General
Property | Value | Comment | |
---|---|---|---|
Carbon equivalent (CET) | 0.29 [-] Show Supplier Material materials with Carbon equivalent (CET) of 0.29 [-] | typical value for thickness 20 < t ≤ 50 mm | |
Carbon equivalent (CEV) | 0.47 [-] Show Supplier Material materials with Carbon equivalent (CEV) of 0.47 [-] | typical value for thickness 20 < t ≤ 50 mm | |
0.49 [-] Show Supplier Material materials with Carbon equivalent (CEV) of 0.49 [-] | max. value for thickness 20 < t ≤ 50 mm | ||
Carbon equivalent note | CEV = C + Mn/6 + (Cr+Mo+V)/5 + (Cu+Ni)/15 and CET = C + (Mn+Mo)/10 + (Cr+Cu)/20 + Ni/40 |
Mechanical
Property | Temperature | Value | Comment |
---|---|---|---|
Charpy impact energy, V-notch | -20 °C | 20 J Show Supplier Material materials with Charpy impact energy, V-notch of 20 J | average of 3 tests | longitudinal/transverse specimens |
-20 °C | 40 J Show Supplier Material materials with Charpy impact energy, V-notch of 40 J | average of 3 tests | longitudinal/transverse specimens | |
-10 °C | 24 J Show Supplier Material materials with Charpy impact energy, V-notch of 24 J | average of 3 tests | longitudinal/transverse specimens | |
-10 °C | 43 J Show Supplier Material materials with Charpy impact energy, V-notch of 43 J | average of 3 tests | longitudinal/transverse specimens | |
0 °C | 27 J Show Supplier Material materials with Charpy impact energy, V-notch of 27 J | average of 3 tests | longitudinal/transverse specimens | |
0 °C | 47 J Show Supplier Material materials with Charpy impact energy, V-notch of 47 J | average of 3 tests | longitudinal/transverse specimens | |
Elongation | 16 % Show Supplier Material materials with Elongation of 16 % | min. for plate thickness 20 < t ≤ 50 mm | transverse specimens, A5 | |
Tensile strength | 640 - 820 MPa Show Supplier Material materials with Tensile strength of 640 - 820 MPa | for plate thickness 20 < t ≤ 50 mm | transverse specimens | |
Yield strength | 550 MPa Show Supplier Material materials with Yield strength of 550 MPa | min. ReH for plate thickness 20 < t ≤ 50 mm | transverse specimens |
Chemical properties
Property | Value | Comment | |
---|---|---|---|
Aluminium | 0.02 % Show Supplier Material materials with Aluminium of 0.02 % | min. | |
Carbon | 0.09 % Show Supplier Material materials with Carbon of 0.09 % | max. | |
Chromium | 0.3 % Show Supplier Material materials with Chromium of 0.3 % | max. | |
Copper | 0.5 % Show Supplier Material materials with Copper of 0.5 % | max. | |
Iron | Balance | ||
Manganese | 1 - 2 % Show Supplier Material materials with Manganese of 1 - 2 % | ||
Molybdenum | 0.3 % Show Supplier Material materials with Molybdenum of 0.3 % | max. | |
Nickel | 0.8 % Show Supplier Material materials with Nickel of 0.8 % | max. | |
Niobium | 0.06 % Show Supplier Material materials with Niobium of 0.06 % | max. | |
Nitrogen | 0.025 % Show Supplier Material materials with Nitrogen of 0.025 % | max. | |
Phosphorus | 0.02 % Show Supplier Material materials with Phosphorus of 0.02 % | max. | |
Silicon | 0.15 - 0.55 % Show Supplier Material materials with Silicon of 0.15 - 0.55 % | ||
Sulfur | 0.005 % Show Supplier Material materials with Sulfur of 0.005 % | max. | |
Titanium | 0.025 % Show Supplier Material materials with Titanium of 0.025 % | max. | |
Vanadium | 0.08 % Show Supplier Material materials with Vanadium of 0.08 % | max. |
Technological properties
Property | ||
---|---|---|
Cold Forming | With regard to its high toughness, DI-MC 550 can generally be well cold formed, i.e. at temperatures below 580 °C. Cold forming is always related to a hardening of the steel and to a decrease in toughness. This change in the mechanical properties can in general be partially recovered through a subsequent stress relief heat treatment. Flame cut or sheared edges in the bending area should be ground before cold forming. For larger cold forming degrees we recommend consulting us prior to ordering. | |
Delivery condtion | DI-MC 550 can be delivered: DI-MC 550 can be delivered in thickness from 20 to 50 mm according to the dimensional program. Unless otherwise agreed, the general technical delivery requirements in accordance with EN 10021 apply. | |
