1.8959
1.8959 properties and heat treatment forged piece, Including 1.8959 application and specifications, We have all specifications，Including 1.8959 steel plate, 1.8959 sheet, 1.8959 square steel, 1.8959 flat bar,1.8959 round bar,1.8959 forgings, we can own production and sales.
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forged/hot rolling/ extrusion of steel
We can produce the 1.8959 has the following specifications:
Round bar steel: 1mm to 3000mm
Square-shape steel: 1mm to 2000mm
Plate steel:0.1mm to 2500mm
Width: 10mm to 2500mm
Lenth: We can supply any lenth based on the customer's requirement.
Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes
Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.
Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement
Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement
Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.
Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirementExcellent service for all kinds of industries,with advantages of technologies, equipment and price.
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Chemical composition % of the ladle analysis of grade 1.8959 and Standards
| Grade : | S355J0W |
| Number: | 1.8959 |
| Standard: | EN 10025 - 5 : 2004 Technical delivery conditions for structural steels with improved atmospheric corrosion resistance. |
| Classification: | Structural steels with improved atmospheric corrosion resistance |
| Method of deoxidation FN = rimming steels not permitted For long products the P and S content can be 0.005% higher The steels may show a Ni content of max. 0,65 % It is permissible to exceed the specified values provided that for each increase of 0,001 % N the P max. content will be reduced by 0,005 %; the N content of the ladle analysis, however, shall not be more than 0,012 % The steels may contain max. 0,30 % Mo and max. 0,15 % Zr The max. value for nitrogen does not apply if the chemical composition shows a minimum total Al content of 0,020 % or if sufficient other N binding elements are present |
| C | Si | Mn | P | S | Cr | N | Cu | CEV |
| max 0.16 | max 0.5 | 0.5 - 1.5 | max 0.035 | max 0.035 | 0.4 - 0.8 | max 0.009 | 0.25 - 0.55 | max 0.52 |
| Temperature | -20 | 0 |
| Notch impact test. Min. absorbed energy | 27 | 27 |
| Nominal thickness (mm) | to 16 | 16 - 40 | 40 - 63 | 63 - 80 | 80 - 100 | 100 - 150 |
| ReH - Minimum yield strength (MPa) | 355 | 345 | 335 | 325 | 315 | 295 |
| Nominal thickness (mm) | to 3 | 3 - 100 | 100 - 150 |
| Rm -Tensile strength (MPa) | 510-680 | 470-630 | 450-600 |
| Nominal thickness (mm) | 3 - 40 | 40 - 63 | 63 - 100 | 100 - 150 |
| A - Minimum elongation Lo = 5,65 √ So (%) | 22 | 21 | 20 | 18 |
| Nominal thickness (mm) | 1.5 - 2 | 2 - 2.5 | 2.5 - 3 |
| A - Minimum elongation Lo = Lo = 80 mm (%) | 16 | 17 | 18 |
Equivalent grades of grade S355J0W (1.8959)
| France AFNOR |
England BS |
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Machining performance
Download 1.8959 the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>
Principal Design Features
One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.
Machinability
Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.
Heat Treatment
CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.
Welding
Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.
Forging
Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.