giangnguyen92
Aerospace
- Oct 3, 2019
- 20
Hi everyone,
I am reading the old gas turbine engine book and I am in trouble to understand their definition of positional tolerance and “total fit” in doweled rotor.
Problem: bolts are used to concentrically locating 02 disks stacked and transport between them in gas turbine engine.
Bolt has fit mode to hole on each disk (here transitional fit) and it must go through 02 discs. And holes on each disk has positional tolerance themselves. I attached here the scanned picture for your reference.
According to the book (dimensions are in inch):
Bolt diameter = .7545 +/- .0001
Hole diameter = .75495 +/- .00045
Thus fit = .00045 +/- .00055, i.e. from .0001 interference to .001 clearance.
Hole true position = +/- .0005
Hence, total fit = .00045 +/- .00105, i.e. from .0006 interference to .0015 clearance
So my 02 first questions are:
- What is “total fit”?
- How is that determined?
I try to refer to ASME Y14.5 but cannot find anything similar to this. I am looking for your engineering comments.
Perhaps it follows different tolerancing definition in aero engine OR it is just the old way of defining?
I am reading the old gas turbine engine book and I am in trouble to understand their definition of positional tolerance and “total fit” in doweled rotor.
Problem: bolts are used to concentrically locating 02 disks stacked and transport between them in gas turbine engine.
Bolt has fit mode to hole on each disk (here transitional fit) and it must go through 02 discs. And holes on each disk has positional tolerance themselves. I attached here the scanned picture for your reference.
According to the book (dimensions are in inch):
Bolt diameter = .7545 +/- .0001
Hole diameter = .75495 +/- .00045
Thus fit = .00045 +/- .00055, i.e. from .0001 interference to .001 clearance.
Hole true position = +/- .0005
Hence, total fit = .00045 +/- .00105, i.e. from .0006 interference to .0015 clearance
So my 02 first questions are:
- What is “total fit”?
- How is that determined?
I try to refer to ASME Y14.5 but cannot find anything similar to this. I am looking for your engineering comments.
Perhaps it follows different tolerancing definition in aero engine OR it is just the old way of defining?