Hu's posts on any subject tend to cause a person to think. (good)
But maybe the direction this recent discourse sends my mind is a little risky.
Has anyone actually tried a rubber ferule? something stiffer than 90 Duro A, of course. I do mean experimental, just to see what happens.
Seems like designed right it would spin like crazy. (longer contact period) Maybe a rubber plug embedded in that aluminum thin-wall ferule?
6061 T6 is about the most common aluminum alloy out there. Cheap, strong, easy machining, relatively (that is "relatively") corrosion resistant though not as good as the lower alloys like the 5xxx series. 7075 - hmmmm, probably not a factor but intergranular corrosion just form sitting around in humid air unprotected is an ugly thing. My impression is that It is used less in GA aircraft structure than at first simply because of the protection requirments and potential maintenance issues. Sort of like (true) magnesium wheels. Ideal on a performance/competition basis at one time, costly and risky to maintain in "real life".
smt
But maybe the direction this recent discourse sends my mind is a little risky.
Has anyone actually tried a rubber ferule? something stiffer than 90 Duro A, of course. I do mean experimental, just to see what happens.
Seems like designed right it would spin like crazy. (longer contact period) Maybe a rubber plug embedded in that aluminum thin-wall ferule?
6061 T6 is about the most common aluminum alloy out there. Cheap, strong, easy machining, relatively (that is "relatively") corrosion resistant though not as good as the lower alloys like the 5xxx series. 7075 - hmmmm, probably not a factor but intergranular corrosion just form sitting around in humid air unprotected is an ugly thing. My impression is that It is used less in GA aircraft structure than at first simply because of the protection requirments and potential maintenance issues. Sort of like (true) magnesium wheels. Ideal on a performance/competition basis at one time, costly and risky to maintain in "real life".
smt