Cal Haines
Diamond
- Joined
- Sep 19, 2002
- Location
- Tucson, AZ
Over in the Heavy Iron forum we are having a discussion about correcting the spindle taper on a Van Norman milling machine. My suggestion was to lap the taper using one or more piloted laps, made on a lathe by setting the compound to match the taper of a known good tool (or tools). I am NOT suggesting using an actual tool to lap the taper.
The taper in question (VN ‘C’) has an included angle of 30°15’. It’s about 3/8” long and has a keyway slot the full length and two notches for drive dogs which are about 3/16” long (see attached photo of a generic 'C' spindle). The spindle is ground oversized by maybe 0.030” for about 1-1/4” behind the taper before dropping down to a smaller diameter that registers the tool.
My idea is to use several brass laps with a 1-1/4” long pilot, sized to be a close running fit in the oversized section of the spindle. The laps would be used in rotation to clean up and true the spindle taper. The laps would be returned to the lathe for truing as needed and the spindle would be checked against the “master” tool(s) on a frequent basis. The pilots would be kept clean to avoid lapping the oversized section of the spindle bore. Perhaps an O-ring would help keep abrasive and swarf from migrating into the bore?
It has been suggested that it is impossible to clean up a taper this way:
Now mind you, the only things that I’ve lapped are the IDs of holes that I was trying to bring to a precise size, using commercial expanding brass laps, so I don’t know if what I propose will work, but I don’t see why it wouldn’t. I understand that grinding would be a better approach, but let’s ignore that for now, eh?
In my limited understanding, over time the rotating lap and the spindle will both wear (the harder spindle more so than the lap) until the surfaces conform to one another. The surfaces will be surfaces of rotation; every cross section, taken perpendicular to the common axis of the surfaces, will be circular. The surfaces will not, however, be perfectly conical. High spots on the spindle will be abraded down, but will produce a slightly depressed ring on the lap, which can, in turn create a raised ring on the spindle. Even if the spindle starts out oval in cross section, it will end up with very round cross sections. Of course, the more oval the cross section of the spindle, the more it will wear the lap out of a true cone and into something else, which is why the lap needs to be replaced or trued as necessary.
Concentricity is another matter. Over time both the spindle and the lap will develop a common center which will probably be eccentric to the true bore of the spindle to some degree. That’s where I’m hoping the long pilot will help.
In post #4 of this thread, Forrest Addy discusses lapping tapered marine propeller shafts for a permanent fit and touches on the idea of lapping spindle tapers: http://www.practicalmachinist.com/vb/general/lapping-tapers-189746/#post1206601
Here’s another post where Forrest mentions lapping spindle tapers: http://www.practicalmachinist.com/vb/general/rust-patch-spindle-taper-186514/#post1172289
In both of the above, he suggests using a brake cylinder hone, but I’m not sure I understand exactly what he has in mind or if it would work with a taper as steep as 30 degrees.
I would appreciate it very much if experts like Forrest could comment on the above and correct any misunderstandings that I have.
Cal
The taper in question (VN ‘C’) has an included angle of 30°15’. It’s about 3/8” long and has a keyway slot the full length and two notches for drive dogs which are about 3/16” long (see attached photo of a generic 'C' spindle). The spindle is ground oversized by maybe 0.030” for about 1-1/4” behind the taper before dropping down to a smaller diameter that registers the tool.
My idea is to use several brass laps with a 1-1/4” long pilot, sized to be a close running fit in the oversized section of the spindle. The laps would be used in rotation to clean up and true the spindle taper. The laps would be returned to the lathe for truing as needed and the spindle would be checked against the “master” tool(s) on a frequent basis. The pilots would be kept clean to avoid lapping the oversized section of the spindle bore. Perhaps an O-ring would help keep abrasive and swarf from migrating into the bore?
It has been suggested that it is impossible to clean up a taper this way:
...
Hand scraping a CRITICAL internal taper, is NOT how I would do it....
Lapping is also NOT going to work right... Fine for finish improvement on a straight clean taper.. not one that is off, oval, not concentric, lumpy.......
Now mind you, the only things that I’ve lapped are the IDs of holes that I was trying to bring to a precise size, using commercial expanding brass laps, so I don’t know if what I propose will work, but I don’t see why it wouldn’t. I understand that grinding would be a better approach, but let’s ignore that for now, eh?
In my limited understanding, over time the rotating lap and the spindle will both wear (the harder spindle more so than the lap) until the surfaces conform to one another. The surfaces will be surfaces of rotation; every cross section, taken perpendicular to the common axis of the surfaces, will be circular. The surfaces will not, however, be perfectly conical. High spots on the spindle will be abraded down, but will produce a slightly depressed ring on the lap, which can, in turn create a raised ring on the spindle. Even if the spindle starts out oval in cross section, it will end up with very round cross sections. Of course, the more oval the cross section of the spindle, the more it will wear the lap out of a true cone and into something else, which is why the lap needs to be replaced or trued as necessary.
Concentricity is another matter. Over time both the spindle and the lap will develop a common center which will probably be eccentric to the true bore of the spindle to some degree. That’s where I’m hoping the long pilot will help.
In post #4 of this thread, Forrest Addy discusses lapping tapered marine propeller shafts for a permanent fit and touches on the idea of lapping spindle tapers: http://www.practicalmachinist.com/vb/general/lapping-tapers-189746/#post1206601
Here’s another post where Forrest mentions lapping spindle tapers: http://www.practicalmachinist.com/vb/general/rust-patch-spindle-taper-186514/#post1172289
In both of the above, he suggests using a brake cylinder hone, but I’m not sure I understand exactly what he has in mind or if it would work with a taper as steep as 30 degrees.
I would appreciate it very much if experts like Forrest could comment on the above and correct any misunderstandings that I have.
Cal