1.8916
1.8916 properties and heat treatment forged piece, Including 1.8916 application and specifications, We have all specifications，Including 1.8916 steel plate, 1.8916 sheet, 1.8916 square steel, 1.8916 flat bar,1.8916 round bar,1.8916 forgings, we can own production and sales.
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forged/hot rolling/ extrusion of steel
We can produce the 1.8916 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 1.8916 and Standards
| Grade : | S460QL1 |
| Number: | 1.8916 |
| Standard: | EN 10025 - 6 : 2004 Technical delivery conditions for flat products of high yield strength structural steels in the quenched and tempered condition |
| Classification: | High yield strength structural steels in the quenched and tempered condition |
| Nominal thickness =< 50(mm) CEV max = 0.47 Nominal thickness from 50 to 100 (mm) CEV max = 0.48 Depending on the thickness of the product and the manufacturing conditions, the manufacturer may add to the steel one or several alloying elements up to the maximum values given in order to obtain the specified properties Nb, Ti, V, Zr: There shall be at least 0.015% of a grain-refining element present. AL is also one of these elements. The minimum content of 0.015% applies to soluble aluminium, this value is regarded as attained if the total aluminium content is at least 0.018%; in case of dispute the soluble aluminium content shall be determined |
| C | Si | Mn | Ni | P | S | Cr | Mo | V | N | Nb | Ti | Cu | Zr | B | CEV |
| max 0.2 | max 0.8 | max 1.7 | max 2 | max 0.02 | max 0.01 | max 1.5 | max 0.7 | max 0.12 | max 0.015 | max 0.06 | max 0.05 | max 0.5 | max 0.15 | max 0.005 | max 0.5 |
| Temperature | -60 | -40 | -20 | 0 |
| Notch impact test. Min. absorbed energy | 30 | 40 | 50 | 60 |
| Nominal thickness (mm) | 3 - 50 | 50 - 100 | 100 - 150 |
| ReH - Minimum yield strength (MPa) | 460 | 440 | 400 |
| Nominal thickness (mm) | 3 - 50 | 50 - 100 | 100 - 150 |
| Rm -Tensile strength (MPa) | 550-720 | 550-720 | 500-670 |
| Nominal thickness (mm) | - |
| A - Minimum elongation Lo = 5,65 √ So (%) | 17 |
Equivalent grades of grade S460QL1 (1.8916)
| Germany DIN,WNr |
France AFNOR |
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Machining performance
Download 1.8916 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.