
AISI Grade |
8620 |
9310 |
1018 |
4130 |
4140 |
4150 |
4340 |
4330V |
6150 |
O-6 |
O-1 |
300M |
FLEXOR® |
|
Alloy Symbol |
Alloy Name |
|||||||||||||
C |
Carbon |
0.200 |
0.100 |
0.180 |
0.300 |
0.400 |
0.500 |
0.400 |
0.300 |
0.500 |
1.450 |
0.900 |
0.420 |
0.340 |
Cr |
Chromium* |
0.500 |
1.200 |
0.000 |
0.900 |
0.900 |
0.900 |
0.800 |
0.800 |
0.950 |
0.200 |
0.500 |
0.800 |
0.850 |
Mo |
Molybdenum* |
0.200 |
0.100 |
0.000 |
0.200 |
0.200 |
0.200 |
0.200 |
0.400 |
0.000 |
0.250 |
0.000 |
0.380 |
0.500 |
V |
Vanadium* |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.070 |
0.000 |
0.000 |
0.000 |
0.070 |
0.000 |
W |
Tungsten* |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.000 |
0.500 |
0.000 |
0.500 |
Ni |
Nickel |
0.550 |
3.250 |
0.000 |
0.000 |
0.000 |
0.000 |
1.750 |
1.750 |
0.000 |
0.000 |
0.300 |
1.800 |
0.100 |
Mn |
Manganese |
0.800 |
0.550 |
0.750 |
0.800 |
0.800 |
0.800 |
0.800 |
0.850 |
0.800 |
0.800 |
1.200 |
0.750 |
0.800 |
Si |
Sillicon |
0.250 |
0.250 |
0.000 |
0.250 |
0.250 |
0.250 |
0.250 |
0.300 |
0.250 |
1.200 |
0.500 |
1.650 |
0.300 |
S |
Sulfur |
0.030 |
0.020 |
0.050 |
0.030 |
0.030 |
0.030 |
0.030 |
0.006 |
0.040 |
0.030 |
0.030 |
0.050 |
0.015 |
Total % Alloy |
2.530 |
5.470 |
0.980 |
2.480 |
2.580 |
2.680 |
4.230 |
4.476 |
2.540 |
3.930 |
3.930 |
5.920 |
3.405 |
|
Total % Carbide Forming Alloy |
0.700 |
1.300 |
0.000 |
1.100 |
1.100 |
1.100 |
1.000 |
1.270 |
0.950 |
0.450 |
1.000 |
1.250 |
1.850 |
*Carbide Forming Alloys Elements are based upon averages and may vary from typicals above.
ANNEAL - This is similar to normalizing, but instead of air cooling, the part must be slow cooled in the furnace. The part will become soft, due to carbon being released from solution.
HARDEN - This is achieved with most steels by quenching the steel from the proper austenitizing temperature, into either air, oil or water.
HARDENABILITY - Hardenability is a function of alloy content. This term is used to designate the depth and distribution of hardness. Reduced core hardnesses are a result of low hardenability, and therefore, low alloy content. Low hardenability, in effect, reduces the overall strength of a part.
HARDNESS - Hardness is a function of the total carbon content of a steel, and is relative to the tensile strength and yield strength. The higher the carbon content – the higher the attainable surface hardness! However, hardness alone does not guarantee success in your application. Other factors to consider when selecting the correct steels are listed herein.
MACHINABILITY – The ease to which a material can be turned or milled generally denoted by a percentage of a free machining steel such as B1112. FLEXOR in the as rolled condition has a rating of approximately 60%.
NORMALIZE - This is a high temperature draw or temper. The purpose is to eliminate stress from cold working (ie: machining) or welding. The range is usually between 1400 degrees Fahrenheit and 1700 degrees Fahrenheit.
STRESS RELIEVE - This is usually a low temperature draw or temper. The temperature range to stress relieve most alloy and carbon steels is between 350 degrees and 500 degrees Fahrenheit. The stress relieve temperature of 350 degrees will not reduce the “as quenched” hardness of the part.
TEMPER OR DRAW - After hardening (see above), all steels must be tempered to bring the hardness down into a usable range. This is done by reheating the steel to an approximate temperature of between 350 degrees and 1200 degrees, depending on the type of steel being tempered and hardness required. It is important to note that you must harden and quench the steel in the proper agent, prior to tempering.
TENSILE STRENGTH - This measure is used widely but means little since the part will always fail before the “tensile load” is reached.
TOUGHNESS - Toughness is measured in foot pound force, Izod impact, or
Charpy impact tests. The higher the hardness, the lower the toughness. Therefore, caution must be taken to choose a steel where you do not sacrifice toughness for higher hardness. This can result in a brittle part, and possible failure.
WEAR RESISTANCE - Wear resistance is the ability to resist erosion caused by mechanical working or abrasion. Wear resistance is related to hardness, but most importantly it is increased by higher alloy content. Alloys such as chromium, molybdenum, vanadium, and tungsten are all carbide forming alloys. Best wear properties are achieved when higher amounts of these alloys and carbon are used in a steel.
WORKHARDEN - When a steel is cold worked, this area deforms, and will increase in hardness. This increases surface wear properties, but reduces ductility. Nickel based steels such as 9310, 300M, 4330V, and 4340 tend to workharden.
YIELD STRENGTH - This is the load in which the part will return to its original size after the load is removed.
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Pennsylvania Steel Corporation
12380 Beech Daly Road
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