Hertzian contact stress SS-2244 / AISI-SAE 4140

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SUMMARY

The forum discussion centers on determining the maximum allowed Hertzian contact stress for SS-2244 / AISI-SAE 4140 steel. Key material properties include tensile strength (F_tu = 150 ksi), yield strength (F_ty = 132 ksi), and bearing strength (F_bru = 219 ksi). The conversation highlights the importance of material condition, noting that AISI-4140 can be heat treated to achieve higher strength levels compared to AISI-4130. For calculations involving a 2.5 mm pin, a bearing strength approximation of 158 ksi for annealed and 225 ksi for heat-treated conditions is recommended.

PREREQUISITES
  • Understanding of Hertzian contact stress principles
  • Familiarity with material properties of AISI-SAE 4140 and AISI-SAE 4130
  • Knowledge of heat treatment effects on steel
  • Basic mechanics of materials, including elastic modulus and Poisson's ratio
NEXT STEPS
  • Research the MMPDS (Metallic Materials Properties Development and Standardization) for material properties
  • Explore the ASMD (Aerospace Materials Database) for advanced material data
  • Learn about the calculation methods for Hertzian contact stress
  • Investigate the effects of heat treatment on AISI-4140 and AISI-4130 steel
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Mechanical engineers, materials scientists, and anyone involved in the design and analysis of components subjected to contact stresses, particularly in applications using AISI-SAE 4140 steel.

Ian06
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Hello guys!


Is there anyone who knows where i can find information about maximum allowed Hertzian contact stress for material SS-2244 / AISI-SAE 4140 or any similar material quality?

I have been searching for this information in several Swedish books and material tables, without success.
 
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Can you give us some more information on the potential failure mode?

AISI-4140 Low Alloy Steel at room temperature
F_tu = 150 ksi
F_ty = 132 ksi
F_cy = 145 ksi
F_su = 90 ksi
F_bru = 219 ksi
F_bry = 189 ksi

t = tensile; c = compressive; br = bearing; u = ultimate; y = yield
 
You need to define what your failure criteria is, especially with contact stresses.
 
A pin made of high grade spring steel is pressed tangential against the inside of a hub.

Pin diameter (r1) = 2,5 mm
Hub diameter (r2) = 55 mm (concave, and therefore -55 mm in Hertzian calculations)
Contact length = 40 mm
Hub material SS-2244 / AISI-SAE 4140

The objective is to "backwards" calculate the maximum force F (N) that can be applied without causing plastic deformation on the inside of the hub.

I´ll draw a simple sketch and add it tomorrow.

Unfortunately my english is rather bad.
 

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minger said:
Can you give us some more information on the potential failure mode?

AISI-4140 Low Alloy Steel at room temperature
F_tu = 150 ksi
F_ty = 132 ksi
F_cy = 145 ksi
F_su = 90 ksi
F_bru = 219 ksi
F_bry = 189 ksi

t = tensile; c = compressive; br = bearing; u = ultimate; y = yield

Thank you minger! Do you have any reference (book/website etc.) for this information?
 
minger said:
Can you give us some more information on the potential failure mode?

AISI-4140 Low Alloy Steel at room temperature
F_tu = 150 ksi
F_ty = 132 ksi
F_cy = 145 ksi
F_su = 90 ksi
F_bru = 219 ksi
F_bry = 189 ksi

t = tensile; c = compressive; br = bearing; u = ultimate; y = yield
That seems awfully high for 4140 in the annealed state. Are you sure that isn't in some heat treated condition? The OP didn't mention anything about the final condition so this may be correct.
 
Oh, the 2.5mm (roughly 0.1") makes a difference. The spec I quoted was for 1" or greater...

Nope, that is for less than 1". It should be good if it is 4140. It seems that for smaller diameters, AISI-4130 is more commonly used, which is significantly weaker.

Some comments:

AISI 4130 is a chromium-molybdenum steel that is in general use due to its well-established heat-treating practices and processes techniques. It is available in all sizes of sheet, plate and tubing. Bar stock of this material is also used for small forgings under one-hal finch in thickness. AISI-4135 is a slightly higher carbon version of AISI 4130, is available in sheet, plate and tubing.

AISI 4140 is a chromium-molybdenum steel that can be heat treated in thicker sections and to higher strength levels than AISI 4130. This steel is generally used for structural machined and forged parts one-half inch and over in thickness. It can be welded but it is more difficult to weld than the lower carbon grade AISI 4130.

OK, so agreed Fred, without a little more material information, it's hard to tell. Let me get the other source. OK, 1" round bar has
Annealed - F_ty = 62ksi
Normalized - F_ty = 93 ksi

You're probably looking at a bearing strength, so for bar, forgings
Annealed - no data
Normalized - 158 ksi
Normalized and heat treated (with Ftu = 140) - 225 ksi
Normalized and heat treated (with Ftu = 160) - 252 ksi
Normalized and heat treated (with Ftu = 180) - 284 ksi

edit: Ian, my first source is a MIL spec manual called the MMPDS (Metallic Materials Properties Development and Standardization). It's a slightly more current version of something that was called...(something else can't remember). We just 'have' it, although I do know for fact that it is available from off of a website hosted by a Big10 school that makes a name for itself with engineering.

I also use the ASMD (Aerospace Materials Database), which we have both in several extremely large old books, and as an online website we need to log into.
 
So a value between 140-284 ksi will work as an approximation for calculations with the 2,5 mm pin?
 
I would say 158 ksi if its not heat-treated, 225 if it is.

Since you're doing Hertzian stress, you're probably going to need elastic modulus and Poisson's huh?
 
  • #10
minger said:
I would say 158 ksi if its not heat-treated, 225 if it is.

Since you're doing Hertzian stress, you're probably going to need elastic modulus and Poisson's huh?

Yes please! :smile:
 

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