Inspector
Nyuck, Nyuck, Nyuck!
galvernisednuts since you don't as yet have the drill press perhaps consider getting a mill drill right off the bat. They don't take up much more room than the pillar drill and already have the X/Y table. They also have better spindle runout specs and tool holding because of the draw bar. If you can get a dovetail column rather than round column machine you can raise and lower the head without loosing registration. Round ones can swing from side to side when changing height like many drill presses. I understand the higher up front cost but they hold their value and sell for more if you ever decide to move it on.
The use of Loctite (proper bearing and bushing retaining) is widespread and good enough that all the Cessna Sovereign business jets hold the flap bushings in the titanium flap brackets (14 of) with it. They are a loose drop in fit that have to have the Loctite to stay put.
My one concern lies with the reason the plastic links were used in the first place. I wonder if it was chosen because it has enough give in it to absorb shock while still being strong? Perhaps using a stiffer material like aluminium will transfer the forces elsewhere else and cause wear there instead? Motor bearings for instance. It might have been designed as an easy to replace part rather than other more expensive and difficult to replace failing parts.
You should study Aluminium alloys and their properties before getting any to make the parts from. Some of the alloys are weaker, soft and "gummy" to machine ranging up to harder, stronger (almost as strong as mild steel) and nicer to machine. Availability and costs factor into the choices.
Best of luck with your project and keep us posted.
Pete
The use of Loctite (proper bearing and bushing retaining) is widespread and good enough that all the Cessna Sovereign business jets hold the flap bushings in the titanium flap brackets (14 of) with it. They are a loose drop in fit that have to have the Loctite to stay put.
My one concern lies with the reason the plastic links were used in the first place. I wonder if it was chosen because it has enough give in it to absorb shock while still being strong? Perhaps using a stiffer material like aluminium will transfer the forces elsewhere else and cause wear there instead? Motor bearings for instance. It might have been designed as an easy to replace part rather than other more expensive and difficult to replace failing parts.
You should study Aluminium alloys and their properties before getting any to make the parts from. Some of the alloys are weaker, soft and "gummy" to machine ranging up to harder, stronger (almost as strong as mild steel) and nicer to machine. Availability and costs factor into the choices.
Best of luck with your project and keep us posted.
Pete