2.4663 NiCr23Co12Mo Forging Parts | China Professional Manufacturer

2.4663 NiCr23Co12Mo Forging Parts — Custom NiCr23Co12Mo Forged Components by Jiangsu Liangyi, China

Key Specifications at a Glance

Material Designations2.4663 / NiCr23Co12Mo
Alloy SystemNi-Cr-Co-Mo (Nickel Base)
Density8.36 g/cm³ (0.302 lb/in³)
Melting Range1,332 – 1,380 °C
Max Service Temp (Continuous)1,100 °C
Max Service Temp (Intermittent)1,150 °C
Yield Strength (20 °C)≥ 270 MPa
Tensile Strength (20 °C)≥ 630 MPa
Weight Range (per piece)30 kg – 30,000 kg
Max Ring Outer Diameter6,000 mm
StandardsEN 10302, ASTM B564, EN 10204
CertificationISO 9001:2015 / EN 10204 3.1 (3.2 on request)
Lead Time (Standard)25–35 working days
Export Markets50+ countries worldwide

Material Overview: 2.4663 NiCr23Co12Mo Alloy

Jiangsu Liangyi Co., Ltd., a top professional manufacturer of open die forging parts and seamless rolled rings located in Jiangyin, Jiangsu Province, China, specializes in producing  2.4663 NiCr23Co12Mo forged parts.This alloy is a solid‑solution‑strengthened nickel‑chromium‑cobalt‑molybdenum superalloy, and it has excellent metallurgical stability, ultra‑high‑temperature oxidation resistance up to 1,100 °C, and excellent corrosion resistance in extreme industrial environments.

Why Choose 2.4663 NiCr23Co12Mo? This alloy occupies a unique performance range that few alternatives can equal:it combines the oxidation protection of an aluminum-doped chromia layer (a dual-scale structure of Cr₂O₃ + Al₂O₃), the creep strength from cobalt solid-solution hardening, and the sulfidation resistance of molybdenum — all at the same time. No single element can deliver all three properties; only the engineered Ni-Cr-Co-Mo balance in 2.4663 makes this possible.That is why it remains the preferred material for gas turbine combustors, nuclear steam generator nozzles, and high-temperature valve internals throughout Europe, North America, and Asia.

With over 25 years of forging experience, ISO 9001:2015 certification, we have exported products to more than 50 countries — including the USA, Germany, UAE, Saudi Arabia, Australia, Singapore, UK, France, Japan, and South Korea. We provide a full range of service for custom 2.4663 forging from steel melting, open die forging, and heat treatment to  CNC machining.All products meet ASTM, EN, and DIN international material standards.

Main Performance Advantages of 2.4663 NiCr23Co12Mo Alloy

Global Standard Equivalents of 2.4663 NiCr23Co12Mo

Engineers and procurement teams from different countries and industries use different designation systems for the same alloy. The table below is the definitive cross-reference for 2.4663 NiCr23Co12Mo — all designations listed refer to the identical chemical composition and alloy system:

Table 1 — International Standard Equivalents for 2.4663 NiCr23Co12Mo Alloy
Standard SystemCountry / RegionDesignation / GradeApplicable Product Standard
EN (European Norm)Europe / Global2.4663 / NiCr23Co12MoEN 10302 (forgings & semi-finished products)
ASTM / UNS (American)USA / GlobalN06617ASTM B564 (forgings), B168 (plate/sheet), B166 (rod/bar)
Commercial BrandUSA (Haynes International)Haynes® 617
DIN (German)GermanyNiCr22Co12MoDIN 17742
AMS (Aerospace)USA (Aerospace)AMS 5888Sheet, strip, plate; AMS 5664 (bar, forgings) — reference standard only
ISOInternationalNC22Co12Mo (ISO 9722)ISO 9722
ASMEUSA (Pressure Vessels)N06617ASME Section II Part B, SB-564 (forgings)
GB / China NationalChinaGH617GB/T 14992
⚙ Jiangsu Liangyi Manufacturing Note

A common sourcing error we encounter: buyers from China or India occasionally enquire for "2.4816" or "2.4858" when they actually need 2.4663. These are entirely different alloys (Inconel® 600 and Incoloy 825, respectively). Always confirm the 2.4663 / NiCr23Co12Mo designation or share your drawing's chemical composition table to avoid costly material mix-ups before production begins.

Physical and Thermal Properties of 2.4663 NiCr23Co12Mo

These physical properties are essential for engineering calculations including thermal stress analysis, heat exchanger design, creep modelling, and weight estimation for large-section 2.4663 forgings. Values are for solution-annealed condition unless otherwise noted.

