Traditional multi-cylinder exhaust gas
and cylinder head temperature systems
that force the pilot to switch or scan
an indicator from cylinder to cylinder
in search of critical engine data, are
long obsolete. Using the latest computer
technology, the G4 presents a clear,
concise, graphic picture of all engine
temperatures simultaneously for
interpretation at a glance.
Never before
has so much engine diagnostic
information been available to the pilot
and never before, has the pilot been
able to control mixture with such ease
and precision for peak fuel efficiency.
Insight's latest G4 automatically
records flight temperature and will also
interface with other data sources and
report information to other instruments
like MFD’s. The data-log files stored on
the SD card can be easily retrieved by
the pilot, in-flight or post-flight, for
instant viewing or permanent
record-keeping.
The G4 is a sophisticated tool for
engine management. Its microprocessor
performs many tasks that used to be
handled by the pilot. One of the basic
functions performed by the G4 is
monitoring exhaust gas temperatures for
all cylinders with one degree
resolution. What is important is the
exhaust gas temperature of a particular
cylinder in relation to its peak. But
peak EGT is not a constant; it changes
with atmospheric conditions, altitude,
power setting and engine condition and
for this reason absolute exhaust gas
temperatures in degrees Fahrenheit are
quite meaningless.
The real objective of mixture management
is finding a mixture setting which
represents the correct position on the
EGT/Fuel Flow Curve. As we will see
later, this abstract task is easily
accomplished by the G3's microprocessor
which samples EGT's for all cylinders
many times a second and subjects this
data to a complex mathematical analysis
can identify peak. This capability
allows the pilot to operate his or her
aircraft engine at the most economical
mixture settings.
It is generally known that EGT can be a
valuable source of information for
engine diagnosis and troubleshooting,
but there is a great deal of confusion
when it comes to interpreting this data.
One of the basic principles of EGT
engine analysis is that engine
temperatures (EGT and CHT) achieve
equilibrium in an engine operating at a
constant power and mixture setting. What
is often overlooked is that this
equilibrium cannot be defined as a
single point but rather a range of
temperatures.
The Graphic Engine Monitor is ready
to operate the moment electrical power
is applied. Within seconds after
starting the engine, the white EGT bar
graph columns will begin to appear on
the G4 display. Each column corresponds
to the Exhaust Gas Temperature (EGT) of
a cylinder. The lowest exhaust gas
temperature that can be displayed by the
G4 is 800° F. In some engines, the
throttle will have to be opened to the
fast idle range to get an EGT indication
for all cylinders. As the cylinder heads
begin to warm up, the display will
indicate Cylinder Head Temperature (CHT)
for all cylinders as a smaller green bar
in each EGT column. A horizontal red
line across each column represents the
maximum allowable CHT. Digital numbers
below each bar graph column indicates
the exact EGT and CHT for each cylinder.
G4 Buss Voltage
The G4 Buss Voltage attempts to display
the buss voltage in green when it’s
normal and red when it’s outside of
normal. In an aircraft with a 12V
electrical system the Buss Voltage will
be annunciated in green so long as the
voltage is 12.0V to 14.9V (inclusive).
In an aircraft with a 24V electrical
system the Buss Voltage will be
annunciated in green so long as the
voltage is 24.2V to 28.7V (inclusive).
Below this range the alternator isn’t
charging the battery and above that it’s
overcharging, and the Buss Voltage will
be annunciated in red.
The instrument must be connected to the
main voltage buss (not in series with
something else, on a lighting buss, etc)
and must have a good low-resistance
ground connection, otherwise the voltage
measurement itself will be in error
causing the Buss Voltage to indicate in
red erroneously.
Controlling the G4 instrument
The instrument has two control knobs
that operate combination rotary and push
button switches. The top knob in general
controls screen selection while the
bottom knob controls items within the
given screen. Each screen assigns its
own functional needs to the controls
that may change depending on context. A
screen may also label the controls with
guidance information like “Push to
exit”.
G4 MONITORING
The Bar-Graph Display Screen
The Exhaust Gas Temperature is displayed
in white bar graph form and is
interpreted much like a conventional
mercury thermometer. The higher the bar,
the higher the temperature.
The cylinder head temperature is
displayed in green single bar format.
During normal operation it shows as a
green illuminated bar in the lower half
of the bar column. Since EGT is normally
higher than CHT, the green bar which
represents CHT is on top of the white
illuminated EGT bar and stands out
clearly. However, when the engine is
shutdown, the EGT quickly drops to zero
and the cylinders remain warm for
sometime.
The G3 provides a reliable indication of
cylinder head temperature even with the
engine shut down. Should an EGT probe
fail, the entire EGT column for that
cylinder will go blank, and the numeric
indication will show --- that is dashes,
but the CHT bar will still remain green.
The failure of one probe will not affect
the display of any other probe.
The instrument may eventually
accommodate engines with 4,6,7 or 9
cylinders in which case the appropriate
number of columns will be displayed and
numbered.
An Easy Upgrade