jasoncwells
Aerospace
- Jun 23, 2014
- 54
Figure 4-8 in the GD&T spec shows a datum reference frame. I am aware of the two mutually perpendicular planes that exist on the axis of the part per section 4.10.3. The part that puzzles me is, how are those two planes oriented about the part axis? That is, why did the author of figure 4-8 align those planes with the holes in the part?
Perhaps the more important question, does the orientation of the u and v planes about the Z axis even matter? (On a side note, a purely cylindrical part, there would be no feature at all to control orientation of the two planes associated with datum K.)
My understanding persuades me that one of those holes has to be a datum for the orientation of the two planes of datum K to be restrained in rotation about the part axis. That's not how figure 4-8 is shown, so my understanding must not be complete.
And if you are so kind as to help me, would you please point me to the part of the spec that is pertinent? I've spent quite a bit of time studying this, and I still am not satisfied with my understanding and my command of the spec.
Thanks,
Jason C. Wells
Perhaps the more important question, does the orientation of the u and v planes about the Z axis even matter? (On a side note, a purely cylindrical part, there would be no feature at all to control orientation of the two planes associated with datum K.)
My understanding persuades me that one of those holes has to be a datum for the orientation of the two planes of datum K to be restrained in rotation about the part axis. That's not how figure 4-8 is shown, so my understanding must not be complete.
And if you are so kind as to help me, would you please point me to the part of the spec that is pertinent? I've spent quite a bit of time studying this, and I still am not satisfied with my understanding and my command of the spec.
Thanks,
Jason C. Wells