TCM cylinder assembly design consists of a cast aluminum alloy
head and a steel barrel. Both components are designed with
cooling fins to dissipate heat as air flows around them. Cylinder
heads have been improved over the years to keep pace with engine
improvements greatly increasing cylinder service life. The
cylinder barrels have been made from aircraft quality steel
forgings for the past several decades. Initially, the finished
machined barrels were only heat treated as there was no
requirement for a case hardened bore surface in the early days of
low compression, naturally aspirated engines. However, with the
advent of turbocharging, higher compression ratios with the
associated higher operating temperatures, not forgetting the
requirement for extended TBOs Teledyne was compelled to introduce
nitrided cylinder bores.
Cylinder assemblies and their related components are subjected
to a severe operating environment. Although many operational
factors can contribute to the deterioration of a cylinder's
durability, the loads resulting from combustion pressure and
operating temperatures are the largest. The number of engine
starts, or thermal cycles is also a contributing factor.
Corrosion of the cylinder head and rusting of the cylinder barrel
can destroy the durability of a cylinder rapidly.
Over the typical range of operating temperatures, the steel
cylinder barrel is not much affected. However, the cast aluminum
cylinder head strength can be compromised if operated at maximum
temperature for unusually long periods of time. Clearly, for good
durability of cylinder assemblies, it is necessary to minimize
operation at maximum temperatures, otherwise cracking may occur.
High temperature, which increases cylinder loads, is the biggest
enemy your cylinder assembly can have. We have observed over the
years that inter-cylinder baffles and the perimeter baffles are
much neglected accessories. These items are commonly found to be
worn, missing, bent and cracked which may result in one or more
cylinders operating at unusually high temperatures. Just
remember, keeping a cool head is the key to extended cylinder
life.
The horizontally opposed engine
of today is considerably different from its predecessors. One of
the important differences is the cooling requirements of the
modern air cooled engine. As greater performance demands, mainly
more horsepower, higher efficiency and greater reliability, were
placed on the horizontally opposed engines, the requirement for
cooling could no longer be met by velocity cooling. Cowlings were
placed around the engines and baffles were installed between the
cylinders so air could be directed around the entire area of the
cylinders. Thus pressure cooling was born and the results were
superior for uniform engine cooling.
The baffling installed on the
engine of today is the result of considerable study. Special wrap
around baffles now guide the cooling air completely around the
cylinder heads and barrels. On a pressure aircooled system it is
important to understand that to control the airflow from the
propeller and ram air there has to be a pressure differential
inside the cowling. Peripheral baffles with rubber seals are
installed on the engine to provide this pressure differential. On
most installations this pressure differential is around 4 to 6
inches of water pressure.
Heat related problems have become
more prevalent with the fleet of aircraft getting older and more
power upgrades being made. Therefore, it is very important to
make sure the baffles are maintained properly.
Engine accessories consist of
components such as magnetos, alternator, starter, fuel pump, etc.
These accessories are cooled with airflow the same as the engine.
This is accomplished by direct ram air flow into the nacelle area
by air scoops and hoses routed directly to the accessory.
It is very important to make sure
the air ducts are routed and secured properly. Proper cooling of
the accessories is required to prevent failure and to get good
service life.
The advent of turbocharging has
been one of the key factors in the continual growth of general
aviation aircraft. Turbocharging provided the added edge for more
horsepower, greater altitude and increased airspeed. But, as with
the normally aspirated engine, the age old problem of heat had to
be dealt with. On turbocharged engines you now have added the
following variables which must be dealt with by proper
installation and operation:
Increased compressor temps at
altitude
Increased exhaust temps
Increased cylinder head temps
Increased temps in the cowling
The aircraft manufacturer has
provided the proper installation to assure proper cooling of the
turbo systems. It is very important that at maintenance intervals
the turbo systems be inspected and maintained so as to function
properly. You the owner/operator need to be aware of the proper
power setting and leaning procedures which will be required to
control the increased horsepower and temps.
One of your engine's worst
enemies is dirty, contaminated oil. Badly worn bearings and
excessive cylinder wear are typical examples of running with
contaminated oil. The lubricating oil in your engine has five
specific functions:
Cushion moving parts against
shock and help seal the piston rings to the cylinder wall.
Reduce friction between moving
parts.
Protect highly finished
internal parts of the engine from rust and corrosion.
Provide necessary cooling to
the internal area of the engine that cannot be reached by
external means.
Keep the interior of the engine
clean and free of sludge, dirt, varnish and other harmful
contaminants.
TCM recommends the oil be changed
as follows:
Engines that have only the oil
screen - Every 25 hours
Engines that use 4.80 high oil
filters - Every 50 hours or 6 months whichever occurs first
Engines that use 5.80 high
filters - Every 100 hours
Oil additives are not specified
or recommended by TCM. The oil companies maintain that the
necessary additives are formulated into the oil and no additional
additives are required.