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From: "Frederick Moreno" <frederickmoreno@bigpond.com>
To: "Lancair Mail (lml@lancaironline.net)" <lml@lancaironline.net>
Subject: EGT/TIT Calibration - the MYTH


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Forget calibration.  It is a waste of time.  All you will EVER get in the
cockpit is relative temperature indications: when the exhaust gases are
(probably) hotter or (probably) cooler.  That is ALL the EGT/TIT number
tells you.  The absolute value of the numbers means not much.  The number=
s
are for comparison purposes only.=0D
=0D
Measuring gas temperature in the exhaust pipe of a piston engine is very
tough stuff if you want to really know the exact answer.  Reason?  There =
are
many confusing effects, and the temperature and flow are constantly chang=
ing
  See attached picture for a bit more understanding if you want to wade i=
nto
some of the details.  =0D
=0D
The temperature displayed by the instrument is the temperature read by th=
e
thermocouple which is buried inside a probe which is sheathed with a
stainless skin and filled with some kind of ceramic insulator.  These
combine to yield a very slow response time, much slower than the cycle ti=
me
of the engine (40 times per second at 2400 RPM).  So the thermocouple is
time-averaging the temperature in the vicinity where the thermocouple is
located. =0D
=0D
I found that the EGT SYSTEM (thermocouple plus sheath plus surrounding
thermal mass of exhaust pipe and cylinder head) take sabout three minutes=
 to
come to full equilibrium.  =0D
=0D
Don't believe me?  =0D
=0D
Do GAMI lean test.  Start rich, Lean down in steps waiting, say, one minu=
te
per step while you record data.  Then reverse, going from lean back riche=
r.=20
Then plot the data.  The curve going leaner will not lie on top of the cu=
rve
going richer.  Why? Because when you took the reading, it was still chang=
ing
 slowly, but still changing.  It takes a lot of time and patience to get
good data.  =0D
=0D
But drawing the curve has value because it shows which cylinder goes lean
first, second, and so forth.  But the absolute numbers are subject to hug=
e
errors as noted below.  =0D
=0D
The instrument temperature reading is related to the gas temperature in t=
he
same way that a stopped clock is accurate twice a day.  That is, the EGT
reading is only accurate when the GAS temperature is rising through the
reading, or falling through the reading, which may occur once or more eac=
h
cycle.  =0D
=0D
Look at the figure.  The exhaust event lasts about 180 degrees out of a
total 720 degrees required to complete the four stroke cycle.  So you get
WHOOSH for about a quarter of the time, and then nothing except some ring=
ing
of the exhaust gas column back and forth as the pressure pulse oscillates=
 up
and down the exhaust pipe.  There is nothing like "steady state" (smooth =
and
unchanging) occurring in the exhaust flow. =0D
=0D
Similarly, there is nothing like steady state about exhaust gas temperatu=
re.
 When the exhaust valve opens, the temperature of the escaping gases is
highest, but falls as gas expansion occurs in the cylinder as the gas exi=
ts
the cylinder. So the temperature starts out high, and ends up lower at th=
e
end of the exhaust pulse. =0D
=0D
So both flow and temperature are constantly changing, but flow is nearly
zilch about 3/4 of the time.  =0D
=0D
Now the poor thermocouple is shielded from all this variability by the
stainless steel sheath.  The sheath is heated by convection (passage of
gases), and heated by thermal radiation from anything hotter than the she=
ath
(portions of exhaust pipe, or exhaust valve perhaps?).  And the sheath lo=
ses
heat to the surroundings via radiation going to any surface that is coole=
r
than the sheath (some portion of exhaust manifold pipe probably, certainl=
y
the aluminum exhaust port in the head).  =0D
=0D
And the sheath is also losing heat to the outside via conduction to the
cooler exterior. =0D
=0D
So the sheath is arriving at some time-averaged temperature that is proba=
bly
close to the thermocouple temperature, but which is influenced by a heat
balance of gain and loss between gas, conduction, and thermal radiation w=
ith
the surroundings.  And the gas is active only 1/4 of the time, and the fl=
ow
rate and temperature of the gas are changing during this short interval. =
=0D
=0D
Getting the picture?  The thermocouple is related to the gas temperature,
but is delivering a signal to the instrument that is averaging out all th=
ese
variations in time and thermal balance heat flows.  =0D
=0D
In short, we do not really know what the gas temperature is.  We only hav=
e a
number that kinda sorta represents some sort of average of gas temperatur=
e
and flow, installation geometry, and ambient environment under the cowl
(cooling air blowing on exhaust pipes and thermocouples, radiation
environment inside and outside of exhaust pipe, conduction losses and on =
and
on). =0D
=0D
The number in the cockpit is only valid for comparison with other numbers
obtained during other power and mixture settings and flight conditions. =0D
=0D
Some observations can follow from considering the figure and discussion
above, such as:=0D
