Jiangyin Jiangnan Metal Co., Ltd. Open-die forging factory, Jiangyin, Jiangsu, China +86 189 2135 9659 Request a quote

Heat-resistant nickel alloy forgings

1.4864 forgings

X12NiCrSi35-16 / Alloy 330 / AISI 330 / UNS N08330 (near equiv.) / Z12NCS35.16 / EN 10095

1.4864 is a heat-resistant austenitic nickel-iron-chromium alloy with roughly 35 % nickel, 16 % chromium and 1 to 2 % silicon, standardised in EN 10095. The silicon addition gives it resistance to oxidation, carburisation and nitridation at high temperature. Jiangyin Jiangnan Metal Co., Ltd., an open-die forging factory in Jiangyin, Jiangsu Province, China, forges 1.4864 into seamless rolled rings, shafts, flanges, discs, bars, sleeves and tube sheets, melted by EAF + VOD + ESR and supplied solution annealed with EN 10204 3.1 certificates.

Designations

1.4864 equivalents and related grades

1.4864 international designations and closely related heat-resistant grades
SystemDesignationNote
EN number1.4864Governing designation on this page
EN nameX12NiCrSi35-16EN 10095 chemical designation
UNSN08330Near equivalent, chromium range differs, see note below
AISI / SAE330Common North American designation
AFNORZ12NCS35.16French designation
Industry nameAlloy 330Also sold as RA330 and Incoloy 330, trade names of other producers
Related, higher Cr1.4886 / X10NiCrSi35-19Same family, about 19 % Cr
Related, Alloy DS1.4862 / X8NiCrSi38-18Higher Ni and Cr, sold as Alloy DS
Cast counterpart1.4806 / GX40NiCrSi35-17ASTM Grade HT for cast components

Chromium ranges differ between 1.4864 and N08330

EN 1.4864 specifies chromium at 15.0 to 17.0 %. UNS N08330 specifies 17.0 to 20.0 %. A heat certified to one will not automatically satisfy the other. State the governing specification on the purchase order, because the mill certificate is issued against that specification and not against the trade name.

Chemistry

Chemical composition of 1.4864

To EN 10095, 1.4864 contains max 0.15 % carbon, 1.00 to 2.00 % silicon, max 2.00 % manganese, 15.0 to 17.0 % chromium and 33.0 to 37.0 % nickel, with iron as the balance. Molybdenum, titanium, vanadium, tungsten and niobium are not specified elements in this grade.

Chemical composition, weight %, EN 1.4864 compared with UNS N08330
Element EN 1.4864 (X12NiCrSi35-16) UNS N08330 (Alloy 330)
C, Carbonmax 0.15max 0.08
Si, Silicon1.00 to 2.000.75 to 1.50
Mn, Manganesemax 2.00max 2.00
P, Phosphorusmax 0.045max 0.03
S, Sulphurmax 0.015max 0.03
Cr, Chromium15.0 to 17.017.0 to 20.0
Ni, Nickel33.0 to 37.034.0 to 37.0
Fe, Ironbalancebalance

Highlighted rows are where the two specifications diverge. EN 1.4864 limits per EN 10095. UNS N08330 limits per ASTM B511 / B535 / B536. Product analysis tolerances apply as given in the governing standard. Actual heat analysis is reported on the EN 10204 3.1 certificate.

Properties

Mechanical and physical data

Typical room-temperature values in the solution annealed condition. Actual values per heat appear on the certificate.

1.4864 typical properties, solution annealed
PropertyMetricImperial
Proof strength Rp0.2205 to 295 MPa30 to 43 ksi
Tensile strength Rm550 to 590 MPa80 to 85 ksi
Elongation A540 to 45 %40 to 45 % in 2 in
Hardness70 to 85 HRB70 to 85 HRB
Density8.08 g/cm³0.292 lb/in³
Max continuous serviceapprox. 1000 °Capprox. 1850 °F
StructureAustenitic, solid solution, not hardenable by heat treatment
Magnetic responseEssentially non-magnetic in the annealed condition
Silicon

Carburisation resistance

The 1 to 2 % silicon forms a stable protective scale that resists carbon pickup. This is the reason the grade is used for heat-treatment furnace fixtures and carburising boxes.

Nickel

No sigma embrittlement

At 33 to 37 % nickel the austenite stays stable through long high-temperature exposure, so the alloy resists sigma-phase embrittlement and chloride stress corrosion cracking.

Limitation

Modest strength at room temperature

Tensile strength is lower than most alloy steels. The grade is specified for high-temperature service, not for load-bearing duty at ambient temperature.

Processing

Forging window and heat treatment

1.4864 is hot worked between about 1150 °C and 950 °C. It must not be forged or bent between roughly 650 °C and 870 °C, where ductility is low and cracking is likely. Solution anneal after hot working.

