datum system on complicated part
datum system on complicated part
(OP)
I've realized the most difficult part of applying GD&T is datum system establishment.
I'm working on a part that is huge in size and has thousands of features on it. It is an air flow inlet part. The part has outer housing and inner housing. The air flows between outer housing and inner housing. The part assembles with a cylinder to its right, a bearing inside the inner housing. There are two Supports to support the part. A rotor shaft goes in bearing and on the part there are 3 grooves for 3 rings which are coaxial with rotor shaft. Detailed description please see attached sketch.
Currently in our drawing there are just 2 datum features are specified which are horizontal and vertical flange. I think there is room to improve the existing datum system of the part.
Comments, suggestions, ideas are appreciated.
I'm working on a part that is huge in size and has thousands of features on it. It is an air flow inlet part. The part has outer housing and inner housing. The air flows between outer housing and inner housing. The part assembles with a cylinder to its right, a bearing inside the inner housing. There are two Supports to support the part. A rotor shaft goes in bearing and on the part there are 3 grooves for 3 rings which are coaxial with rotor shaft. Detailed description please see attached sketch.
Currently in our drawing there are just 2 datum features are specified which are horizontal and vertical flange. I think there is room to improve the existing datum system of the part.
Comments, suggestions, ideas are appreciated.





RE: datum system on complicated part
RE: datum system on complicated part
You are the only one who knows how the part works.
You are the one who (possibly) knows how the part will be manufactured.
You are the one to decide how many datums to have. Sometimes it may be possible to produce good part based on general tolerances all alone.
Sorry. Still feel like Monday.
RE: datum system on complicated part
It is not that your question is not interesting - it is simply too general. I am pretty sure that most of us here would really like to help you, as this is real-world application, however without knowing more it is really difficult, if possible, to provide any useful info.
I personally think your assembly needs a datum axis established from one of cylindrical features, but that is all I am able to help at the moment.
RE: datum system on complicated part
Frank
RE: datum system on complicated part
For this part, I don't know how to bring very detailed description up to you guys. I thought it may not be necessary for datum system. Maybe later during the weekend I can work on the sketch to explain more. But let me try to start with this: there are two things that puzzle me the most right now.
1. I totally agree with pmac that a datum axis is needed. But, when using a diameter to establish a datum axis, a rule of thumb is its length should be sufficient to establish a repeatable relationship with gage. In my case there are 4 cylinder features are used to mate with or hold another part. I put the diameters of these 4 features in view A in the sketch of my original post. The problem is all of them are very short in axial direction (compared with diameters). So I'm not sure if the rule is valid in this case.
2. The part assembles with following parts:
-- A cylinder
-- 3 rings
-- A bearing
-- 2 Supports symmetrically
I was wondering if an individual datum reference frame is needed for each assembly process. If it is, then it would end up with 1+3+1+1=6 datum reference frames. CheckerHater says, it's all up to me. Is this why people say applying gd&t is art instead of engineering? I still think there is one approach works best for function, maybe another one for measurement, another for manufacturing.
Sorry for providing you very less details and asking for valuable help.
RE: datum system on complicated part
Some say your GD&T should represent the function of the part.
Some say it should represent machining and related fixturing.
Some say it should represent quality control procedure.
It looks like in reality it should be meaningful compromise between all three; and that where it becomes art.
Say, your part may have five different interfaces for assembling with other components, and every interface may have each own datum(s); it is not technically wrong.
On the other hand, if all five can be machined from one single fixturing; it makes sense to have only one datum framework to represent that fixturing and dimension everything in relation to that framework.
This is why we are so curious about details.
RE: datum system on complicated part
The part function requires the 2 X ø18 holes have 0 offset to the BRG CENTERPLANE established by the 8 X ø6 holes. See section A. I'm not sure how to reflect this design requirement by any callout. Any ideas?
Thanks.
