Pioneers in the industry, we offer Forging Steel such as Forging Steel C15, Forging Steel C 20, Forging Steel C 25, Forging Steel C 35, Forging Steel C 40, Forging Steel C 45 and many more items from India. |
Application | Automobile Industry, Construction |
Usage/Application | Automobile Industry, Construction |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
Grade | Min | Max |
---|---|---|
Carbon, C | 0.35 | 0.45% |
Manganese, Mn | 0.45 | 0.70% |
Silicon, Si | 0.10 | 0.35% |
Nickel, Ni | 1.3 | 1.8 |
Molybdenum, Mo | 0.20 | 0.35 |
Chromium,Cr | 0.90 | 1.40% |
Sulfur, S | -.-- | 0.05% |
Phosphorous, P | -.-- | 0.05% |
Carbon(C) | Directly influences the hardness and strength of the steel, decreases toughness. |
Chromium(Cr) | Improves Hardenability, high temperature strength, wear resistance and even corrosion resistance(Cr>14%). |
Cobalt(Co) | Improves retention of hardness at high temperatures. |
Molybdenum(Mo) | Increases yield point and strength. Improves Hardenability and wear resistance. Manganese Lowers effects of Iron sulphides, increases hardenability, wear resistance. |
Nickel(Ni) | Increases toughness at lower temperatures, slows the corrosion process. Improves toughness, grain structure, high temperature strength, wear resistance, etc. |
Vanadium(V) | Increases wear resistance, high temperature strength, retention of hardness etc. |
Silicon(Si) | It is a deoxidizing agent. Increases strength and wear resistance. It is of importance that certain elements are as low as possible. Elements like Hydrogen, Oxygen, Nitrogen, Phosphorous, Sulphur create defects inside & also reduce the mechanical properties of steels. |
Minimum Order Quantity | 1000 Kg |
Size | 1 inch |
Thickness | 6 mm |
Single Piece Lengh | 3 meter |
Usage/Application | Manufacturing |
Shape | Round |
Application | Construction, Manufacturing |
Material Grade | NA |
Steel Grade | Duplex 2205 |
Material | NA |
Steel Type | Mild Steel |
Single Piece Length | 3 meter |
Surface Finish | Polished |
Surface Finishing | NA |
Technique | NA |
Color | NA |
Packaging Size | NA |
Packaging Type | NA |
Product Type | NA |
Surface Treatment | NA |
Customization | Customized |
Alloy | With Alloy |
Brand | v |
Country of Origin | Made in India |
Mild Steel, fairly easy to machine but with a tendency to ‘rip’ if unlubricated. It is very easy to weld and is used as a more general purpose steel for multiple applications. DescriptionC-20 is an unalloyed low carbon mild steel grade supplied as a hot rolled or bright drawn finish bar. As a low carbon steel grade it provides low strength with good machinability and is suitable for welding. Chemical composition
Lightly stressed bolts, fixings, shafts, spacers, hubs and bushings. Bracket, linkages and base plates would be fine to produce using EN3. Not suitable forStress components such as torque loaded shafts, high bending forces and shock loading. The material will yield and distort under stress conditions, bending before shear. MachiningSurface ‘ripping’ is more evident in EN3 so lubrication is essential. Fairly high surface speeds should be used with moderate feeds. Screw cutting is easy with cutting oil and achieving a fine finish is achieved with slight polishing. Very nice to weld with good flow and strength. ApplicationsCommonly used for general engineering C-20 is suitable for applications such as bolts, shafts, spaces, hubs, base plates, brackets. fixtures and jigs. AnnealingC-20 is commonly supplied bright drawn or as rolled. If annealing is required heat to 880-910°C, furnace cool. HardeningAs a low carbon steel C-20 is not ideally suited for heat treatment(EN8 or EN9) may be a better suited option). If hardening is required heat to a temperature of 880-910°C. Quench in water and temper. Heat TreatmentWhen hardening C-20 heat treatment temperatures, including rate of heating, cooling and soaking times will vary due to factors such as the shape and size of each component. Other considerations during the heat treatment process include the type of furnace, quenching medium and work piece transfer facilities. Please consult your heat treatment provider for full guidance on heat treatment of C-20 carbon steel. Thermal Properties
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Minimum Order Quantity | 1 Kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
C40 steel plate is one mainly of high carbon steel,EN 10083 C40 steel plate is meduim Carbon Steels are similar to low carbon steel except that the carbon ranges from 0.30 to 0.60% & the manganese from 0.50 to 1.65%. Increasing the carbon content is approximately 0.5% with an accompanying increase in manganese allows medium carbon steels to be used in the quenched & tempered conditions.