Table 2 — Physical and Thermal Properties of 2.4663 NiCr23Co12Mo, Solution-Annealed Condition
PropertyValue at 20 °C (RT)Value at 400 °CValue at 700 °CValue at 900 °CUnit
Density8.368.208.037.89g/cm³
Melting Range1,332 – 1,380 °C (solidus to liquidus)°C
Elastic Modulus (Young's)211196172148GPa
Coefficient of Thermal Expansion (CTE)12.713.514.815.6µm/(m·°C)
Thermal Conductivity13.417.522.827.5W/(m·K)
Specific Heat Capacity419460502535J/(kg·K)
Electrical Resistivity1.221.261.301.33µΩ·m
Thermal Diffusivity3.814.625.676.52mm²/s
Magnetic Permeability≈ 1.001 (essentially non-magnetic)
⚙ Engineering Insight from Our Technical Team

The relatively low thermal conductivity of 2.4663 — 13.4 W/m·K at room temperature, versus about 50 W/m·K for carbon steel — directly affects  forging die design and cooling strategy.Heat dissipates far more slowly through the workpiece, meaning the core of a heavy section forging can remain hot long after the surface has cooled.In our 6,300-ton press operations, we compensate by extending die contact time and monitoring core temperature using embedded thermocouples during heavy-section forging — a practice most conventional forging shops do not apply to nickel alloys.

Full Range of 2.4663 NiCr23Co12Mo Forged Product Forms

We manufacture custom 2.4663 NiCr23Co12Mo forging parts strictly according to customer drawings and technical specifications, and they all meet EN 10204 3.1 certification requirements (EN 10204 3.2 available upon customer arrangement with an approved third-party inspector). Visit our Products Page for further details.

2.4663 Forged Bars and Rods

Round bars, square bars, flat bars, rectangular bars, step shafts, and valve spindles. The maximum forging diameter is up to 2,000 mm, the maximum length is up to 15,000 mm. and they  are widely used for turbine blades, fasteners, valve stems, compressor shafts, and critical structural parts. All parts are tested by UT and can be traced.

NiCr23Co12Mo Seamless Rolled Forged Rings

Custom seamless rolled rings, contoured forged rings, and open die forged rings up to 6,000 mm OD and 30 tonnes in weight. They are the best choice material for  turbine guide rings, seal rings, labyrinth rings, valve seat rings, gear rings, and pressure vessel flanges. All parts are produced on our advanced 5-metre radial-axial ring rolling mill — see our Equipment Page.

2.4663 Hollow Forgings, Sleeves and Pipes

Forged sleeves, bushes, bushings, hollow bars, heavy-wall cylinders, seamless pipes, tubes, and casings with outer diameter up to 3,000 mm. They are the best choice material  for pump casings, valve bodies, reactor nozzles, bore protectors, and heat exchanger shells — deleting weld seams and their associated integrity risks in high-pressure corrosive environments.

NiCr23Co12Mo Forged Discs, Plates and Blocks

Forged discs, disks, blanks, plates, blocks, and flanged blanks with maximum outside diameter up to 3,000 mm and single-piece weight up to 20 tonnes. They are used for gas and steam turbine discs, impellers, blisks, valve discs, tube sheets, and pressure vessel parts.

Dimensional Capability Summary

The table below consolidates the dimensional ranges we can get per product form for 2.4663 NiCr23Co12Mo. All values represent our in-house capability without sub-contracting:

Table 3 — 2.4663 NiCr23Co12Mo Forging Dimensional Capability at Jiangsu Liangyi
Product FormMax Outer Diameter / WidthMax Length / HeightMax Single-Piece WeightWall / Thickness RangeDelivery Surface
Forged Round BarØ 2,000 mm15,000 mm30 tSolid / steppedAs-forged / machined
Seamless Rolled RingØ 6,000 mm OD1,500 mm height30 t50 – 600 mm wallAs-rolled / machined
Open Die Forged RingØ 4,000 mm OD2,000 mm height25 t80 – 800 mm wallAs-forged / machined
Hollow Forging / SleeveØ 3,000 mm OD5,000 mm20 t50 – 500 mm wallAs-forged / machined
Forged Disc / PlateØ 3,000 mm1,200 mm thick20 t100 mm min thicknessAs-forged / machined
Forged Block / Slab2,000 × 1,500 mm3,000 mm25 t150 mm min thicknessAs-forged / machined
2.4663 NiCr23Co12Mo Open Die Forging Production at Jiangsu Liangyi Factory, Jiangyin, China

