Nickel superalloy · Werkstoff 2.4952 · UNS N07080
2.4952 Forgings (Nimonic 80A / Alloy 80A / UNS N07080)
Jiangyin Jiangnan Metal Co., Ltd. forges 2.4952 (NiCr20TiAl) into seamless rolled rings, flanges, shafts, discs, sleeves, bushings, tube sheets, hollow bars and round bars. Parts leave the works solution treated and aged, with EN 10204 3.1 or 3.2 certification.
What is 2.4952?
2.4952 is the European material number (Werkstoff-Nr.) for NiCr20TiAl, an age-hardenable nickel-chromium superalloy known commercially as Nimonic 80A or Alloy 80A and designated UNS N07080. It carries 19.0-21.0 % chromium, 2.0-2.6 % titanium and 1.10-1.70 % aluminium, with nickel as the balance. Titanium and aluminium form a gamma-prime precipitate during ageing, and that precipitate is what separates 2.4952 from the softer, solid-solution Nimonic 75.
The alloy holds tensile and creep-rupture strength to about 815 °C (1500 °F) and stands up to oxidation and sulphur-bearing combustion gas. It goes into gas turbine blades, rings and discs, turbine bolting, nuclear boiler tube supports and exhaust valves for large diesel engines.
- Werkstoff: 2.4952 (also 2.4631)
- UNS: N07080
- DIN name: NiCr20TiAl
- Trade names: Nimonic 80A, Alloy 80A
- Density: 8.19 g/cm³ (0.296 lb/in³)
- Max service temperature: 815 °C (1500 °F)
- Tensile strength, aged: 1250 MPa (181,000 psi) typical
- Hot working range: 1050-1200 °C
2.4952 equivalent grades and standards
The same alloy is ordered under six or seven names, depending on the country the drawing came from. Every designation below refers to one composition, and we take orders against any of them.
| System | Designation | Notes |
|---|---|---|
| Werkstoff-Nr. (DIN/EN) | 2.4952 | 2.4631 covers the same composition |
| DIN chemical name | NiCr20TiAl | DIN 17742, DIN 17754 |
| UNS (USA) | N07080 | ASTM B637 / ASME SB-637 |
| Trade name | Nimonic 80A | Alloy 80A is the generic form |
| British Standard | BS 3076 NA20, HR1, HR201, HR401, HR601 | Bar, sheet, forgings |
| AFNOR (France) | NC20TA | - |
| JIS (Japan) | NCF 80A | - |
| Aerospace | MSRR 7011, AECMA prEN 2188-2190 | Confirm the exact release requirement at enquiry |
| European standard | EN 10302 | Creep-resisting steels, nickel and cobalt alloys |
Use a cross-reference for identification only. State the standard, revision, heat-treatment condition and acceptance criteria on the purchase order.
Chemical composition of 2.4952
Composition is held to the DIN 17742 limits below. Where a customer orders to ASTM B637 / UNS N07080 instead, the wider limits in the right-hand column apply.
| Element | 2.4952 min. % | 2.4952 max. % | UNS N07080 (ASTM B637) |
|---|---|---|---|
| Carbon (C) | 0.04 | 0.09 | ≤ 0.10 |
| Chromium (Cr) | 19.0 | 21.0 | 18.0 - 21.0 |
| Nickel (Ni) | Balance | Balance | Balance |
| Titanium (Ti) | 2.00 | 2.60 | 1.8 - 2.7 |
| Aluminium (Al) | 1.10 | 1.70 | 1.0 - 1.8 |
| Iron (Fe) | - | 1.00 | ≤ 3.0 |
| Manganese (Mn) | - | 1.00 | ≤ 1.0 |
| Cobalt (Co) | - | 2.00 | ≤ 2.0 |
| Boron (B) | - | 0.008 | ≤ 0.008 |
| Silicon (Si) | - | 1.00 | ≤ 1.0 |
| Copper (Cu) | - | - | ≤ 0.20 |
| Zirconium (Zr) | - | - | ≤ 0.15 |
| Sulphur (S) | - | - | ≤ 0.015 |
Tighter limits, for example a reduced sulphur or cobalt maximum, can be agreed at order and are then reported on the EN 10204 certificate.