Installation details count a lot.  The depth of the thermocouple,
thermocouple construction details, thermocouple mounting details, locatio=
n
in the exhaust pipe, distance from the cooler aluminum exhaust port,
nearness to a bend in the pipe, effect of the cooling air blast coming of=
f
the cylinders onto the exhaust pipe - all these things and more will affe=
ct
the "EGT/TIT reading" up or down independent of the "real" gas temperatur=
e
(which is constantly changing each cycle).  This is why you get a differe=
nt
number in the airplane as opposed to on a dyno stand at ground level.  =0D
The TIT will read higher than EGT of a single cylinder.  Why? The EGT get=
s
gas blasted about 1/4 of the time, but the TIT theremocouple on a twin tu=
rbo
6 cylinder engine gets blasted 3/4's of the time.  Any surprise it reads
hotter?  For this reason, the exhaust pipe is also a bit hotter at the tu=
rbo
inlet than below an individual cylinder.=0D
If you wrap your exhaust pipes, the pipe wall will be hotter and will aff=
ect
the radiant exchange and thermal losses raising the apparent gas temperat=
ure
- probably quite a bit- as well as raising the actual gas temperatures in
the pipe, at least near the pipe wall (in the thermal boundary layer).=0D
For all these reasons, EGT spread normally means little unless one readin=
g
is WAY off the program in which case it does mean something (blocked
injector, fouled spark plug, etc).  But the value of EGT/TIT is the TREND
and THE COMPARISON to other operating conditions.=0D
=0D
What about TIT limits, typically 1650F or sometimes 1750F?  The TIT is th=
e
best data we have, and if the turbo guys say we can expect trouble sooner=
 or
later if these temperatures are exceeded, it is based on experience and s=
ome
safety factor using the best data available to the pilot.  Respect these
limits.  Inaccurate data is better than no data in such circumstances.=0D
=0D
But don't worry about absolute values or calibration.  They are meaningle=
ss
values and exercises.  Watch the trend and comparison with other operatin=
g
conditions.  Those tell the important tales we need to know and understan=
d. =0D
=0D
Fred Moreno
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<DIV style=3D"PADDING-LEFT: 80px" id=3DINCREDI_TEXT_AREA>
<DIV>Forget calibration.&nbsp; It is a waste of time.&nbsp; All you will =
EVER get in the cockpit is relative temperature indications: when the exh=
aust gases are (probably) hotter or (probably) cooler.&nbsp; That is ALL =
the EGT/TIT number tells you.&nbsp; The absolute value of the numbers mea=
ns not much.&nbsp; The numbers are for comparison purposes only.</DIV>
<DIV>&nbsp;</DIV>
<DIV>Measuring gas temperature in the exhaust pipe of a piston engine is =
very tough stuff if you want to really know the exact answer.&nbsp; Reaso=
n?&nbsp; There are many confusing effects, and the temperature and flow a=
re constantly changing.&nbsp; See attached picture for a bit more underst=
anding if you want to wade into some of the details.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>The temperature displayed by the instrument is the temperature read =
by the thermocouple which is buried inside a probe which is sheathed with=
 a stainless skin and filled with some kind of ceramic insulator.&nbsp; T=
hese combine to yield a very slow response time, much slower than the cyc=
le time of the engine (40 times per second at 2400 RPM).&nbsp; So the the=
rmocouple is time-averaging the temperature in the vicinity where the the=
rmocouple is located. </DIV>
<DIV>&nbsp;</DIV>
<DIV>I found that the EGT SYSTEM (thermocouple plus sheath plus surroundi=
ng thermal mass of exhaust pipe and cylinder head) take sabout three minu=
tes to come to full equilibrium.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>Don't believe me?&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>Do GAMI lean test.&nbsp; Start rich, Lean down in steps waiting, say=
, one minute per step while you record data.&nbsp; Then reverse, going fr=
om lean back richer.&nbsp; Then plot the data.&nbsp; The curve going lean=
er will not lie on top of the curve&nbsp;going richer.&nbsp; Why? Because=
 when you took the reading, it was still changing, slowly, but still chan=
ging.&nbsp; It takes a lot of time and patience to get good data.&nbsp; <=
/DIV>
<DIV>&nbsp;</DIV>
<DIV>But drawing the curve has value because it&nbsp;shows which cylinder=
 goes&nbsp;lean first, second, and so forth.&nbsp; But the absolute numbe=
rs are subject to huge errors as noted below.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>The <U>instrument temperature reading</U> is related to the gas temp=
erature in the same way that a stopped clock is accurate twice a day.&nbs=
p; That is, the EGT reading is only accurate when the GAS temperature is =
rising through the reading, or falling through the reading, which may occ=
ur once or more each cycle.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>Look at the figure.&nbsp; The exhaust event lasts about 180 degrees =
out of a total 720 degrees required to complete the four stroke cycle.&nb=
sp; So you get WHOOSH for about a quarter of the time, and then nothing e=
xcept some ringing of the exhaust gas column back and forth as the pressu=