Industry Applications and Verified Project Cases

2.4663 NiCr23Co12Mo forging parts are the best choice material for important industrial sectors needing long-term stable performance in extreme high-temperature, high-pressure, and highly corrosive environments. Our verified project cases cover global mainstream markets, with full compliance with local industry standards:

Nuclear Power Industry (Asia and Europe Market)

Project Case: Nuclear Reactor Coolant Pump Forgings for Asian Nuclear Power Plants

Customer Pain Point: Nuclear-grade parts need ultra-high material purity, excellent impact toughness, and 100% defect-free performance in radioactive coolant environments, and all parts must meet nuclear-industry safety standards.

Our Solution: We supplied custom 2.4663 NiCr23Co12Mo forged reactor coolant pump casings, rotor impellers, containment seal chambers, and pump shafts. All parts were produced via vacuum melting + ESR to control impurity content, with 100% volumetric UT, MT, and PT inspection, plus full raw-material-to-finished-product traceability.

Project Value: Our 2.4663 forgings have been working stably for over 8 years, and they all meet strict safety requirements. We have become a long-term qualified supplier for 3 big Asian nuclear power groups.

Power Generation Turbine Industry (Global Market)

Project Case: High-Temperature Turbine Parts for 660 MW Thermal Power Plants

Customer Pain Point:  Main steam valves and turbine parts work at high pressure and 650 °C for long periods of time. To avoid unplanned shutdowns, they must strongly resist creep, oxidation, and thermal fatigue.

Our Solution: We delivered custom 2.4663 forged turbine discs, impellers, blades, MSV/GV/CV/CRV valve seats, valve spindles, control reheat valve discs, and diaphragm nozzles. We improved heat-treatment parameters to guarantee stable high-temperature mechanical properties, with full high-temperature tensile and creep tests performed per batch.

Project Value: Our parts extended the power plant maintenance cycle from 12 to 24 months. They have been applied in more than 20 thermal power projects across Asia, Europe, and the Middle East.

Oil and Gas Valve Industry (Middle East and North America Market)

Project Case: High-Pressure Corrosion-Resistant Valve Forgings for Middle East Oilfield Wellhead Projects

Customer Pain Point: Oilfield wellhead valves work in high-pressure H₂S and CO₂ corrosive environments, they must have excellent sour-service resistance, high strength, and long lifetime, with reference to API 6A material and dimensional requirements.

Our Solution: We manufactured NiCr23Co12Mo forged valve bodies, bonnets, stems, seat rings, valve cores, valve balls, and valve discs for ball, gate, check, and back-pressure valves. All products are manufactured based on API 6A dimensional and material requirements; NACE MR0175 sour-service version available. Cobalt-based hardfacing alloy applied to sealing surfaces for enhanced wear resistance.

Project Value: They all used in oilfield projects for clients in the Middle East and North America, with verified lifetime significantly exceeding conventional alloy-steel valve alternatives.

Petrochemical and Heat Exchanger Industry (Europe & Southeast Asia Market)

Project Case: Heat Exchanger andPressure Vessel Forgings for European Petrochemical Plants

Customer Pain Point: Petrochemical reactors and heat exchangers face prolonged exposure to strong oxidising and reducing chemical media, needing excellent uniform corrosion resistance and structural stability.

Our Solution: We provided 2.4663 forged tube sheets, baffle plates, pressure vessel reactor nozzles, seamless pipes, shells, and channel flanges. We strictly control  the chemical composition and heat-treatment to guarantee consistent corrosion resistance of the whole part, with hydrostatic and intergranular corrosion testing per product.

Project Value:  They have been working steadily for more than six years in harsh chemical environments without any  failures. and many European petrochemical companies have recognized them.

Turbomachinery and Compressor Industry (Global Market)

Project Case: Centrifugal Compressor Impeller Forgings for Global Gas Compression Systems

Customer Pain Point: High-speed centrifugal compressor impellers require exceptional metallurgical stability, high fatigue strength, and consistent internal matrix to prevent fracture failure at 10,000+ rpm.

Our Solution: We supplied 2.4663 NiCr23Co12Mo forged centrifugal compressor impellers, shrouded impellers, labyrinth shaft seals, pump casings, and shafts. Multi-directional forging guarantees consistent grain matrix; 100% UT and high-speed dynamic balancing performed.

Project Value: Applied in more than 50 gas compression systems worldwide, stable at 12,000 rpm. Qualified supplier for international top-tier turbomachinery OEMs.

