UMDpru
Mechanical
- May 16, 2007
- 41
Hello,
I am trying to determine the maximum allowable torque to be applied to te a 3/8-16UNC-2A Bolt made of the following materials:
Ti CP1(Grade4) Yield=70ksi
Ti CP4(Grade1) Yield=25ksi
Ti 6A1-V4 Yield= 120ksi
I have found some formulas that relate to steel in the Machinery's handbook 23rd edition page 1279 formulas (2a) and (2b). My first question is why do they list two different formulas which can give vastly different stress areas based upon the material yield Strength? Shouldnt the stress area be based upon the bolt geometry and not any material properties?
Using the two different formulas yields really different numbers for maximum torque.
Secondly, it states in the handbook that these are for steels. can they be used with titanium or other bolt materials? If they can not be used, can someone please point in the direction where I can find the correct formulas?
I have used the following formulas to determine maximum allowable torque.
Fmax=Maximum tensile load
Fmax=.8Yield*At where At=Stress Area
Tmax=Maximium Torque
Tmax=.2*D*Fmax where .2=assumed coefficient of dynamic friction, D=nominal thread diameter
Ti CP1 Tmax=95.33 ft-lbs
Ti CP4 Tmax=34 ft-lbs
Ti 6A1-4V Tmax= 163.5 ft-lbs
These numbers were generated using formula 2a for calculating At for all.
If I use formula 2a for Ti CP1, and Ti CP4 which have yields below 100ksi and use Formula 2b for Ti 6A1-4V which has a yield of 120ksi, it turns out that the Ti CP1 can be torqued to twice as much as the Ti 6A1-4V? that doesnt make sense to me.
Please help.
I am trying to determine the maximum allowable torque to be applied to te a 3/8-16UNC-2A Bolt made of the following materials:
Ti CP1(Grade4) Yield=70ksi
Ti CP4(Grade1) Yield=25ksi
Ti 6A1-V4 Yield= 120ksi
I have found some formulas that relate to steel in the Machinery's handbook 23rd edition page 1279 formulas (2a) and (2b). My first question is why do they list two different formulas which can give vastly different stress areas based upon the material yield Strength? Shouldnt the stress area be based upon the bolt geometry and not any material properties?
Using the two different formulas yields really different numbers for maximum torque.
Secondly, it states in the handbook that these are for steels. can they be used with titanium or other bolt materials? If they can not be used, can someone please point in the direction where I can find the correct formulas?
I have used the following formulas to determine maximum allowable torque.
Fmax=Maximum tensile load
Fmax=.8Yield*At where At=Stress Area
Tmax=Maximium Torque
Tmax=.2*D*Fmax where .2=assumed coefficient of dynamic friction, D=nominal thread diameter
Ti CP1 Tmax=95.33 ft-lbs
Ti CP4 Tmax=34 ft-lbs
Ti 6A1-4V Tmax= 163.5 ft-lbs
These numbers were generated using formula 2a for calculating At for all.
If I use formula 2a for Ti CP1, and Ti CP4 which have yields below 100ksi and use Formula 2b for Ti 6A1-4V which has a yield of 120ksi, it turns out that the Ti CP1 can be torqued to twice as much as the Ti 6A1-4V? that doesnt make sense to me.
Please help.