Mechanical properties of 2.4952
Figures are for the solution-treated and aged condition at room temperature. The typical columns show what our forgings normally reach; the last column lists the minima that purchase specifications usually call for.
| Property | Typical (metric) | Typical (imperial) | Common specified minimum |
|---|---|---|---|
| Tensile strength, Rm | 1250 MPa | 181,000 psi | ≥ 1000 MPa |
| Yield strength, Rp0.2 | 780 MPa | 113,000 psi | ≥ 620 MPa |
| Elongation at break, A | 30 % | 30 % | ≥ 20 % |
| Reduction of area, Z | 30 % | 30 % | ≥ 12 % |
| Hardness | - | - | ≥ 300 HV |
| Property | Value |
|---|---|
| Density | 8.19 g/cm³ (0.296 lb/in³) |
| Melting range | approx. 1360 - 1390 °C |
| Maximum service temperature, stressed | 815 °C (1500 °F) |
| Oxidation and scaling resistance | to approx. 1000 °C (Cr2O3 layer) |
| Hot working temperature range | 1050 - 1200 °C (1920 - 2190 °F) |
| Solution treatment | 1080 °C / 8 h / air cool |
| Precipitation ageing | 700 °C / 16 h / air cool |
| Welding | TIG, MIG and MMA; weld solution treated, then re-age |
2.4952 forged product forms and size range
Every item below is made to drawing or to a dimensional standard, with machining allowance agreed at order. Hot working between 1050 °C and 1200 °C refines the grain and lays the flow lines along the part contour, which is why turbine rings and valve parts in this alloy are forged instead of cut from plate.
| Product form | Typical size range | Typical use |
|---|---|---|
| Seamless rolled rings | OD 200 - 3000 mm, wall 20 - 300 mm, height ≤ 600 mm | Turbine casing rings, bearing rings, flanged rings |
| Forged flanges | OD 100 - 2000 mm | Pressure vessels, heat exchangers, piping |
| Forged discs and blanks | Ø 100 - 1500 mm, thickness 30 - 400 mm | Turbine discs, valve discs, blade carriers |
| Forged shafts and spindles | Ø 80 - 800 mm, length ≤ 6000 mm | Rotors, eccentric shafts, valve stems |
| Forged round bars | Ø 50 - 800 mm | Bolting, fasteners, machined components |
| Sleeves and bushings | OD 100 - 1200 mm, ID ≥ 80 mm | Compressors, wear parts, subsea equipment |
| Hollow bars and forged tubes | OD 150 - 1200 mm | Pressure parts, nozzles, tube sheets |
| Blocks and rectangular forgings | to customer drawing | Valve bodies, die inserts, manifolds |
| Single-piece weight | 5 kg - 10,000 kg | - |
How we produce and test 2.4952 forgings
Melting and raw material
2.4952 billet is bought double melted, VIM plus ESR or VIM plus VAR, for turbine and aerospace-related work. The melt route is recorded on the certificate and heat numbers are traceable from billet to finished part.
Open-die forging
Billets are soaked into the 1050-1200 °C window, then upset, drawn, punched or ring rolled. Reduction ratio and finish-forging temperature are watched closely, since 2.4952 loses workability fast below roughly 1000 °C.
Heat treatment
Solution treatment at 1080 °C for 8 hours with air cooling, then ageing at 700 °C for 16 hours with air cooling. Furnace charts go out with the certificate on request.
Testing and certification
Chemical analysis, room-temperature tensile test, hardness and grain size as required. Ultrasonic testing to EN 10228-3, SEP 1921, ASTM A388 or ASTM E2375; penetrant testing to ASTM E165 or EN ISO 3452. Certificates to EN 10204 3.1, or 3.2 with third-party witness.