Smelting and Forging Production Process

The production of our 2.4663 NiCr23Co12Mo forged parts follows internationally advanced standards, with full in-house capability from raw-material smelting to finished-product inspection:

Step 1 — Premium Alloy Smelting

To guarantee ultra-high purity and consistent chemical composition of 2.4663 alloy, we use industry-leading processes:

⚙ 25-Year Forging Insight: Why Carbon Control Is Critical in 2.4663

Unlike stainless steels, where low carbon is always preferred to avoid sensitization, 2.4663 needs a minimum carbon content of 0.05%.This is because M₂₃C₆ carbides formed at grain boundaries effectively improve creep resistance at 750–900 °C — they pin grain boundaries and slow down creep deformation.Our AOD melting process maintains carbon within a tight tolerance of ±0.01%, a level of control that standard EAF-only smelters cannot consistently achieve.This directly determines the long-term creep performance of gas turbine discs and nuclear steam generator parts.

Step 2 — Open Die Forging and Seamless Ring Rolling

We use 2,000–6,300 T hydraulic forging presses and 1–9 T electro-hydraulic hammers for open die forging. Key parameters for 2.4663:

Step 3 — Solution Annealing and Optional Ageing

After forging, all 2.4663 parts are given solution annealing at 1,150–1,200 °C, with a holding time of at least1 hour per 25 mm of maximum section thickness, followed by rapid water quenching within 60 seconds of leaving the furnace.This dissolves any secondary carbides formed during forging and restores a uniform austenitic matrix. An optional stabilization treatment at 980–1,010 °C is available for applications requiring controlled carbide distribution to meet specific creep performance requirements. All heat treatment is performed in our fully automatic, temperature-controlled continuous and batch furnaces equipped with multi-point thermocouple monitoring, traceable to NIST/PTB calibration standards. Full heat treatment charts are included with each delivery.

Step 4 — CNC Machining and Dimension Test

CNC turning, milling, drilling, boring, and grinding to customer drawings. Dimension test by CMM (coordinate measuring machine) and laser scanning. We keep machining tolerances to IT8 as standard, with IT6 available for critical-fit parts such as turbine disc bore diameters.

Welding and Machining Guidelines for 2.4663 NiCr23Co12Mo

The following guidelines are drawn from our 25 years of hands-on experience welding and machining 2.4663 NiCr23Co12Mo forgings, and from interactions with customers who undertake site welding of our components. This information is not replicated from any generic datasheet — it reflects what we have learned from real production problems and failures.

Welding

Machining

⚠ Common Sourcing Pitfall We See in the Market

 Some low-cost suppliers supply 2.4663 forgings in the as-forged condition without solution annealing, claiming they “meet hardness requirements”. This is an incorrect practice. Without proper solution annealing at 1,150–1,200 °C, the grain boundary carbide networks formed during forging remain, resulting in a severe loss of ductility — elongation can drop from ≥30% to below 15% — and unpredictable high-temperature creep performance. Always verify that the heat treatment chart is included with the material test certificate (MTC), and that the solution temperature and holding time are clearly specified.

Corrosion & Oxidation Resistance of 2.4663 NiCr23Co12Mo — In Depth

The corrosion resistance of 2.4663 NiCr23Co12Mo operates through fundamentally different mechanisms depending on the environment. Understanding these mechanisms allows engineers to confirm whether 2.4663 is the right alloy — or whether a different material should be specified.

High-Temperature Oxidation (Air / Combustion Gases)

The primary oxidation protection mechanism involves two simultaneous oxide scale layers:

  1. Outer Cr₂O₃ layer — formed by the 20–23% chromium content; provides the bulk diffusion barrier against oxygen ingress and is the first defence in cyclic oxidation. Begins forming above 600 °C.
  2. Inner Al₂O₃ sub-layer — formed by the 0.7–1.4% aluminium content; far more thermodynamically stable than Cr₂O₃ at temperatures above 950 °C, and critically important when the chromia layer is disrupted by thermal cycling or mechanical spallation. This is what separates 2.4663 from Cr-only alloys above 950 °C.

In cyclic oxidation testing (1,000 °C, 1,000 cycles, air), 2.4663 NiCr23Co12Mo exhibits a weight change of less than ±3 mg/cm² — comparable to oxide dispersion-strengthened alloys costing 5–10× more.

