight at equal MP, RPM, and mixture settings. After that, the throttle
is increased, and the mixture decreased, to produce what you see here, with no tendency to
yaw/roll/turn. This situation is actually very sensitive to very small differences in
Remember,both engines are producing exactly the same power!
The left MP is 3" higher than the right, but the left fuel flow is 3.2 GPH lower!
Note further, the EGT is only 10° F higher, but the CHT (as shown by the missing bars on
the Graphic Engine Monitor display) are 1 to 3 bars lower, with each bar representing 25°
Ponder this: cooler CHTs, less fuel, same power. Sounds like
magic, doesn't it? Why, if we could run that MP up high enough, and pull the mixture back
far enough, we might invent perpetual motion! Unfortunately, this is another aviation case
where a little is good, but "more" isn't. There are other forces at work.
Just as there is a right time to make your move on that blonde across the room, there
is a right time to "light the fire" in the cylinder. (In my experience, the
latter is far more easily determined than the former.) Intuitively, you would think it a
simple matter, just light it off when the piston hits TDC (Top Dead Center). But the fact
is, it takes quite a bit of time to light that fire, and for the flame front to propagate
sufficiently to do anything useful. The fuel/air mixture nearest the spark plug must be in
the combustible range, and the fuel molecules must be close enough together to continue
the process. Even under the best of circumstances, combustion is still something of a
random process, so there is a variation from cycle to cycle in the same cylinder. But for
the most part, the molecules cooperate with great glee, flinging themselves into the fire
in order to do useful work, even if that's only to transport us to the site of a $100
The best time to "light the fire" also changes with RPM and mixture. At a
high RPM, it takes a short amount of time for the piston to rise and fall. At a slower
RPM, it takes longer. But the flame doesn't know anything about pistons rising and falling
(or crankshafts turning), it's still burning at the same speed. (Well, almost.) This can
change the point at which useful work is done quite dramatically. When, then, should we
"light the fire?"
The answer depends on all three engine parameters mixture, RPM and MP so ideally
our ignition timing would be adjusted accordingly. Some of the big radials do in fact have
variable spark settings, but the flat engines most of us fly behind are stuck with fixed
timing. (But "Stand by for NEWS!") Since maximum power is the most critical
case, ignition timing is typically set to be optimum at full takeoff power, and operation
at lower power settings is something of a compromise.
At maximum power, long experience has shown that discharging the spark at 20° to 25° before
top dead center (TDC) is about right. That much " lead time" gives the fuel/air
charge time enough to develop a good fire, and the pressure will start to build just as
the piston reaches the top-of-stroke. From that point, the fire gets really serious, and
the pressure builds rapidly, just as the piston starts falling away.
Again, through long experience and actual measurement, it is clear that about 16° to
18° after TDC is the best place for that pressure peak to occur, in order to
extract the maximum amount of useful work, as shown by the following picture from the
Pratt & Whitney book:
As you can see in the first picture, when ignition occurs the crankshaft knuckle is
reaching the top of its arc, which also puts the piston very close to the top of its
stroke. At first glance, igniting the charge at 22° before TDC seems like it would be
counterproductive, since the piston is still coming up. However, in reality, it takes some
time for the fire to get going, and by the time that happens, the piston is already pretty
much topped out, so the building pressure cannot really produce the "negative
power" you might have expected at this point.
The second picture shows perfect TDC. No matter what the pressure in the combustion
chamber is doing, there is no "mechanical advantage", no leverage, as the piston
is just pushing straight down on the connecting rod, which is pushing straight down on the
crankshaft throw. Combustion chamber pressure at this point produces no useful work at all
(but it sure loads the bearings.)
The third picture shows the approximate position of the assembly at the peak pressure
point (PPP). If the pressure peaked a little sooner the piston would be at the top of its
travel, with less mechanical advantage on the crankshaft, and engine stresses would get
very, very high. At about 16° after TDC, some decent mechanical advantage is just
beginning to take place, and that allows time for the rest of the combustion event to
"push" the piston down. If the peak of the pressure pulse occurs much later than
16° , the initial peak would have a greater mechanical advantage, but then much of the
energy in the later stages of the combustion event would be lost. On balance, a PPP at
16° after TDC turns out to be about the best you can do. Another compromise.
