DILLIMAX 965 Tough (EN 1.8933)

DILLIMAX 965 is preferentially used for welded steel structures within mechanical constructions, plant constructions and structural steel works, such as machines for structural engineering, conveying plants, hoists and cranes.

Cold forming means forming below 560 °C (1040 °F). DILLIMAX 965 can be cold formed with regard to its high yield strength. Flame cut or sheared edges in the bending area should be ground before cold forming. Cold forming is related to a hardening of the steel and to a decrease in toughness. Some codes may limit the maximum permissible strain during cold forming. Depending on the relevant code this can result in the need of larger bending radiuses than indicated in the chart. For larger cold forming amounts we recommend you to consult the steel producer prior to ordering.

During the processing, the necessary safety measures have to be taken, so that nobody will be exposed to a danger by a possible fracture of the work piece during the forming process. The following geometries can usually be achieved by cold forming without the formation of surface defects (t is the plate thickness):

Water quenched and tempered according to EN 10025-6.

General technical delivery requirements: Unless otherwise agreed, the general technical delivery requirements in accordance with EN 10021 apply.

Due to its high yield strength, DILLIMAX 965 requires special care during plate processing.

For flame cutting, the following minimum preheating temperatures are recommended: 50 °C (122 °F) for plate thickness up to 20 mm (0.8 in.), 100 °C (212 °F) for plate thickness up to 50 mm (2 in.) and 150 °C (302 °F) for thicker plates.

For general welding instructions, please consult the EN 1011. In order to ensure that the tensile strength of the weld metal fulfils the requirements of the base metal, the heat input and interpass temperature must be limited during welding. Experience has shown that the welding conditions should be chosen so that the cooling time t8/5 does not exceed 8 seconds. This is applicable when using suitable filler materials of a corresponding yield strength class.

The high yield strength of the base material must be taken into account when choosing the filler materials. It should be considered that increased heat input leads to lower tensile properties in the weld metal. If a stress relieving heat treatment is planned during or after plate processing, this must also be considered when selecting the filler materials. To avoid hydrogen-induced cold cracking, only filler materials, which add very little hydrogen to the base metal, may be used. Therefore, shielded arc welding should be preferred. For manual arc welding, electrodes with basic coating (type HD < 5 ml/100 g in accordance with ISO 3690) and dried according to the manufacturer’s instructions should be used. With increasing plate thickness, increasing hydrogen charge and restraint of the weld, a soaking for hydrogen effusion immediately after welding is recommended.

If particular 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 technical data sheet is a product description. This material data sheet is updated at irregular intervals. The current version is available from the mill or as download at www.dillinger.de.

A stress relief heat treatment can be performed at a maximum temperature of 560 °C (1040 °F) and maximum holding time of 60 minutes without significant impairment of the properties. After a stress relief heat treatment using the specified parameters, the requirements for mechanical and technological properties are met. It has to be specified prior to ordering if higher stress relieving temperatures or longer holding times have to be applied. The verification of appropriate stress relieving parameters for a delivered plate may be possible on request. Detailed instructions for flame cutting, welding, machining and about the structural properties of DILLIMAX are provided in the technical information.

If the temperature of about 560 °C (1040 °F) is exceeded, the initial tempering can be altered so that the mechanical properties are affected. To regain the initial properties new quenching and tempering become necessary. In this respect we recommend you to contact the steel producer prior to ordering, in all cases where hot forming at higher temperatures is required.

Finally, it is the fabricator’s responsibility to obtain the required values of the steel through an appropriate heat treatment.

DILLIMAX 965 can be delivered in thicknesses from 6 to 125 mm (1⁄4 to 4.9 in.) according to the dillinger dimensional programme.

For DILLIMAX 965, under the designations DILLIMAX 965 B/S960Q, DILLIMAX 965 T/S960QL and DILLIMAX 965 E/S960QL1, a CE marking according to EN 10025-1 is applied in thicknesses up to 125 mm (4.9 in.), unless otherwise agreed.

Identification of plates: Unless otherwise agreed, the marking is carried out via steel stamps with at least the following information:

The steel is fine grained through sufficient aluminium content.

The entire processing and application techniques are of fundamental importance to the reliability of products 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 of the EN 1011 (welding) and CEN/TR 10347 (forming) as well as recommendations regarding job safety in accordance with national rules should be observed.

Surface quality: Unless otherwise agreed, the specifications will be in accordance with EN 10163-2, class A2.

Ultrasonic testing: If not agreed otherwise, DILLIMAX 965 fulfils the requirements of class S1E1 in accordance with EN 10160.

Tensile and impact tests will be performed according to EN 10025-6 once per heat and 60 t. Tests on every heat treatment unit may be possible on request. The test pieces are taken and prepared according to parts 1 and 6 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. Tensile tests according to ASTM A370 may be agreed. The impact test will be carried out on longitudinal Charpy-V-specimens in accordance with EN ISO 148-1 using a 2 mm striker. Unless otherwise agreed, the test results are documented in an inspection certificate 3.1 in accordance with EN 10204.

Tensile test at ambient temperature – transverse test pieces