Wholesale price stable quality EN DIN 34CrNiMo6 | 1.6582 | 4337 Engineering Steel in Portugal
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...
It adheres to the tenet "Honest, industrious, enterprising, innovative" to develop new products constantly. It regards customers, success as its own success. Let us develop prosperous future hand in hand for Wholesale price stable quality EN DIN 34CrNiMo6 | 1.6582 | 4337 Engineering Steel in Portugal, Please send us your specifications and requirements, or feel free to contact us with any questions or inquiries that you may have.
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 educational video explains flush rivet construction of aluminum aircraft air-frames. It shows the flush rivet method on aircraft to reduce unnecessary aerodynamic drag increasing performance and efficiency in flight. Additional post-installation machining may be performed to perfect the airflow. Before being installed, a rivet consists of a smooth cylindrical shaft with a head on one end. The end opposite the head is called the tail. On installation the rivet is placed in a punched or drilled hole, and the tail is upset, or bucked (i.e., deformed), so that it expands to about 1.5 times the original shaft diameter, holding the rivet in place. In other words, pounding creates a new “head” on the other end by smashing the “tail” material flatter, resulting in a rivet that is roughly a dumbbell shape. To distinguish between the two ends of the rivet, the original head is called the factory head and the deformed end is called the shop head or buck-tail.
To learn more about rivets, goto:
HOW IT WORKS playlist:
http://www.stainless-steel-india.com/ The Aesteiron Steels is an ISO 9001:2008 certified company, offering a wide of Stainless Steel products. Over the past decade, We have become a market leader and trailblazer in the Industrial Raw Materials business.
Began in 1983 by purchasing and selling stainless steel bars from a small office in Toronto, Ontario. Since that time, we have grown into one of Canada’s leading distributors of specialty metal products with five branches strategically located across the country.
We have total spectrum of trading, stockholding and processing activities in Stainless Steel, Carbon Steel, nickel Alloy, Alloy Steel, Copper, Brass, Monel, Inconel, Aluminium, Hastalloy, Lead in the shape of Pipes, Tubes, Rods, Sheets, Plates, Wires, Angles, Coils, Strips and the entire range of Pipes Fittings such as BW/ SW/ Screwed/ Forged & Compression Type with Ferrules such as Elbow, Tees, Reducers, Stub ends, Flanges, Unions, Caps, Nipples, Couplings, Elbowlets, Sockolets, Weldolets, Nuts, Bolts, Studs, Washers etc.
Knowledgeable and experienced sales specialists, with support from our staff metallurgist are eager to respond to all inquiries including those hard to find aircraft items. In addition, when non-standard requirements are creating a problem, let ASA / Magna support your efforts by providing the following services.
Our basic objective of developing business both In India and aboard by maintaining the quality of the products, ensuring price competitiveness and enhancing service standards still remain the same. We are proud to offer our customers a large selection of materials in various forms and sizes readily available from our inventory. Our Major markets are Australia/NZ, Caribbean, Central America, East Europe, South America, East/Middle Africa and Indian Subcontinent.