Chemical compositionElement | Min | Max |
---|---|---|
Carbon, C | 0.35 | 0.45 |
Manganese, Mn | 0.60 | 01.00 |
Silicon, Si | 0.5 | 0.35 |
Sulfur, S | -.-- | 0.06 |
Phosphorous, P | -.-- | 0.06 |
20-100°C | 20-200°C | 20-300°C | 20-400°C | 20-500°C | 20-600°C | 20-700°C |
---|---|---|---|---|---|---|
11.1 | 11.9 | 12.7 | 13.4 | 14 | 14.4 | 14.8 |
Nominal thickness (mm): | to 16 | 16 - 100 | 100 - 250 |
---|---|---|---|
Rm - Tensile strength (MPa) (+N) | 580 | 550 | 530 |
Nominal thickness (mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
Rm - Tensile strength (MPa) (+C) | 700-1000 | 650 - 980 | 620 - 920 | 590-840 | 550 - 820 |
Nominal thickness(mm): | to 16 | 16 - 100 | 100 - 250 |
---|---|---|---|
Re - Upper yield strength or R p0.2 - 0.2% proof strength (MPa) (+N) | 320 | 290 | 260 |
Nominal thickness(mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
R p0.2 0.2% proof strength (MPa) (+C) | 540 | 460 | 365 | 330 | 290 |
Nominal thickness (mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
A - Min. elongation at fracture (%) (+C) | 6 | 7 | 8 | 9 | 9 |
Nominal thickness (mm): | to 16 | 16 - 100 | 100 - 250 |
---|---|---|---|
A - Min. elongation Lo = 5,65 √ So (%) (+N) | 16 | 17 | 17 |
Brinell hardness (HBW): (+SH) | 163 - 211 |
USA | Germany DIN,WNr | Russia GOST | Japan JIS | France AFNOR | England BS | Italy UNI | China GB | Czechia CSN |
---|---|---|---|---|---|---|---|---|
1038 1040 | 1.0511 C40 Ck40 | 40 | S40C | AF60C40 AF60C45 XC42HI | 070M40 080M40 En8 | C40 | 40 | 12041 |
Low hardenability; it shows intermediate features between those of steels with medium and those of steels with high carbon content; therefore it is not easy to obtain the required features by quenching in oil and the quenching in water can result in cracking.
Mechanical propertiesR eH | Minimum yield strength / Mindestwert der oberen Streckgrenze / Limite d�elasticite minimale |
---|---|
R m | Tensile strength / Zugfestigkeit / Resistance a la traction |
A | Minimum elongation / Mindestwert der Bruchdehnung / Allongement minimal |
J | Notch impact test / Kerbschlagbiegeversuch / Essai de flexion par choc |
Minimum Order Quantity | 1 kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
Element | Min | Max |
Carbon, C | 0.35 | 0.45% |
Manganese, Mn | 0.60 | 1.0% |
Silicon, Si | 0.5 | 0.35% |
Sulphur | -.-- | 0.6 |
Phosphorus | -.-- | 0.6 |
Max Stress | 700-850 n/mm 2 | |
Yield Stress | 465 n/mm 2 Min | (up to 19mm LRS) |
0.2% Proof Stress | 450 n/mm 2 Min | (up to 19mm LRS) |
Elongation | 16% Min | (12% if cold drawn) |
Impact KCV | 28 Joules Min | (up to 19mm LRS |
Hardness | 201-255 Brinell |
BS970: 1955 | EN8 |
BS970/PD970: | 080M40 |
1970 onwards | |
European | C40, C45, Ck40,Ck45, Cm40, Cm45 |
Werkstoff No. | 1.0511, 1.1186, 1.1189 |
US SAE (AISI) | 1039, 1040, 1042, 1043, 1045 |
Carbon | 0.35-0.45% |
Manganese | 0.60-1.00% |
Silicon | 0.05-0.35% |
Phosphorous | 0.06% max |
Sulphur | 0.06% max |
Minimum Order Quantity | 1 kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
EN9, also known as 070m55, available in diameters, flats, squares and plates with a carbon content 0.50/0.60 this is a medium carbon steel which can develop a tensile strength of 700N/mm 45tsi. In the normalized condition EN9 can be used for gears, sprockets and cams.
EN9 is a medium carbon steel grade commonly supplied in the as rolled condition. It can be flame or induction hardened to produce a high surface hardness with excellent wear resistance for a carbon steel grade.
Chemical CompositionElement | Min | Max |
Carbon, C | 0.50 | 0.60% |
Manganese, Mn | 0.50 | 0.80% |
Silicon, Si | 0.05 | 0.35% |
Sulfur, S | -.-- | 0.06% |
Phosphorous, P | -.-- | 0.06% |
Heat Treatment | Condition Tons/SQ.inch | Tensile Stress RE MPA | RP0.2 MPA | A min on 5.65so | Impact | Hardness HB | Limited Ruling Section mm | |
---|---|---|---|---|---|---|---|---|
IZODFT.L.b | KCV Joules | |||||||
Normalise | 45 | 700 | - | 12 | - | - | 201-255 | 63 |
39 | 600 | - | 13 | - | - | 170/223 | 250 | |
R | 45/55 | 700/850 | 385 | 14 | - | - | 201/277 | 100 |
S | 50/60 | 775/925 | 450 | 14 | - | - | 223/277 | 63 |
T | 55/65 | 850/1000 | 555 | 12 | - | - | 248/302 | 19 |
EN9 is used commonly for many general engineering applications. Typical applications include, shafts, axes, knives, bushes, crankshafts, screws, sickles, wood working drills and hammers.
CharacteristicsHeat treatment temperatures, including rate of heating, cooling and soaking times will vary due to factors such as the shape and size of each EN9 steel component. Other considerations during the heat treatment process include the type of furnace, quenching medium and work piece transfer facilities. Please consult your heat treatment provider for full guidance on heat treatment of EN9 carbon steel.
