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Error: Compound or pattern datum must be perpendicular to datum plane.

ninjachachi
I recently was tasked with measuring a part bent at an angle with a pattern of holes on both surfaces of the bend. The bottom plane is Datum A, the bottom pattern of holes is Datum B. There is a profile locating all of the edges on the bottom plane to Datums A|B. The top bent plane is Datum C and this angled bend is controlled with flatness and Profile to Datums A|B. Finally, on the Datum C plane, there is a set of two holes, Datum D. These 2 holes have a position callout to Datums C|B as well as just to Datum C. Everything works fine in PC-DMIS until I try and find the position of these top 2 holes. Finding their position to Datum C works just fine (as it's controlling their relation to each other and perpendicularity to the plane they're on), but when trying to calculate their position to Datums C|B I get the following error: "Compound or pattern datum must be perpendicular to datum plane."

Attached is a rough sketch of the print (everything, but hole positions and Basic dimensions were removed). I certainly get the design intention, and the GD&T kind of makes sense as well. The design intends for the top holes on Datum C to be within XXX position of the Datum B hole pattern (located on Datum A)

Am I doing something wrong? Is the GD&T wrong? If it is wrong, why is it wrong and how can it be corrected? I talked with the design engineer behind this part and they think that they GD&T is correct, so I'd definitely need a strong argument to make any sort of print change.

Sorry for the rambling, I hope it all makes sense!
Parents
  • Yet another brilliant engineering exercise that in the real world makes little sense. I got 2016 dmis cad. No fancy stuff. If I see something like this I request assembly drawing & based on that I figure things out. Often I just toss engineering datum schemes out of proverbial window after seeing assembly drawing or Pro/E assembly model & make up my own based on that. The worst problem is engineers forget you need to have 6 degrees of freedom to make sure CMM knows where part is & how it's oriented. Heck you need those in the CNC machining as well. But since their computer models look nice it's all good to them. The exceptions are cylinders like ring gauges or shafts. Anyway, 1st the 2nd hole next to D should have had CBD callout since you can see a basic dim going from D. 2nd, project circles from constructed and/or auto cylinders onto plane C. From those 2 holes have the software check their locations with respect to B. Plug the differences into the T.P equation using a calculator. Screw the datum shift. If the hole locations pass then it's all good regardless. Then report perpendicularity of those cylinders to C plane to take care of the refinement of that composite position. If the bottom part of that composite doesn't have any other datums I don't see any relations between each other.
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  • Yet another brilliant engineering exercise that in the real world makes little sense. I got 2016 dmis cad. No fancy stuff. If I see something like this I request assembly drawing & based on that I figure things out. Often I just toss engineering datum schemes out of proverbial window after seeing assembly drawing or Pro/E assembly model & make up my own based on that. The worst problem is engineers forget you need to have 6 degrees of freedom to make sure CMM knows where part is & how it's oriented. Heck you need those in the CNC machining as well. But since their computer models look nice it's all good to them. The exceptions are cylinders like ring gauges or shafts. Anyway, 1st the 2nd hole next to D should have had CBD callout since you can see a basic dim going from D. 2nd, project circles from constructed and/or auto cylinders onto plane C. From those 2 holes have the software check their locations with respect to B. Plug the differences into the T.P equation using a calculator. Screw the datum shift. If the hole locations pass then it's all good regardless. Then report perpendicularity of those cylinders to C plane to take care of the refinement of that composite position. If the bottom part of that composite doesn't have any other datums I don't see any relations between each other.
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