Where 2.4952 forgings are used
The alloy earns its cost where a part carries load in hot, sulphur-bearing gas. The main groups are:
| Industry | Typical 2.4952 forgings |
|---|---|
| Gas and steam turbines | Blades, blade carriers, seamless rolled rings, turbine discs, high-temperature bolting and studs |
| Large diesel and gas engines | Exhaust valves, valve spindles, valve seat rings, valve stems |
| Nuclear power | Boiler tube supports, hangers, fasteners |
| Oil, gas and subsea | Wellhead and Christmas tree components, subsea sleeves and bushings, compressor parts |
| Pressure equipment | Forged flanges, tube sheets, nozzles, shell-and-tube heat exchanger parts |
| Valves | Bodies, seat rings, discs and stems for ball, gate, globe, check and plug valves in hot service |
| Power transmission | Gear blanks, spindles, rolls and shafts running at elevated temperature |
| Chemical and process plant | Reactor internals, crystallizer parts, furnace fixtures, die-casting inserts and cores |
2.4952 compared with neighbouring superalloys
Where 2.4952 does not fit the duty, one of these grades usually does. We forge all of them.
| Alloy | Werkstoff / UNS | Strengthening | Service limit | Choose it when |
|---|---|---|---|---|
| Nimonic 75 | 2.4951 / N06075 | Solid solution, Ti only | approx. 1000 °C, low stress | Oxidation resistance matters more than strength, such as furnace fixtures |
| 2.4952 (Nimonic 80A) | 2.4952 / N07080 | Gamma prime, Ti and Al | 815 °C | High strength plus hot gas and sulphur resistance at moderate cost |
| Nimonic 90 | 2.4632 / N07090 | Gamma prime plus cobalt | approx. 920 °C | Creep strength above the 80A limit is required |
| Inconel X-750 | 2.4669 / N07750 | Gamma prime, Nb, Ti and Al | approx. 700 °C | Springs and bolting where relaxation resistance to 700 °C is enough |
| Waspaloy | 2.4654 / N07001 | Gamma prime plus Co and Mo | approx. 870 °C | Aerospace turbine discs and shafts with high strength requirements |
Request a quotation for 2.4952 forgings
Send a drawing or the finished dimensions. We quote forged weight, machining allowance, heat treatment condition, testing scope and delivery time, normally within 24 hours on working days.
Include these five items and we can quote without a second email:
- Grade and standard, for example 2.4952 to DIN 17742, or UNS N07080 to ASTM B637
- Drawing or finished dimensions, and whether the price should include machining
- Quantity and required delivery date
- Heat treatment condition: as forged, solution treated, or solution treated and aged
- Testing and certification: UT class, EN 10204 3.1 or 3.2, third-party inspection body
Jiangyin Jiangnan Metal Co., Ltd.
No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China
Phone and WhatsApp: +86-189-2135-9659
Email: sales@steelforgepieces.com
Frequently asked questions about 2.4952
What is material 2.4952?
2.4952 is the European material number (Werkstoff-Nr.) for NiCr20TiAl, an age-hardenable nickel-chromium superalloy carrying 19.0-21.0 % chromium, 2.0-2.6 % titanium and 1.10-1.70 % aluminium with nickel as the balance. It is sold commercially as Nimonic 80A or Alloy 80A and designated UNS N07080 in the United States. Jiangyin Jiangnan Metal Co., Ltd. forges 2.4952 into seamless rolled rings, flanges, shafts, discs and bars.
Is 2.4952 the same as Nimonic 80A?
Yes. 2.4952, NiCr20TiAl, Nimonic 80A, Alloy 80A and UNS N07080 all describe one alloy, and the Werkstoff number 2.4631 covers the same composition. Only the naming system differs.