Minimum Order Quantity | 1000 kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
Element | Min | Max |
Carbon, C | 0.35 | 0.45% |
Manganese, Mn | 0.50 | 0.80% |
Silicon, Si | 0.10 | 0.35% |
Nickel, Ni | -.-- | -.-- |
Molybdenum, Mo | 0.20 | 0.40% |
Chromium,Cr | 0.90 | 1.50% |
Sulfur, S | -.-- | 0.05 |
Phosphorous, P | -.-- | 0.05 |
Heat | Tensile | Yield | a% on | Impact | Impact | Proof | Hardness | Size |
---|---|---|---|---|---|---|---|---|
Treatment | Strength | Stress | 5.665ÖSo | Izod J | KCV J | Stress | HB | mm |
Rm N/mm² | Re N/mm² | rp0.2 | ||||||
R | 700/850 | 495 | 15 | 34 | 28 | 480 | 201/225 | >100≤250 |
S | 775/925 | 555 | 13 | 27 | 22 | 540 | 223/277 | >150≤250 |
S | 775/925 | 585 | 15 | 54 | 50 | 570 | 223/277 | >63≤150 |
T | 850/1000 | 680 | 13 | 54 | 50 | 665 | 248/302 | >29≤100 |
U | 925/1075 | 755 | 12 | 47 | 42 | 740 | 269/331 | >13≤63 |
V | 1000/1150 | 850 | 12 | 47 | 42 | 835 | 293/352 | >6≤29 |
W | 1075/1225 | 940 | 12 | 40 | 35 | 925 | 311/375 | >6≤19 |
Minimum Order Quantity | 1000 Kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
Element | Min | Max |
---|---|---|
Carbon, C | 0.12 | 0.18% |
Manganese, Mn | 0.30 | 0.60% |
Silicon, Si | 0.10 | 0.35% |
Nickel, Ni | 3.00 | 3.75% |
Molybdenum, Mo | 0.10 | 0.25% |
Chromium,Cr | 0.60 | 1.1% |
Sulfur, S | -.-- | 0.05% |
Phosphorous, P | -.-- | 0.05% |
Tensile Strength N/mm² | Elongation % | Impact Izod J | Impact KCV J | Hardness s HB | Reduction of Area % |
---|---|---|---|---|---|
1110 | 15 | 40 | 35 | 341 | 50 |
Minimum Order Quantity | 1000 kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | NA |
Technique | NA |
Country of Origin | Made in India |
Element | Min | Max |
---|---|---|
Carbon, C | 0.35 | 0.45% |
Manganese, Mn | -.-- | 0.65% |
Silicon, Si | 0.10 | 0.45% |
Nickel, Ni | -.-- | 0.40% |
Molybdenum, Mo | 0.10 | 1.25% |
Chromium,Cr | 1.04 | 1.08% |
Sulfur, S | -.-- | 0.05% |
Phosphorous, P | -.-- | 0.05% |
Aluminium | 0.90 | 1.03 |
Condition | Tensile N/mm² | Yield N/mm² | Elongation % | Izod KCV J | Hardness Brinell |
---|---|---|---|---|---|
R | 700-850 | 480 | 16 | 28 | 201-255 |
S | 775-925 | 525 | 14 | 16 | 223-27 |
Material Grade | EN.19 |
Finish | Polished |
Single Piece Length | 3 meter |
Usage/Application | Construction |
Test Certificate | ISO |
Country of Origin | Made in India |
Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
C15 is a plain carbon steel with a nominal 0.15% carbon content. It is a relatively low strength steel but it may be quenched and tempered for increased strength.
Chemical compositionElement | Min | Max |
---|---|---|
Carbon, C | -.-- | 0.20 |
Manganese, Mn | -.-- | 0.80 |
Silicon, Si | -.-- | 0.10 |
Sulfur, S | -.-- | 0.06 |
Phosphorous, P | -.-- | 0.06 |
Nominal thickness (mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
Rm - Tensile strength (MPa) (+C) | 500-800 | 480-780 | 430-730 | 380-670 | 340-600 |
Nominal thickness(mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
R p0.2 0.2% proof strength (MPa) (+C) | 380 | 340 | 280 | 240 | 215 |
Nominal thickness (mm): | 5-10 | 10-16 | 16 - 40 | 40 - 63 | 63 - 100 |
---|---|---|---|---|---|
A - Min. elongation at fracture (%) (+C) | 7 | 8 | 9 | 11 | 12 |
Element | C | Mn | Si | S | P | cr | Ni | Mo |
---|---|---|---|---|---|---|---|---|
Min | .90 | .35 | .10 | 0.00 | 0.00 | 1.00 | - | |
Max | 1-20 | .75 | .35 | 0.04 | 40 | 1.60 | - | - |
20-100°C | 20-100°C |
---|---|
11 | 11.8 |
Properties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 210 |
Density [g/cm3]: | 7.85 |
Thermal conductivity [W/m.11] | 58.6 |
Electric resistivity [Ohm mm2/m]: | 0.11 |
Specific heat capacity[lig.11] | 0.46 |
The low carbon steels, such as C15 are used for applications such as cold headed fasteners and bolts.