Flame cutting and welding | DI-MC 550 can be flame cut in all thickness ranges without preheating. Plasma and laser cutting can also be carried out without preheating for typical thickness. DI-MC 550 has an excellent weldability if the general technical rules are observed (EN 1011 has to be applied analogously). The risk of cold cracking is low. The choice of the appropriate preheating temperature depends on the construction, plate thickness, welding heat input, chosen welding process, welding filler materials and base materials (basic quality B and low temperature quality T). From experience, an appropriate choice of these parameters allows omitting the preheating. To avoid hydrogen induced cold cracking, only filler materials, which add very little hydrogen to the base metal, may be used (up to 5 ml/100 g DM according to ISO 6390). The low content of carbon and other alloy elements leads to favourable toughness properties in the heat affected zone, even with high heat inputs. Depending on the chosen welding process, welding filler material as well as toughness requirements in the heat affected zone, it permits cooling temperatures (t8/5) above the limiting values of 25 s as stated in EN 1011-2 and SEW 088. | |
Flame straightening | For thermomechanically rolled steel the report CEN/TR 10347 recommends maximum flame straightening temperatures. | |
General note | If special requirements which are not covered in this material data sheet are to be met by the steel due to its intended use or processing, these requirements are to be agreed before placing the order. The information in this data sheet is a product description. This data sheet is updated at irregular intervals. The current version is relevant. The current version is available from the mill or as download at www.dillinger.de. | |
Heat Treatment | Welded joints of DI-MC 550 are usually used in welded condition. If a stress relief heat treatment is necessary, it is carried out in the temperature range between 530 and 580 °C with cooling in air. The holding time should not exceed 1,5 hours (even if multiple operations are carried out). For particular heat treatment requirements we recommend consulting us prior to ordering. | |
Hot forming | Hot forming, i.e. forming at temperatures above 580 °C, leads to changes in the original material condition. It is impossible to re-establish the same material properties that had been achieved during the original manufacture through a further treatment. Therefore hot forming is not permitted. | |
Options | 1) The impact properties and the tensile properties shall be verified for each mother plate. | |
Other | Identification: Unless otherwise agreed, the marking is carried out via steel stamps with at least the following information: | |
Processing methods | The entire processing and application techniques are of fundamental importance to the reliability of the parts and assemblies made from this steel. The user should ensure that his design, construction and processing methods are aligned with the material, correspond to the state-of-the-art that the fabricator has to comply with and are suitable for the intended use. The customer is responsible for the selection of the material. The recommendations in accordance with EN 1011 and SEW 088 should be observed. | |
Surface condition | Unless otherwise agreed, the specifications will be in accordance with EN 10163, class A2. | |
Testings | Tensile test and impact tests are carried out once per heat, 60 t and thickness range as specified for the yield strength according to table 5 of EN 10025-4. Tests on every mother plate are possible on request (see option 1). The test pieces are taken and prepared according to part 1 and 4 of EN 10025. The tensile test is carried out on specimens of gauge length Lo = 5.65⋅√So respectively Lo = 5⋅do, in accordance with EN ISO 6892-1. The impact test will be carried out on Charpy-V-specimens in accordance with EN ISO 148-1 using a 2 mm striker. Unless otherwise agreed, the test will be performed according to EN ISO 148-1 at a temperature of -20 °C for the basic quality B and at -50 °C for the low temperature quality T on longitudinal test pieces. Unless otherwise agreed, the test results are documented in a certificate 3.1 in accordance with EN 10204. Unless otherwise agreed, DI-MC 550 meets the requirements of class S1E1 in accordance with EN 10160. | |
Tolerances | Unless otherwise agreed, tolerances are in accordance with 10029, with class A for the thickness. Flatness deviation may be agreed on request. |