1.4864 hot working temperature window Forging is carried out between 950 and 1150 degrees Celsius. The band between 650 and 870 degrees Celsius is a low-ductility zone where forging must not take place. Solution annealing is carried out between 1020 and 1120 degrees Celsius. 400 C 600 C 800 C 1000 C 1200 C WORKPIECE TEMPERATURE 650-870 DO NOT FORGE 950-1150 FORGE 1020-1120 ANNEAL
Reheat

Return to furnace below 950 °C

Once the piece drops below the finishing temperature, reheat it. Continuing into the low-ductility band is the most common cause of scrap in this grade.

Anneal

1020 to 1120 °C, cool fast

Solution anneal after hot working, then water quench or cool as fast as practical to below 425 °C. This restores the structure and oxidation resistance.

Heat treatment limit

No ageing treatment

1.4864 is a solid-solution alloy and cannot be precipitation hardened. A specification calling for solution plus ageing on this grade should be queried before production starts.

Product forms

1.4864 forgings we produce

All parts made to customer drawing. Supplied as-forged, rough-machined or finish-machined.

1.4864 forged product forms and dimensional envelope
FormOutside diameter Length / heightPiece weight
Seamless rolled rings200 to 2,000 mmup to 600 mm5 to 2,500 kg
Forged rings and flanges100 to 1,500 mmup to 500 mm2 to 1,800 kg
Shafts and spindles60 to 600 mmup to 4,000 mm5 to 3,000 kg
Round bars30 to 500 mmup to 4,000 mm1 to 2,000 kg
Discs, disks and tube sheets100 to 1,800 mmup to 400 mm thick3 to 2,500 kg
Sleeves and bushings80 to 900 mmup to 1,500 mm2 to 1,500 kg
Hollow bars and forged tube blanks100 to 800 mmup to 2,000 mm5 to 1,500 kg
Valve bodies, seat rings, nozzlesto drawingto drawing1 to 800 kg

Applications

Where 1.4864 forgings are used

The alloy is specified where a part must survive prolonged heat, thermal cycling and carburising atmospheres.

Heat treatment plant

Furnace fixtures, baskets, trays, muffles, carburising boxes, hangers, hooks and conveyor components that cycle through carburising and oxidising atmospheres.

Furnace and combustion hardware

Radiant tubes, combustion tubes, thermocouple sheaths, burner components and flare-stack tips exposed to alternating oxidising and reducing conditions.

Pressure vessels and heat exchangers

Forged tube sheets, flanges, nozzles and shell rings for shell-and-tube heat exchangers, air receivers, columns, towers, preheaters and process modules.

Valves

Forged valve bodies, stems, seat rings and blocks for ball, gate, globe, check and plug valves in high-temperature service.

Rotating equipment

Shafts and spindles for chemical pumps and plunger pumps, gas compressor parts, gear blanks and gas turbine components.

Oil, gas and offshore

Bushings, sleeves, discs and forged parts for subsea and deepwater production systems, wellhead and Christmas tree assemblies, industrial air compressors and nitrogen generators.

Cement, mining and mills

Forged crankshafts, nozzles and wear components for cement mills, sugar mills, concrete mills and mixers.

Heavy machinery and marine

Forged wheels, manifolds, rolls and eccentric shafts for shipbuilding, heavy machinery and processing units.

Pulp, paper and pharmaceutical

Forged rolls, crystalliser parts and process components for paper and pulp mills and pharmaceutical and biochemical plant.

Quality

Testing and certification

Inspection applied to 1.4864 forgings
TestStandardNote
Ultrasonic testingEN 10228-4Correct standard for austenitic forgings such as 1.4864
Ultrasonic testing, alternativeASTM A388, SEP 1921Applied where the order specifies them
Liquid penetrantASTM E165, EN ISO 3452-1Surface indications, correct method for non-magnetic grades
Chemical analysisASTM A751Heat and product analysis by spectrometer
TensileASTM A370, EN ISO 6892-1From prolongations representative of the part
HardnessASTM E18, EN ISO 6508Rockwell B for this grade
Grain sizeASTM E112After solution annealing
Intergranular corrosionASTM A262On request
CertificationEN 10204 3.1 / 3.23.2 endorsed by TUV, SGS, BV or Lloyd's Register

Magnetic particle testing does not apply to 1.4864. The alloy is essentially non-magnetic in the annealed condition, so liquid penetrant is used for surface examination.

Questions

1.4864 FAQ

What is 1.4864 material?

1.4864 is the EN material number for X12NiCrSi35-16, a heat-resistant austenitic nickel-iron-chromium alloy containing roughly 33 to 37 percent nickel, 15 to 17 percent chromium and 1 to 2 percent silicon, with iron as the balance. It is standardised in EN 10095 for heat-resisting steels and nickel alloys. The silicon addition gives it resistance to oxidation, carburisation and nitridation at high temperature, and the high nickel content makes it resistant to chloride stress corrosion cracking and to sigma-phase embrittlement.