At very high power settings (such as takeoff power), we've found that throwing extra
fuel into the mixture (providing an enriched mixture at the rich side of the flat peak of
the BHP curve) helps keep temperatures down and allows us to develop even more power
without the risk of detonation. This is why many engines have a "power
enrichment" feature at full throttle. We're willing to waste some fuel for a worthy
cause during takeoff, especially since we usually don't run at that high power for long.
What would happen if we got all the way up to this very high power, and then pulled the
RPM back? (Don't try this at home, folks!) Well, with the spark occurring at 22° before
TDC and PPP occurring at 16° after TDC at full RPM, there is a very precise time
interval between spark and PPP. The crankshaft rotation is 38° (22° + 16° ). If we
reduce the RPM by 20%, the crankshaft will turn only 30° (80% of 38° ) by the time PPP
occurs, so now the peak pressure will occur at only 8° past TDC.
The preceding analysis is actually a bit of an oversimplification. In reality, there
are other factors at work such as the rate of compression at the slower crank speed, so
the relationship between RPM and PPP timing isn't really linear. In this case, the PPP
would probably occur more like 12° after TDC.
In any case, at maximum MP and reduced RPM, the peak pressure will be much
higher, because the combustion chamber will be much smaller when PPP occurs. Since
the pressure will be much higher, the temperature will be much higher, and this increases
the risk of detonation. More on this later, but here's the same picture, this time
illustrating classic detonation:
This is the reason for the old rule of thumb, "Always reduce manifold pressure
before reducing RPM, and increase RPM before increasing manifold pressure."
This is not a bad rule, and it never hurts to do it this way. But you should understand
that it really only applies in the high-power case where the engine is operating at
maximum combustion pressures and temperatures, and detonation is therefore a possibility!
If you're cruising at 22" and 2,100, and want to increase to 24" and 2,400, it
doesn't really matter which control you adjust first, you won't hurt a thing. Sure, as a
matter of habit, run the RPM up, then do the MP. But the engine isn't going to blow up if
you do it the "wrong" way.
What about mixture at very high power settings? Remember, the engine manufacturer has
optimized everything to produce all that power, and many parameters will be running within
very narrow tolerances. Remember also the opening of this column, where I mention how much
difference mixture makes in the speed of combustion. At takeoff power, if we bring the
mixture control back a bit from full rich, the rate of combustion speeds up, and puts that
pressure pulse closer to TDC. Again, a very bad thing. (Combustion speed reaches maximum
around 50° F to 75° F rich of peak EGT, and further leaning causes it to slow down
Our POHs instruct us to use full-rich for takeoff. The extraordinarily rich
mixture is required to assure that detonation does not occur. The conventional wisdom is
that the purpose of the "excess" fuel is to cool the engine, but in fact its
primary purpose is to slow the combustion rate and delay the PPP, which eliminates the
risk of detonation by reducing the pressure peak. This does, in fact, result in cooler
operation, but that's actually a second-order effect of the delayed PPP. (If we could just
retard the ignition timing for takeoff, we wouldn't need to throw all that extra fuel at
Here's what Pratt & Whitney thought a combustion event looked like, back in 1948:
Note how the pressure rises gradually to the point at which the spark occurs. It then
rises very rapidly as the piston comes up to TDC, and continues to rise thereafter, mostly
because the piston hasn't dropped very far, due to the geometry of the piston rod, and
crankshaft throw. Wouldn't it be lovely if we could keep that same pressure on the piston,
all the way down? We can wish, can't we?
I don't know how Pratt & Whitney got that picture, but it's certainly pretty good,
because here's the real picture, as measured by the latest state-of-the-art digital
instrumentation at General Aviation Modifications, Inc. (GAMI) in Ada, Oklahoma:
|Looking Inside The Cylinder
You need to understand a little about how GAMI gathers this data to
appreciate the quality of what you're seeing. They use in-house proprietary software,
hardware, and test equipment to gather this data in ways that have never been done before.
