NB02
Mechanical
- Oct 31, 2007
- 5
Hello,
Looking for some help on calculating the ID of a bushing that has been shrink fitted into a larger bushing. I can't seem to find an equation for this. I have calculated the interference pressure, and the hoop stress'. Application is we have two manufactures of the parts that are shrink fitted together. We would like to tolerance the the interference fit and ID of the inner hub to allow for +/- .005" of the inner hub ID after the shrink fit into the outer hub.
Material Assumptions - Modulus of Elasticity = 30,000 ksi - Poisson's Ratio = .3
Outer Hub OD = 32"
Out Hub ID = 22"
Inner Hub OD = 22.050"
Inner Hub ID = 18"
Interference Pressure ~ 8693 psi
Outer Hub Hoop Stress ~ 24,276 psi
Inner Hub Compression Stress ~43,899 psi
So I am trying to calculate what the ID of the inner hub would be after the shrink fit operation assuming the above is true? We would like to get away from having to do a final machining of the bore after assembly if possible. I was able to find a few old threads on this website about calculation of area but they didn't really make any sense to me. Any help in the right direction would be appreciated.
Best Regards,
Looking for some help on calculating the ID of a bushing that has been shrink fitted into a larger bushing. I can't seem to find an equation for this. I have calculated the interference pressure, and the hoop stress'. Application is we have two manufactures of the parts that are shrink fitted together. We would like to tolerance the the interference fit and ID of the inner hub to allow for +/- .005" of the inner hub ID after the shrink fit into the outer hub.
Material Assumptions - Modulus of Elasticity = 30,000 ksi - Poisson's Ratio = .3
Outer Hub OD = 32"
Out Hub ID = 22"
Inner Hub OD = 22.050"
Inner Hub ID = 18"
Interference Pressure ~ 8693 psi
Outer Hub Hoop Stress ~ 24,276 psi
Inner Hub Compression Stress ~43,899 psi
So I am trying to calculate what the ID of the inner hub would be after the shrink fit operation assuming the above is true? We would like to get away from having to do a final machining of the bore after assembly if possible. I was able to find a few old threads on this website about calculation of area but they didn't really make any sense to me. Any help in the right direction would be appreciated.
Best Regards,