Is 1.4864 the same as UNS N08330 or Alloy 330?

They are close equivalents but not identical. EN 1.4864 specifies chromium at 15.0 to 17.0 percent, while UNS N08330 specifies 17.0 to 20.0 percent, so a part ordered to N08330 will not automatically satisfy 1.4864 and the reverse is also true. Both are commonly sold under the industry name Alloy 330 and both are covered by the AISI 330 designation. State which specification governs on the purchase order, because the certificate is issued against that specification.

What is the chemical composition of 1.4864?

To EN 10095, 1.4864 contains carbon max 0.15 percent, silicon 1.00 to 2.00 percent, manganese max 2.00 percent, phosphorus max 0.045 percent, sulphur max 0.015 percent, chromium 15.0 to 17.0 percent, nickel 33.0 to 37.0 percent, with iron as the balance. Molybdenum, titanium, vanadium, tungsten and niobium are not specified elements in this grade.

Can 1.4864 be hardened by heat treatment?

No. 1.4864 is a solid-solution austenitic alloy and cannot be strengthened by quenching or by precipitation ageing. The only heat treatment applied is solution annealing, normally between 1020 and 1120 degrees Celsius followed by water quenching or the fastest practical cooling, which restores the structure after forging. Room-temperature strength can only be raised by cold work, which does not apply to most forged sections.

What is the forging temperature range for 1.4864?

1.4864 is hot worked between about 1150 and 950 degrees Celsius. The alloy must not be forged or bent between roughly 650 and 870 degrees Celsius, because ductility is low in that band and cracking is likely. Reheat rather than continue forging once the workpiece falls below the finishing temperature, and solution anneal after hot working to restore structure and corrosion resistance.

What are the mechanical properties of 1.4864 in the solution annealed condition?

Typical room-temperature values in the solution annealed condition are a 0.2 percent proof strength of 205 to 295 MPa, a tensile strength of 550 to 590 MPa, elongation of 40 to 45 percent, and a hardness of about 70 to 85 HRB. Density is approximately 8.08 grams per cubic centimetre. Actual values are reported on the mill test certificate for each heat.

Which ultrasonic testing standard applies to 1.4864 forgings?

Because 1.4864 is austenitic, the applicable European ultrasonic standard is EN 10228-4, which covers austenitic and austenitic-ferritic steel forgings. EN 10228-3 applies to ferritic and martensitic forgings and is not the correct choice for this grade. ASTM A388 and SEP 1921 are also used where the order specifies them. Jiangyin Jiangnan Metal states the standard and acceptance class on the works order and reports the result on the certificate.

What forms of 1.4864 forgings does Jiangyin Jiangnan Metal supply?

Jiangyin Jiangnan Metal forges 1.4864 into seamless rolled rings, forged rings, shafts, spindles, flanges, round bars, discs and disks, tube sheets, sleeves, bushings, valve bodies and seat rings, nozzles and forged tube blanks. Parts are supplied as-forged, rough-machined or finish-machined to the customer drawing, solution annealed, with EN 10204 3.1 certificates.

What is 1.4864 used for?

1.4864 is used where components must survive prolonged high temperature with thermal cycling and carburising atmospheres. Typical applications are heat-treatment furnace fixtures, baskets and muffles, radiant and combustion tubes, thermocouple sheaths, flare-stack tips, carburising boxes, gas turbine and compressor parts, heat exchanger and pressure vessel components, salt pots, and rotating parts in chemical and plunger pumps.

How do I order 1.4864 forgings and how long does it take?

Send a drawing or dimensions, the governing specification (EN 1.4864 or UNS N08330), the quantity, the supply condition, the ultrasonic testing standard and acceptance class, and the certificate level to sales@steelforgepieces.com. A quotation is issued within 24 working hours. There is no minimum order quantity because open-die forging requires no part-specific tooling.

Contact

Quote a 1.4864 forging

Send a drawing or dimensions. Tell us which specification governs, EN 1.4864 or UNS N08330, because the two have different chromium ranges and the certificate is issued against whichever you name.

Also include quantity, supply condition, UT standard and acceptance class, and certificate level. Quotations are issued within 24 working hours.

Company Jiangyin Jiangnan Metal Co., Ltd. Factory address No.1 Chengxiqiao Road, Zhouzhuang Town,
Jiangyin City, Jiangsu Province, 214423, China Telephone, WhatsApp, WeChat +86 189 2135 9659 Email sales@steelforgepieces.com Working hours Monday to Saturday, 08:00 to 18:00 (GMT+8)