Driven by George Braly (rumors of whips and chains and
piteous cries late in the night from converted tornado shelters abound) GAMI has developed
a portable 128-channel data acquisition system that can be installed and operated in a
Bonanza. It is entirely independent, with its own power source. Data can be captured to a
laptop computer's hard disk for later processing, and can also be displayed in real time,
up to 50,000 samples per second (all channels). Using specially-modified sensors, GAMI can
capture real time data from the ignition system, crankshaft angle, fuel flow, a large
array of temperatures (including several points around an individual cylinder), and
anything else that can be sensed.
Most amazing of all to me is that this system can
record actual instantaneous pressures within the combustion chamber at those same data
rates! GAMI accomplishes this little trick by drilling a tiny hole down inside the barrel
of the spark plug, and inserting a proprietary sensor that can measure pressure very
accurately and at very high sample rates, sufficient to record every detail of the
combustion event in real time.
For the first time, we can have a look right inside
the very heart of an operating engine, and watch and record what happens when we change
The lowermost (blue) line is the result of simply spinning the engine at 2,700 RPM with
no combustion going on at all. As you might expect, the pressure rises and falls directly
with the piston travel, reaching a maximum at TDC. It is perfectly symmetrical on both
sides of TDC, and rises only to about 350 PSI at TDC.
The next line up (green) is a normal combustion event. Notice the pressure rises almost
identically with the blue line, even after the spark, until the point at which the rise in
the blue line starts to level off. It is at this point that the "fire" has truly
lit off, and begins to increase the pressure on its own. This one peaks at about 18°
after TDC (the "PPP" or "Peak Pressure Pulse") at about 800 PSI, after
which the pressure drops off gradually, but still producing a lot of downwards force on
Finally, the yellow line shows what detonation looks like. This is an abnormal
condition. Note this is "mild detonation," not really "the real
thing" that can literally reduce an engine to an expensive pile of junk in a matter
of seconds. It was deliberately induced by redline CHT and excessive MP (from a
turbocharger). Note very carefully how early this builds and peaks, relative to a
normal event. The actual raw data shows it occurring at about 8° after TDC, and the test
engine did not sound like a happy camper! I've heard it, and it was ugly!
But let us get away from the unpleasantness of detonation, and look at a much more
interesting plot of a power pulse, at a fairly high power setting (80%):
Rich of Peak (click for larger image)
Lean of Peak (click for larger image)
Comparison: Rich of Peak vs. Lean of Peak
Those two individual charts are pretty self-explanatory, thanks to the efforts of
George Braly of GAMI, who prepared them for me. The one on the left does NOT represent a
"desirable" power setting. The RPM and the mixture are such that the peak
pressure occurs only 10.8° after TDC, and this will produce very high CHTs.
The one on the right is far better, even though the MP is much higher! The peak
pressure is out at 16.2° after TDC. Fuel consumption is way down, and so is the CHT.
The third plot simply overlays the previous two. Same day, same engine, same flight,
measurements taken within moments of each other. Both are at 244 horsepower (81%!), both
at 2500 RPM, both show the same cylinder, on a turbonormalized TCM IO-550.
How can we tell that the actual power developed is the same for the two traces? Well,
as a rough check, the airspeed produced was identical. But using numerical integration,
the area beneath each trace can be calculated, and since the area beneath the pink trace
is the same as the area beneath the blue trace, we know the power is the same.
Additionally, by knowing the pressure, the RPM, and other factors, the horsepower can be
calculated quite accurately.
In effect, what happens is a longer, slower, more gentle, and later
"push." This shifts the mechanical advantage to a slightly better position,
where a small change in angles makes a huge difference in effect.
Which combination is "better" to produce 244 HP? Well, the blue trace has a
much higher manifold pressure, but CHT is about 35° F cooler. With cooler CHTs and lower
peak pressure in the cylinder, which do you think is better?
CHT can be measured by a thermocouple washer under a spark plug, or by a probe screwed
into a threaded boss in the cylinder head casting. The latter is probably more accurate.
But there are wide temperature variations at different points around the circumference of
the cylinder barrel, with some poorly-baffled cylinders showing up to 150° F difference
between the hottest and coolest points! Poor baffling will also show up in large
variations between cylinders.