re pulse oscillates up and down the exhaust pipe.&nbsp; There is nothing =
like "steady state" (smooth and unchanging)&nbsp;occurring in the exhaust=
 flow. </DIV>
<DIV>&nbsp;</DIV>
<DIV>Similarly, there is nothing like steady state about exhaust gas temp=
erature.&nbsp; When the exhaust valve opens, the temperature of the escap=
ing gases is highest, but falls as gas expansion occurs in the cylinder a=
s the gas exits the cylinder.&nbsp;So the temperature starts out high, an=
d ends up lower at the end of the exhaust pulse. </DIV>
<DIV>&nbsp;</DIV>
<DIV>So both flow and temperature are constantly changing, but flow&nbsp;=
is nearly zilch about&nbsp;3/4 of the time.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>Now the poor thermocouple is shielded from all this variability by t=
he stainless steel sheath.&nbsp; The sheath is heated by convection (pass=
age of gases), and heated by thermal radiation from anything hotter than =
the sheath (portions of exhaust pipe, or exhaust valve perhaps?).&nbsp; A=
nd the sheath loses heat to the surroundings via radiation going to any s=
urface that is cooler than the sheath (some portion of exhaust manifold p=
ipe probably, certainly the aluminum exhaust port in the head).&nbsp; </D=
IV>
<DIV>&nbsp;</DIV>
<DIV>And the sheath is also losing heat to the outside via conduction to =
the cooler exterior. </DIV>
<DIV>&nbsp;</DIV>
<DIV>So the sheath is arriving at some time-averaged temperature that is =
probably close to the thermocouple temperature, but which is influenced b=
y a heat balance of gain and loss between gas, conduction, and thermal ra=
diation with the surroundings.&nbsp; And the gas is active only 1/4 of th=
e time, and the flow rate and temperature of the gas are changing during =
this short interval. </DIV>
<DIV>&nbsp;</DIV>
<DIV>Getting the picture?&nbsp; The thermocouple is related to the gas te=
mperature, but is delivering a signal to the instrument that is averaging=
 out all these variations in time and thermal balance heat flows.&nbsp; <=
/DIV>
<DIV>&nbsp;</DIV>
<DIV>In short, we do not really know what the gas temperature is.&nbsp; W=
e only have a number that kinda sorta represents some sort of average of =
gas temperature and flow, installation geometry, and ambient environment =
under the cowl (cooling air blowing on exhaust pipes and thermocouples, r=
adiation environment inside and outside of exhaust pipe, conduction losse=
s and on and on). </DIV>
<DIV>&nbsp;</DIV>
<DIV><U>The number in the cockpit is only valid for comparison with&nbsp;=
other numbers obtained during other power and mixture settings and flight=
 conditions</U>. </DIV>
<DIV>&nbsp;</DIV>
<DIV>Some observations can follow from considering the figure and discuss=
ion above, such as:</DIV>
<OL>
<LI>Installation details count a lot.&nbsp; The depth of the thermocouple=
, thermocouple construction details, thermocouple mounting details, locat=
ion in the exhaust pipe, distance from the cooler aluminum exhaust port, =
nearness to a bend in the pipe, effect of the cooling air blast coming of=
f the cylinders onto the exhaust pipe - all these things and more will af=
fect the "EGT/TIT reading" up or down independent of the "real" gas tempe=
rature (which is constantly changing each cycle).&nbsp; This is why you g=
et a different number in the airplane as opposed to on a dyno stand at gr=
ound level.&nbsp; </LI>
<LI>The TIT will read higher than EGT of a single cylinder.&nbsp; Why? Th=
e EGT gets gas blasted about 1/4 of the time, but the&nbsp;TIT theremocou=
ple&nbsp;on a twin turbo 6 cylinder engine gets blasted 3/4's of the time=
=2E&nbsp; Any surprise it reads hotter?&nbsp; For this reason, the exhaus=
t pipe is also a bit hotter at the turbo inlet than below an individual c=
ylinder.</LI>
<LI>If you wrap your exhaust pipes, the pipe wall will be hotter and will=
 affect the radiant exchange and thermal losses raising the apparent gas =
temperature - probably quite a bit- as well as raising the actual gas tem=
peratures in the pipe, at least near the pipe wall (in the thermal bounda=
ry layer).</LI></OL>
<DIV>For all these reasons, EGT spread normally means&nbsp;little unless =
one reading is WAY off the program in which case it does mean something (=
blocked injector, fouled spark plug, etc).&nbsp; But the value of EGT/TIT=
 is the TREND and THE COMPARISON to other operating conditions.</DIV>
<DIV>&nbsp;</DIV>
<DIV>What about TIT limits, typically 1650F or sometimes 1750F?&nbsp; The=
 TIT is the best data we have, and if the turbo guys say we can expect tr=
ouble sooner or later if these temperatures are exceeded, it is based on =
experience and some safety factor using the best data available to the pi=
lot.&nbsp; Respect these limits.&nbsp; Inaccurate data is better than no =
data in such circumstances.</DIV>
<DIV>&nbsp;</DIV>
<DIV>But don't worry about absolute values or calibration.&nbsp; They are=
 meaningless values and exercises.&nbsp; Watch the trend and comparison w=
ith other operating conditions.&nbsp; Those tell the important tales we n=
eed to know and understand. </DIV>
<DIV>&nbsp;</DIV>
<DIV>Fred Moreno</DIV>
<DIV>&nbsp;</DIV></DIV></TD></TR>
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