Brett, can you post a simple line drawing showing a centering B/C & lead out configuration & a non centering or unstable example?
Thanks, Gil
Top is my bellcrank, with my leadout convergence angle. The line perpendicular to each leadout passes through the pivot at neutral.
Second is a "straight" bellcrank, note the line normal to the leadouts passes behind the pivot, which means it is unstable and wants to move away from neutral.
Third is a bellcrank with an exaggerated inboard sweep, it self-centers (as the designers intended, but I discourage (because of Case 4, among other reasons). This is a less-extreme version of the SIG self-centering bellcrank.
Fourth is a "neutral" bellcrank (same as the first) with the bellcrank mounted right in line with the centerline of the airplane with the flap presumably at neutral. It wants to always give you "down" elevator. You are going to end up with the leadouts about 1.5-2.5 degrees aft of the CG.
Interestingly, this is a case where moving the pivot (and blindly lining up the bellcrank on the centerline) actually does have an effect - but everybody knows not to line it up on the centerline at this point, no matter which way you set up your bellcrank (stable, neutral, or, for most people using pre-made bellcranks, unstable). In this case, since the key alignment of the leadouts is the CG, not the pivot, you will get better geometry for the "centerline" alignment of the bellcrank if you move the pivot well behind the CG. Of course that makes the errors and varying angles in the flap pushrod much messier, so you can't make a blanket statement about it. Moving it forward and leaving it aligned with the centerline exaggerates the scenario in the last drawing. It's drawn about how most people did it before the 90's and before anyone ever thought it through carefully (and is actually on the Infinity CAD plans that way because I lost my interest in publishing it, I never tried to fix it).
Brett
p.s. BTW, I will freely admit that I hadn't realized that Case 2 ("straight" bellcrank) was unstable until maybe 2003 - while analyzing someone else's SSW post. I and many others had realized that Case 4 provided a torque bias a long time ago. I think both were missed in Larry Cunningham and John Miller's seminal work on control geometry in SN. And people say we never learn anything new, it wasn't long ago that we habitually used Top Flite 3" bellcranks and bent wire pushrods, and just lived with what we got.