What is the maximum service temperature of 2.4952?
2.4952 holds useful tensile and creep-rupture strength to about 815 °C (1500 °F). The chromium oxide film resists scaling to roughly 1000 °C, but load-bearing forgings are designed to the 815 °C limit.
What heat treatment is applied to 2.4952 forgings?
Solution treatment for 8 hours at 1080 °C (1976 °F) with air cooling, then precipitation ageing for 16 hours at 700 °C (1292 °F) with air cooling. Jiangyin Jiangnan Metal Co., Ltd. supplies 2.4952 forgings in this condition unless the order calls for as-forged or solution-treated only.
What is the difference between 2.4952 and 2.4631?
Both numbers cover NiCr20TiAl and mills use them interchangeably. A Werkstoff number alone does not fix the acceptance limits, so place the order against DIN 17742 or ASTM B637 together with the required condition and test requirements.
How does 2.4952 compare with Nimonic 75 and Nimonic 90?
Nimonic 75 is solid-solution strengthened and much softer. 2.4952 adds titanium and aluminium so it can be precipitation hardened to about 1250 MPa for service to 815 °C. Nimonic 90 adds cobalt for higher creep strength to roughly 920 °C.
What certificates are supplied with 2.4952 forgings?
An EN 10204 3.1 mill certificate is standard. EN 10204 3.2 certification witnessed by a third-party body such as TUV, SGS, BV or Lloyd's Register is available on request, and ultrasonic testing is reported to EN 10228-3, SEP 1921, ASTM A388 or ASTM E2375.
Who supplies 2.4952 open-die forgings in China?
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, producing 2.4952 rolled rings, flanges, shafts, discs, sleeves and bars to customer drawings. Enquiries go to sales@steelforgepieces.com or +86-189-2135-9659.
What is the density of 2.4952?
The density of 2.4952 is about 8.19 g/cm³, or 0.296 lb/in³. A ring of 1000 mm outside diameter, 800 mm inside diameter and 200 mm height weighs roughly 463 kg.
Can 2.4952 be forged into seamless rolled rings?
Yes. The alloy is hot worked between 1050 °C and 1200 °C, so a billet can be upset, pierced and ring rolled into a seamless ring with no weld seam and grain flow following the circumference. Jiangyin Jiangnan Metal Co., Ltd. rolls 2.4952 rings and heat treats them before machining allowance is applied.
This datasheet is published by Jiangyin Jiangnan Metal Co., Ltd., an open-die forging factory in Jiangyin, Jiangsu, China. Composition limits follow DIN 17742, with ASTM B637 / UNS N07080 ranges shown alongside for reference. Mechanical values are room temperature, solution treated and aged. Reviewed 11 August 2026.
Related nickel alloy forgings
- Nimonic 80A
- Nimonic 75
- Waspaloy
- Inconel X-750
- Inconel 625
- Inconel 706
- Haynes 188
- Haynes 230
- Rene 41
- Udimet 500
- Udimet 720
- Incoloy 901
- Hastelloy X
- Hastelloy C-276
- UNS N07252
All nickel and cobalt alloy grades forged by Jiangnan Metal
- Monel 400
- Monel K-500
- Monel R-405
- Inconel 600
- Inconel 601
- Inconel 617
- Inconel 690
- Inconel 693
- Inconel 725
- Incoloy 800
- Incoloy 800H
- Incoloy 800HT
- Incoloy 825
- Incoloy 890
- Incoloy 925
- Incoloy 926
- Incoloy 945
- Hastelloy B
- Hastelloy B-2
- Hastelloy B-3
- Hastelloy B-4
- Hastelloy C-4
- Hastelloy C-22
- Hastelloy C-2000
- Hastelloy G-3
- Haynes 25
- Alloy 59
- Alloy 602
- Udimet 520
- MP35N
- MP159
- Multimet N155
- NI-SPAN-C Alloy 902
- UNS N07022
- UNS N07208