Soft AnnealingHeat to 850-950°C, cool slowly. This will produce a hardness of 90-100 HB.
Stress RelievingStress relieving to remove machining stresses should be carried out by heating to approx. 540°C, holding for 1-2 hours at heat, followed by air cooling. This operation is performed to reduce distortion during heat treatment.
ForgingHot forming temperature: 1200-950°C.
MachinabilityMachinability of C15 steel is fairly good, especially in the cold drawn or cold worked condition. Based upon carbon steel AIS11112 as a reference that is considered 100% machinable (easily machined) the C15 steel has a rating of 55%.
Corrosion ResistanceThis is a plain carbon steel and has no corrosion resistance. It will rust unless protected.
WeldingC 15 is easily cold worked by traditional means. Following severe cold working a stress relief, or full, anneal should be performed.
Single Piece Length | 3 meter |
Surface Finish | Galvanized |
Material Grade | Standard |
Application | Construction |
Shape | Round |
Thickness/Diameter | 1-2 inch, 0-1 inch, 2-3 inch |
Customization | Not Customized |
Description Carbon steel, medium carbon steel. This steel grade has simular propeties as the steel CK35. ApplicationsPlain carbon steel for mechanical engineering and automotive components Applications include levers, boks, studs, nuts, and similar parts which are headed, upset, or extruded. Applications for wires include nails regui-ing high shank rigidity or strength and quench-hardened nails. Chemical composition
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Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
Description C45 is a medium carbon steel is used when greater strength and hardness is desired than Si the as rolled’ condition. Extreme size accuracy, straightness and concentricity combine to minimize wear in high speed appications. Turned, ground and polished. Designation by StandardsBrand Name: C45Mat No: 1.0503 DIN : C45 EN: - AISI: 1045Applications Quenched and subsequently tempered steel for screws, forgings, wheel tires, shafts, sickles,axes, knives, wood working drills, hammers, etc. Chemical composition
Heat to 680-710°C, cool slowly. This will produce a maximum Brinell hardness of 207. NormalizingNormalizing temperature (°C): 840-880°C. HardeningHarden from a temperature of 820-860°C followed by water or oil quenching. TemperingTempering temperature 550-660~C/air Equivalent grades of grade C45
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Single Piece Length | 3 meter |
Surface Finish | Galvanized |
Usage/Application | Construction |
Shape | Round |
Thickness/Diameter | 1-2 inch, 2-3 inch |
Surface Finishing | Standard |
C55 is a medium carbon steel is used when greater strength and hardness is desired than Si the as rolled’ condition. Extreme size accuracy, straightness and concentricity combine to minimize wear in high speed appications. Turned, ground and polished.
Chemical compositionElement | Min | Max |
---|---|---|
Carbon, C | 0.50 | 0.60 |
Manganese, Mn | 0.60 | 0.90 |
Silicon, Si | -.-- | 0.30 |
Sulfur, S | -.-- | 0.30 |
Phosphorous, P | -.-- | 0.30 |
Properties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 205 |
Density [g/cm3]: | 7.85 |
Heat to 650-700°C, cool slowly in furnace. This will produce a maximum Brinell hardness of 229.
NormalizingNormalizing temperature: 825-865°C/air.
HardeningHarden from a temperature of 805-845°C followed by water or oil quenching.
TemperingTempering temperature: 550-660°C/air.
Mechanical PropertiesDiameter d | 0.2 % proof stress | Tensile strength | Elongation | Reduction Z |
---|---|---|---|---|
(mm) | (Wmm 2 ) | (Nfrnm 2 ) | A5 (%) | (%) |
upto 16 | 540 | 780-930 | 12 | 20 |
17-40 | 460 | 740-890 | 14 | 30 |
41-100 | 420 | 700-850 | 15 | 35 |
USA | Germany DIN,WNr | Russia GOST | Japan JIS | France AFNOR | England BS | Italy UNI | China GB | Czechia CSN |
---|---|---|---|---|---|---|---|---|
1055 | C55 | 50 55 | S55C | AF70C55 C54 | 070M55 50 En9 | 1C55 C55 | 55 | 1655 |
Spain | Sweden | Poland | Inter | |||||
UNE | SS | PN | ISO | |||||
C55k | 1655 | 55 | C55 C55E4 |
+A | Soft annealed |
---|---|
+AC | Annealed to achieve spheroidization of the carbides |
+AR | As rolled |
+AT | Solution annealed |
+C | Cold drawn / hard |
+CR | Cold rolled |
+FP | Treated to ferrite-pearlite structure and hardness range |
+I | Isothermal annealing |
+LC | Cold drawn / soft |
+M | Thermo mechanical rolling |
+N | Normalized |
+NT | Normalized and tempered |
+P | Precipitation hardened |
+PE | Peeled |
+QA | Air quenched and tempered |
+QL | Liquid quenched and tempered |
+QT | Quenched and tempered |
+S | Treated to improve shearability |
+SH | As rolled and turned |
+SR | Cold drawn and stress relieved |
+T | Tempered |
+TH | Treated to hardness range |
+WW | Warm worked |
+U | Untreated |
Usage/Application | Automobile Industry, Construction |
Application | Construction |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
Element | Min | Max |
---|---|---|
Carbon | 0.12 | 0.18% |
Manganese | 0.30 | 0.60% |
Silicon | 0.10 | 0.35% |
Nickel | 0.60 | 1.10% |
Molybdenum | -.-- | -.-- |
Chromium | 3.00 | 3.75% |
Sulfur | 0.00 | 0.05% |
Phosphorous | 0.00 | 0.05% |
Tensile Strength N/mm² | Elongation % | Impact Izod J | Impact KCV J | Hardness HB | Reduction of Area % |
---|---|---|---|---|---|
1100 | 15 | 40 | 35 | 341 | 50 |
BS 970 1991 | BS 970 1955 EN | AISI/SAE | Werkstoff |
---|---|---|---|
655M13 | EN36 | 3415 | 1.5752 |
Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
Element | Min % | Max % |
---|---|---|
Carbon, C | 0.45 | 0.55 |
Manganese, Mn | 0.50 | 0.80 |
Silicon, Si | -.-- | 0.50 |
Nickel, Ni | -.-- | -.-- |
Molybdenum, Mo | -.-- | -.-- |
Chromium,Cr | 0.80 | 1.20 |
Sulfur, S | -.-- | 0.05 |
Phosphorous, P | -.-- | 0.05 |
Vanadium | 0.15 | -.-- |
Quantity | Value | Unit |
---|---|---|
young's Modulus | 200000-200000 | MPa |
Tensile strength | 650-880 | MPa |
Elongation | 41876 | % |
Fatigue | 275-275 | MPa |
Yield strength | 350-550 | MPa |
Density | 7700 | kg/m3 |
Quantity | Value | Unit |
---|---|---|
Thermal expansion | 41922 | e-6/k |
Thermal conductivity | 25-25 | W/m.k |
Specofic heat | 460-460 | J/kg.k |
Melting temperature | 1450-1510 | °C |
Density | 7700-7700 | kg/m3 |
Resistivity | 0.55-0.55 | ohm.mm2/m |
Annealing | Quenching | Tempering | Normalizing | Q&T |
---|---|---|---|---|
Minimum Order Quantity | 1 Kg |
Usage/Application | Automobile Industry |
Application | Automobile Industry, Construction |
Material | v |
Technique | NA |
Country of Origin | Made in India |
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Application | Construction, Automobile Industry |
Usage/Application | Construction, Automobile Industry |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
This is a higher carbon (0.30%) manganese steel in the plain carbon steel alloy family. It provides greater strength than the lower carbon grades while still retaining reasonable ductility.
Designation by Standards
Brand Name: Ck 30
Mat No1.1178
DIN Ck30
EN -
AISI 1030
Chemical Composition GradeMinMaxCarbon, C0.250.35Manganese, Mn0.600.90Silicon, Si0.150.35Sulfur, S-.--0.50Phosphorous, P-.--0.50 Applications
CK30 steel is generally used in the quenched and tempered condition for strength. Applications include machinery parts where strength and hardness are requisites.
Physical Properties(average values) at ambient temperature PropertiesMetricModulus of elasticity [10^3x N/mm2]200Density [lbs/in3]7.85Specific heat Capacity0.486Thermal Conductivity51.2 Soft Annealing
A full anneal is accomplished at 870 to 980°C followed by slow cooling in the furnace. A stress relief anneal may be done at 540°C.
Hardening
Heat treat at 810 to 870°C and water quench, followed by a tempering treatment.
Tempering
Temper, after heat treat and quench, at 320 to 540°C depending upon strength level desired
Forging
Hot forming temperature: 1050-850°C.
Machinabilty
Machinabilty of 0K30 steel is rated at 70% that of the AIS11112 steel considered to be 100% machinable as a reference.
Corrosion Resistance
This is a plain carbon steel and will rust unless protected.
Welding
CK30 steel may be welded by all methods. In heavy sections it is advisable to pre-heat at 150 to 260°C and post-heat at 540 to 650°C for welding.
Cold working
Cold working of CK30 steel in the annealed condition may be don by conventional methods. A fuU or stress relief anneal may be needed after cold working.
Mechanical Properties of grade C30 Nominal thickness (mm):0.3 - 3Rm - Tensile strength (MPa) (+A)520Nominal thickness (mm):0.3 - 3Rm - Tensile strength (MPa) (+CR)920Nominal thickness (mm):0.3 - 3A - Min. elongation Lo = 80 mm (%) (+A)20 Vickers hardness ( HV): (+CR)270 Vickers hardness ( HV): (+A)165
Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
CK35 steel has a higher (0.35%) carbon content for greater strength than the lower carbon alloys. It is hardenable by heat treatment, quench and tempering to develop 150 to 250 ksi tensile strength.
Designation by Standards
Element | Min | Max |
---|---|---|
Carbon, C | 0.30 | 0.40 |
Manganese, Mn | 0.60 | 0.90 |
Silicon, Si | 0.15 | 0.35 |
Sulfur, S | -.-- | 0.50 |
Phosphorous, P | -.-- | 0.50 |
Properties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 210 |
Density [lbs/in3] | 7.86 |
Component parts for automobile industry, e.g., shafts, forgings, flanges, bushings, crankshafts, connecting rods and parts for the machine building industry.
Soft AnnealingHeat to 650-700°C, cool slowly in furnace. This will produce a maximum Brinell hardness of 226.
NormalizingNormalizing temperature: 880-910°C.
TemperingTempering from the quenched condition may be done at 550-660°C depending upon the strength desired
Mechanical Properties in Normalized', Hardened+Tempered ConditionDiameter (mm) | 0.2 % proof stress (Wmm 2 ) | Tensile strength (Wmm 2 ) | Elongation A5 (%) | Reduction Z Impact (%) strength (J) | |
---|---|---|---|---|---|
Up to 16* | 300* | 480-670 | 21' | ||
17-100* | 270* | 480-670* | 21' | ||
101-160* | 245* | 460-650* | 19' | ||
Upto 16 | 430 | 630-780 | 17 | 40 | 40 |
17-40 | 370 | 600-750 | 19 | 45 | 40 |
41-100 | 320 | 550-700 | 20 | 50 | 40 |
Hot forming temperature: 1100-850°C.
MachinabilityMachinabilty is good, rated at 60% that of the AISI 1112 alloy used as a 100% machining rated steel.
Cold WorkingIn the annealed state the CK35 alloy is readily cold worked by conventional methods.
Corrosion ResistanceThis is a steel alloy and will rust if not protected. it is not corrosion resistant.
WeldingCK35 steel is weldable by all of the welding methods. However with its higher carbon content it is important to use both pre-heat at 150 to 260°C and post-heat at 590 to 650°C practice per an approved welding procedure.
Application | Automobile Industry, Construction |
Usage/Application | Automobile Industry, Construction |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
Description
1045 is a medium carbon steel is used when greater strength and hardness is desired than in the as rolled’ condition. Extreme size accuracy, straightness and concentricity combine to minimize wear in high speed applications. Turned, ground and polished.
Designation by Standards
Element | Min | Max |
---|---|---|
Carbon, C | 0.40 | 0.50 |
Manganese, Mn | 0.60 | 0.90 |
Silicon, Si | 0.15 | 1.35 |
Sulfur, S | -.-- | 0.50 |
Phosphorous, P | -.-- | 0.50 |
Properties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 190 - 210 |
Density [lbs/in3] | 7.84 |
Thermal Conductivity [W/m.K] | 15.1 |
20-100°C | 20-200°C | 20-300°C | 20-400°C | 20-500°C | 20-600°C | 20-700°C |
---|---|---|---|---|---|---|
11.6 | 12.3 | 13.1 | 13.7 | 14.2 | 14.7 | 15.1 |
Heat to 650-700°C, cool slowly. This will produce a maximum Brinell hardness of 207.
NormalizingNormalizing temperature (°C): 840-870°C.
TemperingTempering temperature: See the data below.
20°C | 50°C | 100°C | 150°C | 200°C | 250°C | 300°C |
---|---|---|---|---|---|---|
56 | 56 | 56 | 54 | 52 | 49 | 45.5 |
Diameter | Tensile Strength (MIDa) | Yield Strength (MPa) | Elongation Reduction (%) in Area (%) | |
---|---|---|---|---|
cold drawn, round bar (16-22 mm) | 655 | 585 | 12 | 35 |
cold drawn, round bar (32-50 mm) | 585 | 515 | 10 | 30 |
cold drawn, round bar (50 - 75mm) | 515 | 485 | 10 | 30 |
cold drawn, round bar (22-32 mm) | 620 | 550 | 11 | 30 |
cold drawn, round bar (19-32 mm) | 625 | 530 | 12 | 30 |
cold drawn, annealed, round bar (19-32 mm) | 585 | 505 | 12 | 45 |
cold drawn, high temperature, stress relieved, round bar (16-22 mm) | 655 | 515 | 15 | 45 |
cold drawn, high temperature, stress relieved, round bar (50-75 mm) | 550 | 450 | 12 | 35 |
cold drawn, high temperature, stress relieved, round bar (32-50 mm) | 585 | 485 | 15 | 40 |
cold drawn, high temperature, stress relieved, round bar (22-32 mm) | 620 | 515 | 15 | 40 |
cold drawn, low temperature, stress relieved, round bar (22-32 mm) | 655 | 585 | 11 | 30 |
cold drawn, low temperature, stress relieved, round bar (16-22 mm) | 690 | 620 | 12 | 35 |
cold drawn, low temperature, stress relieved, round bar (50-75 mm) | 585 | 515 | 10 | 25 |
cold drawn, low temperature, stress relieved, round bar (32-50 mm) | 620 | 550 | 10 | 30 |
hot rolled, round bar (19-32 mm) | 565 | 310 | 16 | 40 |
turned, ground and polished, round bar (19-32 mm) | 875 | 405 | 24 | 45 |
Application | Automobile Industry, Construction |
Usage/Application | Automobile Industry, Construction |
Density | Standard |
Grade | Standard |
Length | Standard |
Country of Origin | Made in India |
CK-50 is a Fe-Cr-Ni alloy containing slightly more chromium and considerably more nickel than the CH-20 grade. The alloy is used provides good resistance to dilute sulfuric acid and resists many co rodents more effectively Than CF-8 type. Chemical Composition
Component parts for vehicles, shafts, bushings, crankshafts, connecting rods and parts for the machine building industry and steel for axes, knives, hammers etc. ApplicationsComponent parts for vehicles, shafts, bushings, crankshafts, connecting rods and parts for the machine building industry and steel for axes, knives, hammers etc. Heat TreatmentSoft AnnealingHeat to 650-700°C, cool slowly. Hardness after annealingMax. 207 HB NormalizingNormalizing temperature (°C): 840-870°C. Thermal Properties
|
Application | Automobile Industry, Construction |
Usage/Application | Construction, Automobile Industry |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
Designation by Standards
Chemical Composition
Properties | Metric | Imperial |
---|---|---|
Density | 7.85 g/cc | 0.284 lb/in3 |
Properties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 210 |
Density [lbs/in3] | 7.85 |
Diameter | 0.2% proof stress | Tensile strength | Elongation A5 | Reduction Z |
---|---|---|---|---|
(mm) | (Wmm 2 ) | (Wmm2) | (%) | (%) |
up to 16* | 540 | 780-930 | 12 | 25 |
17-40 | 460 | 740-890 | 14 | 35 |
41-100 | 420 | 700-850 | 15 | 40 |
up to 16 | 430 | 630-780 | 17 | 40 |
Quantity | Value | Unit |
---|---|---|
Thermal expansion | 16 - 17 | e-6/K |
Thermal conductivity | 16 - 16 | W/m.K |
Specific heat | 500 - 500 | J/kg.K |
Melting temperature | 1370 - 1400 | °C |
Service temperature | 0 - 500 | °C |
Density | 8000 - 8000 | kg/m3 |
Resistivity | 0.7 - 0.7 | Ohm.mm2/m |
Properties | Conditions | ||
---|---|---|---|
T (°C) | Treatment | ||
Thermal Conductivity (W/m-K) | 42.7 | 100 | |
Specific Heat (J/kg-K) | 477 | 50-100 |
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Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
Description
CK60 steel is one of the higher carbon content (0.60%) steels. It is more difficult to fabricate than the lower carbon grades.
Designation by Standards
Grade | Min | Max |
---|---|---|
Carbon, C | 0.55 | 0.65 |
Manganese, Mn | 0.50 | 0.80 |
Silicon, Si | 0.15 | 0.35 |
Sulfur, S | -.-- | 0.50 |
Phosphorous, P | -.-- | 0.50 |
Shafts, bushings, connecting rods, Mechanical engineering components, agricultural hand tools, large forgings, springs, cold rolled strips.
Physical Properties(average values) at ambient temperatureProperties | Metric |
---|---|
Modulus of elasticity [10^3x N/mm2] | 210 |
Density [lbs/in3] | 7.85 |
Diameter (mm) | 0.2% proof stress (Wmm 2 ) | Tensile strength (Wmm 2 ) | Elongation (%) |
---|---|---|---|
up to 16 | 380 | 710 | 10 |
17-40 | 340 | 670 | 11 |
41-100 | 340 | 670 | 11 |
101-160 | 310 | 650 | 11 |
161-250 | 310 | 650 | 11 |
Diameter | 0.2% proof stress | Tensile strength | Elongation A5 | Reduction Z |
---|---|---|---|---|
(mm) | (Wmm 2 ) | (Wmm2) | (%) | (%) |
up to 16* | 580 | 850 -1000 | 11 | 25 |
17-40 | 520 | 800-950 | 13 | 30 |
41-100 | 450 | 750-900 | 14 | 35 |
101- 160 | - | - | - | - |
Heat to 650-700°C, cool slowly in furnace. This will produce a maximum Brinell hardness of 241.
HardeningHarden from a temperature of 800-830°C, 810-840°C followed by water or oil quenching.
NormalizingNormalizing temperature (°C): 820-850°C.
TemperingTempering temperature: 540-680°C.
ForgingHot forming temperature: 1100-850°C.
MachinabilityMachinability of CK60 and all of the higher carbon steels is relatively poor. CK60 rates at 55 to 60 % that of the AIS11112 steel which is considered 100% machinable
Corrosion ResistanceThis steel is not corrosion resistant, it will rust unless protected.
WeldingCK60 steel is weldable by all of the welding methods. However with its higher carbon content it is important to use both pre-heat at 150 to 260°C and post-heat at 590 to 650°C practice per an approved welding procedure.
Cold workingCold working is difficult even in the annealed condition although it may be done by conventional methods but requires greater force than the lower carbon steels.
Density | Standard |
Grade | Standard |
Length | Standard |
Material | Standard |
Modulus Of Elasticity | Standard |
Surface Treatment | Standard |
DIN 41Cr4 and DIN 42Cr
DIN 41Cr4 and DIN 42CrMo4 materials have been widely used in automotive driving elements. Although 42CrMo4 is more expensive than 41Cr4, it is more preferable in terms of material properties. In this study, these two materials were heat treated by austenitizing in a continuous furnace at 850 °C and quenched in oil at 90 °C. After they were tempered at various temperatures, mechanical properties were determined for each tempering temperature. The material properties for both materials were compared with each other. Results indicated that same mechanical properties for 41Cr4 and 42CrMo4 can be achieved by tempering 41Cr4 about 50 °C lower temperature than for 42CrMo4. In addition to the mechanical tests, fatigue tests were performed for both materials. Weibull distributions were plotted. Results indicated that 42CrMo4 had a longer life than 41Cr4 material.
