MechDesignR
New member
- Feb 27, 2010
- 3
I am working for an aircraft company that uses “old school” undimensioned drawings to define brake formed sheet metal parts (the same way things have been done for many decades). These undimensioned drawings go by different names at different companies: PCM, EMD, Mylar, Undimensioned Master, etc. Typically, these “undimensioned” drawings define a flat pattern, show bend centerlines, specify bend angle, direction and radius. They only contain dimensions for features that need to be held tighter than the general tolerance of +/- .030”. For example, full size fastener holes would have a diameter dimension. Please only reply if you are very familar with this type of drawing.
Where I currently work, undimensioned drawings have a general tolerance of +/- .030” with a note that states “no tolerance accumulation is implied in any series of features”. Some people understand this to mean that the length of the part (scaled off of the mylar or measured in cad) would have a tolerance of +/- .030” and similarly, the distance between the centers of two holes would be +/- .030”. Other people interpret this to mean that one edge of the part is held to +/- .030” and that the location of a hole is held to +/- .030” and that the length of the part would have a total tolerance of +/- .060” and similarly, the distance between the centers of two holes would be +/- .060”. The correct interpretation is important since I am designing new sheet metal parts that will mate with purchased parts (things can’t be drilled at instl) – I have to ensure interchangeability by calculating the tolerance needed for my hole pattern. Sometimes a general tolerance of +/- .030 will work for the hole pattern (due to floating nutplates and large holes) and no dimensions are needed. While other times a tighter tolerance is required.
Apparently, the interpretation of undimensioned drawing tolerances varies from company to company. I would like to hear what other people in Aerospace have to say – what is your understanding of the general tolerances on undimensioned parts? What statement is used on the drawing or elsewhere to clarify things? Obviously, GD&T could be used to express exactly what is needed, but that is not an option.
Thanks!
Where I currently work, undimensioned drawings have a general tolerance of +/- .030” with a note that states “no tolerance accumulation is implied in any series of features”. Some people understand this to mean that the length of the part (scaled off of the mylar or measured in cad) would have a tolerance of +/- .030” and similarly, the distance between the centers of two holes would be +/- .030”. Other people interpret this to mean that one edge of the part is held to +/- .030” and that the location of a hole is held to +/- .030” and that the length of the part would have a total tolerance of +/- .060” and similarly, the distance between the centers of two holes would be +/- .060”. The correct interpretation is important since I am designing new sheet metal parts that will mate with purchased parts (things can’t be drilled at instl) – I have to ensure interchangeability by calculating the tolerance needed for my hole pattern. Sometimes a general tolerance of +/- .030 will work for the hole pattern (due to floating nutplates and large holes) and no dimensions are needed. While other times a tighter tolerance is required.
Apparently, the interpretation of undimensioned drawing tolerances varies from company to company. I would like to hear what other people in Aerospace have to say – what is your understanding of the general tolerances on undimensioned parts? What statement is used on the drawing or elsewhere to clarify things? Obviously, GD&T could be used to express exactly what is needed, but that is not an option.
Thanks!