UGMENTALCASE
Aerospace
- Oct 10, 2011
- 123
Morning all,
I have been asked a question which got me thinking. I have attached a little sketch. So the bottom image is a plate with 2 pins, the top image is a plate with 2 holes, they fit on top of each other.
Normally we would tolerance the holes and pins with GD & T and once assembled, finish machine the dimensioned edge. But it got me thinking is there a way to figure out where the edge would end up by finish machining each part separately. So we finish machine the pins on the plate. We finish machine the holes and edge on the top plate. Once assembled the edge needs to be within the tolerance shown for example.
So to get the holes fitting, you can use the formulas for fixed/floating fasteners, depending on the finished article.
So what happens to the edge? The size difference and position tolerance would affect where the face ends up. So is there another formula or some way of working out where the edge could end up?
Thanks in advance
I have been asked a question which got me thinking. I have attached a little sketch. So the bottom image is a plate with 2 pins, the top image is a plate with 2 holes, they fit on top of each other.
Normally we would tolerance the holes and pins with GD & T and once assembled, finish machine the dimensioned edge. But it got me thinking is there a way to figure out where the edge would end up by finish machining each part separately. So we finish machine the pins on the plate. We finish machine the holes and edge on the top plate. Once assembled the edge needs to be within the tolerance shown for example.
So to get the holes fitting, you can use the formulas for fixed/floating fasteners, depending on the finished article.
So what happens to the edge? The size difference and position tolerance would affect where the face ends up. So is there another formula or some way of working out where the edge could end up?
Thanks in advance