without a restriction into the bowl of the carburetor, under negative G the float goes up and the carb floods and the engine cuts.
when the float goes up in a carburetor, it shuts off the fuel flow to the float bowl in the carb., the engine cuts out because it's starved for fuel, not flooded
This stuff gets confusing, doesn't it? According to my engines instructor in mech school, who was an 8thAF mechanic in Britain, originally on the first Mustangs, then shunted off to a B17 outfit, and also worked on some American PR Spits, the float carb thing worked like this:Perhaps it is an issue of what happens to the fuel that is already in the bowl.
The pickup tube rose from near the bottom of the float bowl and exited the top before bending forward and terminating in the throat of the carburetor venturi. It was fairly large diameter with a smooth bend for minimum flow restriction, thus containing a significant volume of fuel. When negative G was applied, everything went up; fuel in the bowl (uncovering pickup tube), floats and needle valve (shutting off inflow), and all the fuel in the pickup tube squirted into the venturi in one liquid slug rather than a metered aerosol flow. So the engine was subjected to a flood followed by starvation.
So Miss Schilling's fix was to put a calibrated orifice in the venturi end of the pickup tube designed to restrict flow to the maximum the engine could ever legitimately demand. Thus under the intense pressure from a negative G bunt, the fuel would come out in an atomized spray that wouldn't exceed the engine's rich limit.
Mr. Hamm said as he shook his head and clucked his tongue he just couldn't understand why the Brits would build such an elegant airplane and then put such a rinky-dink fuel system in it. Everyone else had gone to pressure carbs or fuel injection long ago.
Cheers,
Wes
PS: How do you get Android to stop substituting smiley faces for random words? Can't make it go away.
Last edited: