Super Purchasing for EN DIN 34CrNiMo6 | 1.6582 | 4337 Engineering Steel Manufacturer in Bogota
EN 34CrNiMo6 Steel is an important alloy engineering steel grade as per BS EN10083-3:2006. 34CrNim06 steel has high strength, high toughness and good hardenability. EN / DIN 34CrNiMo6 alloy steel has the stability ofresistance to overheating, but the white sensitivity of 34CrNiM06 ishigh. It also has the temper brittleness, so the weldability of34CrNiMo6 material is poor. The steel 34CrNiMo6 needs the hightemperature preheating before welding in order to eliminate the stressafter welding pr...
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is an important alloy engineering steel grade as per BS EN
10083-3:2006. 34CrNim06 steel has high strength, high toughness and good
hardenability. EN / DIN 34CrNiMo6 alloy steel has the stability of
resistance to overheating, but the white sensitivity of 34CrNiM06 is
high. It also has the temper brittleness, so the weldability of
34CrNiMo6 material is poor. The steel 34CrNiMo6 needs the high
temperature preheating before welding in order to eliminate the stress
after welding processing.
1.EN Steel 34CrNiMo6 Supply Range
Round Steel Bar Sizes: diameter 80mm – 1200mm
Other steel shape and sizes available according to your requirements.
Surface finish: Black, machined, peeled, turned or according to other customers’ pecial requirements.
2.EN 34CrNiMo6 Steel Standards And Equivalents
|BS EN 10083 -3: 2006||34CrNiMo6 / 1.6582||: 2004||4337|
|BS EN 10250 – 3: 2000|
3. EN/DIN 34CrNiMo6 Steel Chemical Composition Properties
|BS EN 10083 – 3:2006||34CrNiMo6
|0.30-0.38||0.5-0.8||0.40 max||0.025 max||0.035 max||1.3-1.7||0.15-0.30||1.3-1.7|
|BS EN 10250-3:2000||C||Mn||Si||P||S||Cr||Mo||Ni|
|0.30-0.38||0.5-0.8||0.40 max||0.035 max||0.035 max||1.3-1.7||0.15-0.30||1.3-1.7|
|ASTM A29: 2004||4337||C||Mn||Si||P||S||Cr||Mo||Ni|
|0.30-0.40||0.6-0.8||0.20-0.35||0.035 max||0.040 max||0.70-0.90||0.20-0.30||1.65-2.00|
4.Mechanical Properties of EN/DIN 34CrNiM06 / 1.6582 Alloy Steel
|Properties||< 16||>16 – 40||>40 – 100||>100 – 160||>160 – 250|
|Thickness t [mm]||< 8||8<t<20||20<t<60||60<t<100||100<t<160|
|Yield strength Re [N/mm²]||min. 1000||min. 900||min. 800||min. 700||min. 600|
|Tensile strength Rm [N/mm2]||1200 – 1400||1100 – 1300||1000 – 1200||900 – 1100||800 – 950|
|Elongation A [%]||min. 9||min. 10||min. 11||min. 12||min. 13|
|Reduction of area Z [%]||min. 40||min. 45||min. 50||min. 55||min. 55|
|Toughness CVN [J]||min. 35||min. 45||min. 45||min. 45||min. 45|
5.Heat Treatment of 34CrNiMo6 Engineering Steel
Quenched and Tempered (Q+T) of 34CrNiMo6 Steel
Heat 34CrNiMo6 round steel slowly to the temperature of 850°C;
Soak at this hardening temperature quench in oil;
Temper as soon as 34CrNiMo6 steels reach room temperature.
Heat uniformly to the suitable temperature;
Withdraw from the furnace and cool in the air.
The usual tempering temperature is 600°C which depending on the actual requirements.
6.Forging of DIN 34CrNiMo6 / 1.6582 Steel
Hot forming temperature: 1100-900oC.
7.Machinability of Steel 34CrNiMo6
is best done with this 1.6582 alloy steel in the annealed or normalized
and tempered condition. It can be machined by all conventional methods.
alloy materials can be fusion or resistance welded. Preheat and post
heat weld procedures should be followed when welding this alloy by
34CrNiMo6 steel is used to make tools which demands good plasticity and
high strength. It is usually selected to make the big size and important
parts, such as heavy machinery axle,turbine shaft blade, high load of
transmission parts, fasteners, crank shafts, gears, as well as heavily
loaded parts for motor construction etc.
Otai Steel is reliable to
supply engineering 34CrNiMo6 steels / 1.6582 engineering alloy steels.
Please tell us your detailed requirements and have the best offer soon.
This Steel Detailing project involved the modification and renovation of 3 Hangars to accommodate maintenance of a C130 Hercules Aircraft.
The scope included a roof replacement on three hangar buildings, 6 new interior mezzanines with handrail & ladders, 6 new stair towers with pivoting walk bridges for aircraft access, plus 3 new 160′ foot long box trusses and supporting tower structures for the new MegaDoors.
Embedded into this video is a rendered and animated portion of our sds/2 model showing the pivoting and articulating aircraft access platform.
Steel Detailing: Yes
Music by: Bensound
Title: Dream ambient track
The Thompson Creek molybdenum mine, owned and operated by the Thompson Creek Mining Company (TCMC), is 20 miles southwest of Challis, Idaho. The mine is the fourth largest primary molybdenum mine in the world, producing approximately 5 percent (up to 15 percent in the past) of the world molybdenum supply. TCMC is the largest employer in Custer County, with approximately 375 employees. Typically, the mine accounts for one out of every five jobs in Custer County, 45 percent of wages and salaries in Custer County, and $114 million of Idaho’s total personal income. Most of the molybdenum produced from the mine is used as an alloy to make high-strength and corrosion-resistant steel.
The mine has been in operation since 1981 and is permitted for approximately 3,400 acres of surface disturbance, of which approximately 2,300 acres are on private land and approximately 1,100 acres are on BLM administered and National Forest System lands