Chemical CompositionProperties | Metric | Imperial |
---|---|---|
Hardness, Brinell (typical) | 300 | 33 |
Hardness, Rockwell C (typical) | 30 | 30 |
Tensile strength, ultimate | 965-1030 MPa | 140000-150000 psi |
Tensile strength, yield | 827-862 MPa | 120000-125000 psi |
Elongation at break (in 50 mm (2")) | 20.0% | 20.0% |
Compressive strength | 862 MPa | 125000 psi |
Charpy impact (V-Notch) | 27.1-33.9 J | 20.0-25.0 ft-lb |
Poisson's ratio | 0.27-0.30 | 0.27-0.30 |
Elastic modulus | 190-210 GPa | 27557-30457 ksi |
Hot forming | Narmalaizing+N | Quenching+Q | Quenching+Q | Tempering+T | Stress-relieving+SR | |
---|---|---|---|---|---|---|
1100-850 | 870air | 860 oil or polymer | 850 water | 540-680 | 50°C under the temperature | |
Soft annealing+A | Isothermal annealing+i | Spheroidizing annealing+AC | End Quench hardenability test | Pre heating welding | Stress-relieving after welding | |
720 air(HP max 241) | 820 fumace cooling to 670,then air (HB max 200) | 840 water | 300 | 550 fumace cooling | ||
Ac1 | Ac3 | Ms | Mf | |||
745 | 790 | 335 | 120 |
Dia Scope(mm) | Tensile Strength Rm (Mpa) | Yield Strength R2 (Mpa) | Elongation (longitudinal direction) Al (%) | Reduction of area (%) | Impact Energy Joules (-20°C) |
---|---|---|---|---|---|
16 max | 1100-1300 | 900 min | 10 min | 40 min | 30 min |
16-40 | 1000-1200 | 750 min | 11 min | 45 min | 35 min |
40-100 | 900-1100 | 650 min | 12 min | 50 min | 35 min |
100-160 | 800-950 | 650 min | 13 min | 50 min | 35 min |
160-250 | 750-900 | 500 min | 14 min | 55 min | 35 min |
Heat Treatment:
Heat to 1150°C Hold until uniform.Minimum forging temperature 850°C.Cool slowly in ashes or sand etc.
Application | Automobile Industry, Construction |
Usage/Application | Automobile Industry, Construction |
Surface Treatment | Standard |
Technique | Standard |
Thickness | Standard |
Country of Origin | Made in India |
CK40 steel has a higher (0.40%) carbon content for greater strength than the lower carbon alloys. It is hardenable by heat treatment, quench and tempering to develop 150 to 250 ksi tensile strength. Designation by Standards
Used for crankshafts, couplings and cold headed parts. Physical Properties(average values) at ambient temperature
Heat to 870-980°C, cool slowly in furnace. NormalizingNormalizing temperature: 890°C. ForgingHot forming temperature: 1100-850°C. MachinabilityMachinability is good,rated at 60 % that of the AIS11112 alloy steel which is considered 100% machinable Corrosion ResistanceThis is a steel alloy and will rust if not protected. it is not corrosion resistant WeldingCK40 steel is weldable by all of the welding methods. However with its higher carbon content it is important to use both pre-heat at 150 to 260°C and post-heat at 590 to 650°C practice per an approved welding procedure. TemperingTempering from the quenched condition may be done at 320-700°C depending upon the strength desired Cold WorkingIn the annealed state the CK 40 alloy is readily cold worked by conventional methods Mechanical Properties in Normalized', Hardened+Tempered Condition
|
Usage/Application | Construction |
Single Piece Length | 6 meter |
Test Certificate | Lab Tc |
Third Party Inspection Tip | Standard |
Thickness/Diameter | 2-3 inch |
Country of Origin | Made in India |
Ask for Price | Carbon Steel C 60 Description C 60 steel is one of the higher carbon content (0.60%) steels. It is more difficult to fabricate than the lower carbon grades. Chemical Composition
Shafts, bushings, connecting rods, Mechanical engineering components, agricultural hand tools, large forgings, springs, cold rolled strips. Physical Properties(average values) at ambient temperature
Heat to 650-700°C, cool slowly in furnace. This will produce a maximum Brinell hardness of 241. HardeningHarden from a temperature of 800-830°C, 810-840°C followed by water or oil quenching. NormalizingNormalizing temperature (°C): 820-850°C. TemperingTempering temperature: 540-680°C. ForgingHot forming temperature: 1100-850°C. MachinabilityMachinability of C 60 and all of the higher carbon steels is relatively poor. CK60 rates at 55 to 60 % that of the AIS11112 steel which is considered 100% machinable Corrosion ResistanceThis steel is not corrosion resistant, it will rust unless protected. WeldingC 60 steel is weldable by all of the welding methods. However with its higher carbon content it is important to use both pre-heat at 150 to 260°C and post-heat at 590 to 650°C practice per an approved welding procedure. Cold workingCold working is difficult even in the annealed condition although it may be done by conventional methods but requires greater force than the lower carbon steels. |