
110i R2 / 110i R2 CS Engine Manual
provides
the maximum
cooling
for
an
air
cooled engine. Without
ba
f
fling
(meaning wood
or
composite dampers
that direct
the
airflow)
the
air
will
t
ake
the
p
ath
of
least
resis
t
ance. Some
incoming air
will
bounce
o
ff
the cylinder(s) and the
rest
will
escape
around the cylinder(s)
without
coming
into
con
t
act
with
the cylinder(s).
Engine in pusher operation:
Impor
t
ant
note!
When
engines
are
used operating
in
pusher
configuration cooling
ge
ts critical
and
special
attention
has
to
be
given
to
an
e
f
fective
cooling
method. A
good cooling
system
layout
depends
on
the actual
location (position)
of
the engine
in
the fuselage.
Operating temperature
To be able to check the cylinder head temperature ( CHT ) a thermo element has to be installed which fits
under the spark plug ( M 10 thread ). Optimum operating temperature range : 180°C - 220°C. In this range
piston, spark plug and combustion chamber will be free of remains. Maximum temperature of 270°C should
not be exceeded. During a certain time at full speed the temperature could be 250°C.
Colour of the spark plug should be : light or middle brown. A grey / gray colour is a typical sign for over
heating. Temperatures above 270°C are critical and over 300°C, piston can seize and could completely
damage the engine.
Temperatures below 180°C create remains ( carbon ) on the piston crown. Increasing remains hit the cylinder
and cause abnormal running noises ( knocking ) which will increase the load of the needle bearings and can
destroy them. Under extreme conditions the crankshaft can break and a complete damage of the engine will
be the result.
Rear induction
Carburetors, whether
front or
rea
r, require
a
steady
supply
of
fresh
air.
The
best
way
to
supply
air
to
a
rear
carburetor
is
by
ins
t
alling
an
air
scoop.
Some have
thought
to
drill
holes
into
the
fuselage
near
the carburetor
area
rather than creating
an
air scoop
for
the carburetor. This does
not
work,
it
fact
it
will
create
a
vacuum
e
f
fect that
will
draw the
air
away
from
the
carburetor!
Again,
you should
ins
t
all
an
air scoop
into
the
front of
the plane
which
will
supply air
into
the fuselage.
This
air
will
then
need
to flow
out
of
the fuselage.
Drill
exit
holes
into
the
rear
area
of
the fuselage
for this
purpose. Impor
t
ant:
The
interior of
the fuselage
must
be sealed
to
prevent
damage
from
gasoline
that
sprays
from
the carburetor.
Use
a
thin
epoxy
or
other appropriate
fuel proofing
method.
Do
not overlook
this
step
as
gasoline
will
melt some materials
like
S
tyrofoam
very
quickl
y.
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