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Revision:
Date of Issue: 18. November 2011
Date of Rev.: . .
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The heat dissipation of the liquid cooling system for the cylinder heads occurs in
a aluminum gill radiator. An oil cooler for the lubrication circuit is placed below
the aluminum gill radiator. Both coolers are placed below the engine and are
supplied with ram air from the central NACA inlet between the main landing
gear legs on the bottom of the fuselage.
The ram air for cooling the cylinders is inducted through an inlet which is located
to the right of the water cooler. It then is lead through a hose and an air
distributor made of glass fiber composites (GFC) to the cylinders.
The used cooling air is discharged through two outlets. The first is an adjustable
gill outlet on the lower side of the fuselage, whereas the second is the outlet of
the exhaust gas system on top of the fuselage between the wings.
Depending on the value of the operating temperature of the engine, the position
of the gill outlet and of the cowl flaps can be adjusted with a bowden cable.
Operation of the cowl flaps:
The cowl flaps of the inlets and outlets are manually operated with a self locking
black T handle at the center console below the instrument panel.
If the handle is positioned fully forward this causes the cowl flaps to be fully
OPEN. When pulling on the handle, the flaps can be closed up to a minimum
position. To pull the cowl flap handle, it needs to be unlocked by pushing an
unlock button. Lock the cowl flap handle in the desired position by simply
releasing the unlock button.
If the engine is cold or when in the glider configuration (engine not running),
keep the inlets and outlets closed. This minimizes the warm up time for the
running engine or reduces the aerodynamic drag in the glider configuration.
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The cooling system is very powerful. Because of this, it needs to
be regulated in all phases of the flight (T/O, cruise, and others)!
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