HJM
Mechanical
- Jan 26, 2003
- 2
A big, forged crankshaft was metallographically inspected. On the polished and etched surface near a notch radius at the tap, segregations of manganese sulfide (MnS) were found. The largest inclusions were between 100µm and 300µm wide. The grain size was irregular, indicating that the forging reduction had been low, at least locally.
The consequences of a fatigue failure would be very severe, so a high safety factor should be applied.
There was some concern on the impact of the observed segregations on the fatigue life. During service life, the component is exposed to at least 1 Gigacycle, so also small cracks could eventually grow and lead to failure.
I’m slightly confused after looking at the literature:
1) In the ASM Handbook, Volume 1, Properties and Selection: Irons, Steels, and High Performance Alloys, I found:
“From the minor elements, phosphorus and sulfur are the most common and are always present in the composition. They can be as high as 0.15% for low-quality iron and are considerably less for high-quality iron, such as ductile iron or compacted graphite iron. The effect of sulfur must be balanced by the effect of manganese. Without manganese in the iron, undesired iron sulfide (FeS) will form at grain boundaries. If the sulfur content is balanced by manganese, manganese sulfide (MnS) will form, ***which is harmless*** because it is distributed within the grains. The optimum ratio between manganese and sulfur for an FeS-free structure and maximum amount of ferrite is:
% Mn = 1.7(% S) + 0.15”
2) In the ASM Handbook, Volume 19, Fatigue and Fracture, it was confirmed that cracks larger than about 0.1mm can be treated with LEFM, and therefore are dangerous. (see e.g. Kitagawa-Takahashi-diagram).
3) After the forging process, the MnS precipitates are not distributed homogenously, therefore the potential for fatigue cracking seems to be is increased, especially since we must assume that the local stress (3D) also could act locally in the “worst” direction.
4) Till now, I did not find ***relevant experimental*** data on MnS and fatigue life.
Questions
********
- Is the statement of the ASM-HB valid for fatigue, too?
- Are there some experimental data on the influence of MnS on the fatigue performance, especially at high numbers of cycles?
- Shouldn’t any defect of a size beyond the Kitagawa-Takahashi-limit be treated as LEFM-cracks, or does it depend of the type of inclusions, too?
I would be very glad to hear comments on my questions!
Customers specification
-----------------------------
Heat treatment:
Forging reduction: min. 3.0
Normalized
Stress relieved.
Mechanical Data required:
Yield Strength min. 340 MPa
U.T.S: 590-740MPa
Ductility: 20% parallel, 14% perpendicular
Impact test (ISO-U-Notch): min. 20J/15J
Composition
C = max. 0.50%
Si = max. 0.40%
P = max. 0.035%,
S = max. 0.030%
Mn = 0.40% to 1.40%
whereas according to Equation 1 only 0.20% Manganese is needed.
The consequences of a fatigue failure would be very severe, so a high safety factor should be applied.
There was some concern on the impact of the observed segregations on the fatigue life. During service life, the component is exposed to at least 1 Gigacycle, so also small cracks could eventually grow and lead to failure.
I’m slightly confused after looking at the literature:
1) In the ASM Handbook, Volume 1, Properties and Selection: Irons, Steels, and High Performance Alloys, I found:
“From the minor elements, phosphorus and sulfur are the most common and are always present in the composition. They can be as high as 0.15% for low-quality iron and are considerably less for high-quality iron, such as ductile iron or compacted graphite iron. The effect of sulfur must be balanced by the effect of manganese. Without manganese in the iron, undesired iron sulfide (FeS) will form at grain boundaries. If the sulfur content is balanced by manganese, manganese sulfide (MnS) will form, ***which is harmless*** because it is distributed within the grains. The optimum ratio between manganese and sulfur for an FeS-free structure and maximum amount of ferrite is:
% Mn = 1.7(% S) + 0.15”
2) In the ASM Handbook, Volume 19, Fatigue and Fracture, it was confirmed that cracks larger than about 0.1mm can be treated with LEFM, and therefore are dangerous. (see e.g. Kitagawa-Takahashi-diagram).
3) After the forging process, the MnS precipitates are not distributed homogenously, therefore the potential for fatigue cracking seems to be is increased, especially since we must assume that the local stress (3D) also could act locally in the “worst” direction.
4) Till now, I did not find ***relevant experimental*** data on MnS and fatigue life.
Questions
********
- Is the statement of the ASM-HB valid for fatigue, too?
- Are there some experimental data on the influence of MnS on the fatigue performance, especially at high numbers of cycles?
- Shouldn’t any defect of a size beyond the Kitagawa-Takahashi-limit be treated as LEFM-cracks, or does it depend of the type of inclusions, too?
I would be very glad to hear comments on my questions!
Customers specification
-----------------------------
Heat treatment:
Forging reduction: min. 3.0
Normalized
Stress relieved.
Mechanical Data required:
Yield Strength min. 340 MPa
U.T.S: 590-740MPa
Ductility: 20% parallel, 14% perpendicular
Impact test (ISO-U-Notch): min. 20J/15J
Composition
C = max. 0.50%
Si = max. 0.40%
P = max. 0.035%,
S = max. 0.030%
Mn = 0.40% to 1.40%
whereas according to Equation 1 only 0.20% Manganese is needed.