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Mixture Control

in Aircraft Systems

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Carburetors are normally calibrated at sea-level pressure, where the correct fuel-to-air mixture ratio is established with the mixture control set in the FULL RICH position. However, as altitude increases, the density of air entering the carburetor decreases, while the density of the fuel remains the same. This creates a progressively richer mixture, which can result in engine roughness and an appreciable loss of power. The roughness normally is due to spark plug fouling from excessive carbon buildup on the plugs. Carbon buildup occurs because the rich mixture lowers the temperature inside the cylinder, inhibiting complete combustion of the fuel. This condition may occur during the pretakeoff runup at high-elevation airports and during climbs or cruise flight at high altitudes. To maintain the correct fuel/air mixture, the mixture must be leaned using the mixture control. Leaning the mixture decreases fuel flow, which compensates for the decreased air density at high altitude.

During a descent from high altitude, the mixture must be enriched, or it may become too lean. An overly lean mixture causes detonation, which may result in rough engine operation, overheating, and a loss of power. The best way to maintain the proper mixture is to monitor the engine temperature and enrich the mixture as needed. Proper mixture control and better fuel economy for fuel-injected engines can be achieved by use of an exhaust gas temperature (EGT) gauge. Since the process of adjusting the mixture can vary from one aircraft to another, it is important to refer to the airplane flight manual (AFM) or the pilot’s operating handbook (POH) to determine the specific procedures for a given aircraft.


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{ 1 comment }

1 Günter Green October 26, 2011 at 10:49 am

Are you sure that the fuel flow from a float type carburettor remains the same with decreasing air density? Consider the fact that fuel is pulled upwards by the Venturi effect which is proportional to air density also. This would decrease the fuel flow in proportion to the air flow and thus contribute to keeping the air to fuel ratio constant.

(There are additional influences like the force to lift the fuel from the bowl level to the nozzle level and the force to accelerate the fuel from zero to the flow speed in the nozzle pipe.
We could discuss those later.)

I would like to read your comment.

Günter
26-Oct-2011