RE: datum system on complicated part
1) Re the surface that you show as Datum-A in the first drawing and Datum-B in the second drawing. Is this the surface that intimately mates with the mating part, or is it the recessed surface? I suspect it should be the recessed face because it would prevent turbulence caused by air hitting the edge of the gap that would otherwise be there.
2) I suspect that the recessed face that I mention in (1), above, should be the primary datum feature because it is more critical to the alignment of the compressor shaft than the mating faces of the two cast intake-bell halves.
3) The bearing; conical thrust or regular cylindrical mount? It is drawn as a regular cylindrical mount with a conical seat, hence the question. The difference is important because if that conical taper is functional and therefore adequately controlled, it could work effectively with other datum features to establish a datum axis via multiple datum features.
Even if it is a semi-cylindrical seat (per cast half), it can still be used with other semi-cylindrical grooves to establish a datum axis via multiple datum features.
4) The axis of the compressor shaft should establish the relationship of the mating split-faces of the bell halves. This would make the axis the second datum, based on functionality.
5) The mating split-faces of the bell halves would effectively eliminate the final dof; rotation about the datum axis (compressor shaft axis).
Jim Sykes, P.Eng, GDTP-S
Profile Services www.profileservices.ca
TecEase, Inc. www.tec-ease.com
RE: datum system on complicated part
Jim Sykes, P.Eng, GDTP-S
Profile Services www.profileservices.ca
TecEase, Inc. www.tec-ease.com
RE: datum system on complicated part
It is the datum B surface makes the main contact with a mating part. A gap exists between the recessed face and boss face of mating part. There is no turbulence concern in this area. From functionality standpoint, the whole shaft needs to be horizontal, so the split-face is selected as primary datum. Using split-face as primary datum is also process oriented datum selection, I believe. Then comes the mating function and coaxiality.
The bearing has a trunnion on each lateral side. Each trunnion fits into a bore on a pedestal. The pedestal then sits on my part on the surface that has 4 M6 tapped holes(thanks for pointing this out), and is bolted down by four M6 bolts. So axially and vertically the bearing is controlled by the bore on the pedestal. On my part in question, I can say basically the bearing is controlled axially by the eight M6 holes, vertically by datum D, inner split-face. The 8mm width (datum E) tab controls its lateral movement. So the bearing centerplane (taking bearing axial length as a FOS) is established by the 8 tapped holes.
I don't have sketches for the bearing and pedestal right now. I wish I could be more clear.
On the drawing I attached on 7/6, I should've added 151 basic to the four holes to the left, and 89 basic to the four holes to the right to datum B.
I think I want the 0 offset to be directly controlled while this is not.
RE: datum system on complicated part
Assign 8 hole pattern as a datum feature, let's say F, by attaching datum feature symbol to FCF controlling its location wrt |D|B|E| and control location of 2 holes by positional callout |pos.|dia.0(M)|D|F(M)|.
You may also want to re-locate datum feature symbols for A and D to other views, so that it is clear which features are selected as datum features A and D. I would say that current representation is at least confusing, not mentioning that showing GD&T symbols within part's contour should be avoided whenever possible (even if it is a rough sketch).
RE: datum system on complicated part
Agree on the datum D symbol location.
If I work to ISO, would the hole pattern datum feature approach still be valid?
RE: datum system on complicated part
RE: datum system on complicated part
Jim Sykes, P.Eng, GDTP-S
Profile Services www.profileservices.ca
TecEase, Inc. www.tec-ease.com
RE: datum system on complicated part
Hope attached pic explains what I meant. I just modeled them quickly to show the concept.
RE: datum system on complicated part
I can understand what you want the 8 holes to do, but tapped holes automatically have clearance (play) to begin with, and the holes within the pattern will have positional error wrt each other. To me it is not an effective datum feature for this application. Add that you are using shims ... the value as a pattern of datum features drops further.
Jim Sykes, P.Eng, GDTP-S
Profile Services www.profileservices.ca
TecEase, Inc. www.tec-ease.com
RE: datum system on complicated part
By the way, I remember there was a thread discussing threaded hole as datum. I could not find it.