But we've got to start somewhere, and again, the old manuals reflect a great deal of
This chart from the Pratt & Whitney "The Aircraft Engine" shows what
happens to aluminum alloy used in the cylinder heads and pistons of our engines. This is a
scary chart, because it's obvious that even at normal operating temperatures, we've
already given up a substantial amount of strength. The redline CHT on my IO-550 is 460°
F, well out in the "short period of time" area. I would prefer to stay out of
that region entirely, and looking at the sharp gain in strength going from 450° F to
392° F (200° C), I think the conservative pilot ought to limit CHT to that 200° C
value, as much as possible.
There is some support for this. The P&W book goes on to say:
|"The higher limiting temperature (500° F) is for a restricted
period of time, and is confined to take-off, to maximum performance in climb and level
flight, and emergencies. The temperature limit for restricted operations should,
therefore, be used for the shortest possible time only, and must never be exceeded.
lower limiting temperature (450° F) is the maximum for continuous operation. It should
never be exceeded except under the restricted operating conditions mentioned in the
previous paragraph. It is sound practice to hold the cylinder head temperature 50° F
(30° C) below this limit to keep the cylinder head materials at high operating
strength." [emphasis mine.]
That puts us squarely at 400° F, a nice, easy-to-remember number.
There is more. GAMI has cemented thermocouples down in between the fins of a cylinder,
tight against the barrel at the bottom of the grooves. While flying this at various
temperatures, it was obvious that there is a variation around the circumference, even on a
properly baffled and cowled engine. Furthermore, upon getting up around 420°> F (at
the probe), the CHT tends to become unstable, and tries to increase all out of proportion
to whatever is going on. It seems pretty clear that at higher temperatures, the cylinder
barrel goes significantly out-of-round, and since the piston can't change shape to fit,
the piston starts scuffing the narrow part of the resulting oval, leading to the rapid
rise in CHT. I have tried this on my engine, and the same "thermal runaway"
seems to occur. I stopped it long before reaching much over 440° F, so I don't know how
high it will go, nor do I wish to find out. By the way, the standard factory CHT
instrument didn't show anything abnormal at all!
Personally, I have my JPI set to warn me if any cylinder goes over 400° F, and I try
to maintain 380° F as a maximum to provide a margin. TCM suggests limiting normal cruise
temperatures to 380° F in one publication, but then in another they suggest 420° F. Go
figure. I'll take the lower value.
Let's re-visit that TCM chart of basic engine curves, this time with a red area to
correspond to the above:
Remember that this is the chart of operating parameters at 25" and 2,500 RPM. Does
that setting sound somehow familiar? Yes, it's the setting many have used for years right
after takeoff, for climb power! The high temperatures are the direct result of pulling the
MP back to 25", which cuts out the power enrichment feature of the fuel controller,
leaning the engine dramatically!
This practice (pulling the throttle back after takeoff) may be the single most damaging
thing many people do with the best of intentions, to "make it easier on the
engine!" Forget it, folks. Leave that throttle fully in, unless you need to make a
substantial reduction in MP, maybe to 22", or so. (Remember, we're talking about
normally-aspirated engines here.)
Let's take a little different look at those TCM curves:
The top picture is the same one we just looked at. I've cut out a lot of extraneous
detail to illustrate my point. If we consider that area of CHT "off limits"
because it's over 400° F, then the same area of EGT is also "off limits"
because they go together. In this illustration, note there is no possible combination that
will give us what we want, except very lean of peak, which would cost us a lot of power.
In the second picture, I've fiddled the CHT numbers, and erased the EGT numbers, to
give a simple picture of some "Less Power." It's probably up in the 70% range,
but that's not what I'm trying to show. Look at the much-narrower red band covering the
peak CHT (be very careful to read "CHT" and "EGT" correctly, here in
this text, and keep them straight while looking at the picture.) Now run up to the
equivalent range on the EGT, and note where it lies on the curve? At this still-high power
setting, peak EGT produces a satisfactory CHT! From this we should realize that "The
Danger Zone" on the EGT is mostly on the rich side of peak precisely where
many factory documents would have us run. At higher power settings, we need to avoid peak
CHT, which means avoiding some area rich of peak EGT.
Remember I talked about six (or four) cylinders, flying along in loose formation, all
at different power settings? Now you may be getting the idea why I think that's important.
