by M Lightsey » Wed Jun 19, 2013 7:47 pm
I originally had a cap that I'd brazed a forward facing vent line too. A few weeks ago, just before heading to Junction City with the plane, I decided I needed to do something with the cap. It looked kind of ratty from the brazing where it had burned off the cad plating etc. I also wasn't crazy about the looks of it. That vent tube is always in the line of sight.
Anyway, I bought a standard vented cap that fits the same filler neck. It has a tiny hole in the top, and also a notch cut out of the spring disc that lets it vent under the cap flange.
I got ready to install the new cap, but then started second guessing myself, worrying about the suction on the top of the center section. What if the new cap restricted flow, etc.
I called one of my engineering buddies and he went through the calculations. What's the wing loading, vent size, etc.
Bottom line, the amount of negative pressure on the top of the airfoil is the equivalent of lowering the center section 2 inches. The weight and head pressure of the fuel far exceeds the negative pressure of the airflow.
I installed the cap, went on my trip and it never missed a beat, even when run down to minimum reserve.
Mark
I originally had a cap that I'd brazed a forward facing vent line too. A few weeks ago, just before heading to Junction City with the plane, I decided I needed to do something with the cap. It looked kind of ratty from the brazing where it had burned off the cad plating etc. I also wasn't crazy about the looks of it. That vent tube is always in the line of sight.
Anyway, I bought a standard vented cap that fits the same filler neck. It has a tiny hole in the top, and also a notch cut out of the spring disc that lets it vent under the cap flange.
I got ready to install the new cap, but then started second guessing myself, worrying about the suction on the top of the center section. What if the new cap restricted flow, etc.
I called one of my engineering buddies and he went through the calculations. What's the wing loading, vent size, etc.
Bottom line, the amount of negative pressure on the top of the airfoil is the equivalent of lowering the center section 2 inches. The weight and head pressure of the fuel far exceeds the negative pressure of the airflow.
I installed the cap, went on my trip and it never missed a beat, even when run down to minimum reserve.
Mark