No matter where you set your mixture on such a beast, most of the cylinders are not
running where you think you set them! You have set one cylinder, and one only.
Now suppose you lean by the classic advice "lean 'till roughness occurs, then
enrich just enough to restore smoothness." No one wants to run a rough engine, so
this is good advice. A rough engine causes metal fatigue, pilot fatigue, sterility,
, but, I digress. I think we can all agree that vibration is a bad
thing, all around. What's causing that vibration? Aha, I see that hand in back there in
the audience. What's that you say? "Lean misfire?"
Sorry Charlie, no tuna. There's essentially no such thing as "lean misfire."
It's probably a term some tech rep made up because he didn't know the right answer. A
properly set up engine will tolerate leaning and remain smooth right down to that 30%
power range (see combustion chart), at which point it just quits cold. There's no reason
to shake, at all. Now that said, the real world is not perfect, and even well-set-up
engines will show a just a tiny bit of roughness when leaned to the extreme.
What does happen to cause that roughness is that the first cylinder to peak and
start down on the lean side will produce less power than the others, and unequal
power from one cylinder (or more) will cause enough vibration to be obvious. So you
enrich until the vibration goes away, restoring that one cylinder (or more) to
approximately the same actual power as the others. That gets them all up on the "sort
of flat" part of the power curve (see chart). There's no way of telling just where
all that occurred, or what cylinder it was, but the resulting chart might look something
like this, with a new red area added.
This second and much more serious red area holds true through the entire spectrum of
power settings, so it is much more serious. Virtually all factory big bore engines suffer
from this uneven power distribution, which sets an artificial limit on just how lean we
can run. Uneven mixture distribution causes the entire lean-of-peak-EGT region to
become a red zone, not available for use!
From this comes a few pernicious OWTs, all with a modicum of truth.
"Never run lean of peak!" That's right, you can't in most flat engines,
because their uneven mixture distribution causes them to run too rough.
"Leaner is hotter!" That's true only up to the point of maximum CHT, which
occurs at around 35° F to 50° F ROP for most engines. Leaning beyond that point makes
'em run cooler. Naturally, if your engine gets the shakes at lean mixtures because of poor
mixture distribution and the resulting uneven cylinder-to-cylinder power, then the only
leaning range left to you is on the rich side, and if limited to that area, leaner is
"Leaning too much will burn your valves!" True (at higher powers), unless you
continue leaning to the lean side of peak EGT (where leaning makes cylinder heads and
valves run cooler), or you operate at sufficiently low power settings that valve
temperatures remain acceptably cool even at peak EGT. (This works out to around 60% to 65%
of rated power, on most of the flat "big bores".)
These are the kinds of things running through factory tech reps' minds when they scream
(as a Lycoming rep did to me awhile back), "I wouldn't recommend lean-of-peak to my
worst enemy!" Neither would I, in his stock engine with its lousy mixture
There are, however, some alternatives.
First, if you're going to operate one of these expensive big-bore engines properly, you
must install an all-cylinder engine monitor, which at least tells you the CHT and
EGT in each cylinder. If I had a four-banger, I'd put one in it, too, but that's
more for troubleshooting. While I am disgusted at the stupid trademark infringement
lawsuit that the owner of J. P. Instruments (JPI) has initiated recently, I am forced to
concede that JPI makes a superior engine monitor, in my opinion. Insight also makes a good
one that will do the job. I have not yet seen the new Electronics International monitor,
shown at Sun 'n Fun this year, but it looks great on paper. Any of these
probe-per-cylinder systems with bar-graph displays will do the job.
Once you have that all-cylinder monitor, limit the hottest CHT to 400° F at all times.
If it goes over that, increase airspeed (VERY effective!), open the cowl flaps a bit (if
you have cowl flaps), or enrich the mixture if it is on the rich side (lean it more, if on
the lean side). But using extra fuel as a coolant should be your last-resort solution
after the other things have been tried and fallen short.
So far, most of this column has been discussing The Ideal Engine. Unfortunately,
that doesn't quite exist, yet, and those with carbureted engines are really left out in
the cold, except for the above two tips (engine monitor and 400° F CHT limit.)
Here's another tip for carbureted engines, if you're operating high enough to use full
throttle, or nearly so. From the full-throttle position, pull the throttle back until you
observe the slightest drop in MP perhaps a quarter-inch or less. Leave it there. That
will cock the throttle plate a little, just enough to set up a vortex that will cause
better atomization and mixing of the fuel and air. (This is counterproductive in fuel
In principle, we should all operate at the lowest possible RPM allowable for the MP,
and the following TCM chart shows why.
As you can see, the losses to friction are about 37 HP at 2,500 RPM, and about 27 HP at
2,100 RPM. That's 10 very useful HP, in my opinion.
However, this low RPM stuff must be tempered a little bit, by the fact that decreasing
RPM moves the PPP closer to TDC. Anytime we move that PPP away from that ideal 16° to
18° after TDC, we're losing power, and increasing CHT. On the other hand, the leaner we
run the engine, the more we delay the PPP, getting it further from TDC.
From this we can see that there must be a balance between slower/leaner, and
faster/richer. For high power, maximum-performance operation, you should run richer
mixtures and higher RPMs. For low power, maximum-efficiency operation, you should run
leaner mixtures and lower RPMs. It would be really nice if we could develop some sort
of "super linkage" that ties the prop control and mixture control together into
sort of a single-lever power control, but that would be a formidable design task. It
appears to me that running in accordance with the POH will provide good results in the
worst possible cases, and TCM probably felt this was their best option.
With big-bore fuel-injected engines like TCM 520s/550s and Lyc 540s, we're getting some
modern developments that can be of major benefit, and which will pay for themselves in
short order. These improvements should also allow safe and efficient operation well
outside the suggestions in the various POHs and manufacturers manuals, including much
lower RPM, higher MP, and leaner mixtures. At low altitudes, I am routinely running my
IO-550 at 2,100 RPM, full throttle, and very lean, perhaps 50° F LOP EGT. That produces
about 75% of rated power. The engine appears to love it, runs very cool, makes much less
noise, and runs very smooth. However, those settings would be a deadly combination if I
enriched the mixture, or even worse, tried running ROP. I also cannot climb at that power
setting, because the loss in airspeed causes too much increase in CHT.
Once you have the all-cylinder engine monitor installed, the next best thing you can do
for your big-bore flat six is to install GAMIjectorsTM from
General Aviation Modifications, Inc., in Ada, Oklahoma.
The usual disclaimer: I own no stock, directly or indirectly in GAMI. I wish I did.
I do not work for them. I wish I did. I do not benefit in any way from the sales of their
products, and I paid full-boat retail for my own GAMIjectorsTM.
The owners have become personal friends, and are men that I admire greatly. I have been
very distantly involved with them in some very minor testing and comment.
GAMIjectorsTM are custom injectors that match the fuel
flows to the air flows in all cylinders. With these, you can quite easily lean your engine
right down to starvation levels without roughness. This means you cannot use the old trick
of "lean 'till rough, enrich 'till smooth" because the engine never gets rough
at any mixture setting. Your engine will run cleaner, cooler, and smoother, and you will
be able to use the full range of mixtures, just as the operators of the big old radials
did for several hundred million hours in a bygone era. Oh, by the way, there is no
evidence whatsoever to support the OWT that lean mixtures cause corrosion in exhaust
When you lean an engine with GAMIjectorsTM , you will
see all EGTs rise at the same time. (The absolute temperatures may be different from one
cylinder to the next, but that's unimportant.) All should peak at the same time, and all
should fall at the same time. This will produce results as in the following chart:
By this simple, one-hour installation, we bring our current engines up to very nearly
the standards of "The Ideal Engine" I have discussed at length above.
Going well beyond that, GAMI is currently deep in R&D running test engines.
This effort promises to give us all a better ignition system. No, not the junky
current "state of the art" automotive style electronic ignition systems for our
aircraft, but a simple, safe, certified system that will leapfrog all existing
technology. For the first time, there will be a system that fully controls what is
happening inside the combustion chamber.
I haven't seen this experimental system run yet, but George and Tim at GAMI have
invited me to come see it, and have a little Oklahoma BBQ, too. There are rumors that it
may even cure/prevent baldness, loss of memory, cancer, and the common cold!
Be careful up there!