Sulphidation Resistance (H₂S / SO₂ Environments)

2.4663 performs well in mixed oxidising/sulphidising gas streams up to 900 °C, primarily due to the Cr₂O₃ scale acting as a barrier to sulphur diffusion. However, in pure reducing sulphidising environments (very low pO₂), the chromia scale is destabilised and 2.4663 is not the optimal choice — Hastelloy® C-276 or Inconel® 625 would be preferred. For sour-service oil and gas applications with predominantly H₂S/CO₂ in liquid-phase environments (below 200 °C), the selection criterion shifts to NACE MR0175 compliance rather than high-temperature oxidation.

Aqueous Corrosion & SCC Resistance

Carburisation Resistance

In carburizing atmospheres (high CO, hydrocarbon-rich), the dual Cr₂O₃/Al₂O₃ oxide layer acts as an effective barrier against carbon diffusion.2.4663 exhibits outstanding carburization resistance up to 1,000 °C, outperforming Alloy 800H and most austenitic stainless steels.This makes it the preferred forging material for petrochemical reformer tube fittings and radiant tube hangers.

Chemical Composition of 2.4663 NiCr23Co12Mo Alloy

The chemical composition of our 2.4663 NiCr23Co12Mo forgings strictly meet EN 10302 and ASTM B564. Every heat is spectrographically analysed on incoming billet and on the finished forging, with results recorded in the MTC.

Table 4 — Chemical Composition of 2.4663 NiCr23Co12Mo, wt%
ElementContent Range (wt%)ElementContent Range (wt%)
Nickel (Ni)Remainder (base element, ≥ 44%)Carbon (C)0.05 – 0.10%
Chromium (Cr)20.0 – 23.0%Titanium (Ti)0.2 – 0.6%
Cobalt (Co)11.0 – 14.0%Iron (Fe)Max 2.0%
Molybdenum (Mo)8.5 – 10.0%Silicon (Si)Max 0.2%
Aluminium (Al)0.7 – 1.4%Manganese (Mn)Max 0.2%
Phosphorus (P)Max 0.01%Sulfur (S)Max 0.01%
Copper (Cu)Max 0.5%Boron (B)Max 0.006%
⚙ Why Boron Content Matters in 2.4663 Forgings

Although boron is only present in trace amounts (max. 0.006%), its effect is extremely significant.It segregates at grain boundaries and enhances boundary cohesion, improving creep ductility by roughly 15–20% compared to boron-free melts.However, if boron content exceeds 0.008%, it forms low-melting-point borides such as Ni₃B (melting point ~1,080 °C), which can lead to incipient melting during forging reheating and hot cracking during welding.Our spectroscopic analysis controls boron within 0.003–0.005%, placing it firmly in the optimal performance range.

Mechanical Properties, High-Temperature Data and Creep Strength

Mechanical properties are tested on samples cut from tangential test rings in the delivery condition, per EN ISO 6892-1 & -2. Tests are performed at our in-house laboratory with calibration traceable to national measurement standards.

Room-Temperature & Elevated-Temperature Tensile Properties

Table 5 — Short-Time Tensile Properties of 2.4663 NiCr23Co12Mo Forgings, Solution-Annealed
Test TemperatureYield Strength Rp0.2 (MPa)Tensile Strength Rm (MPa)Elongation A (%)Reduction of Area Z (%)Impact Energy KV (J)Hardness (HBW)
20 °C (RT, minimum guaranteed)≥ 270≥ 630≥ 30≥ 50≥ 100 (avg. 3 specimens)130 – 220
400 °C≈ 230≈ 590≈ 34≈ 55
650 °C (minimum guaranteed)≥ 187≈ 510≈ 38≈ 60
750 °C≈ 165≈ 470≈ 40≈ 62
850 °C≈ 140≈ 390≈ 45≈ 65
1,000 °C≈ 85≈ 200≈ 55≈ 70

Note: Values at 400 °C–1,000 °C are typical reference data for solution-annealed condition. EN 10302 mandates verification at 20 °C and 650 °C only. Testing at additional temperatures can be specified at order stage.

Creep Rupture Strength — The Engineering Design Critical Parameter

For gas turbine, nuclear, and high-temperature pressure vessel applications, creep rupture strength is the primary design parameter — not room-temperature yield strength. The following data allows structural engineers to validate whether 2.4663 meets the needed design stress at the intended operating temperature and lifetime:

Table 6 — Creep Rupture Strength of 2.4663 NiCr23Co12Mo, Solution-Annealed Condition (Typical Values)
TemperatureRupture Stress at 1,000 h (MPa)Rupture Stress at 10,000 h (MPa)Rupture Stress at 100,000 h (MPa)1% Creep Strain Stress at 10,000 h (MPa)
650 °C≈ 370≈ 285≈ 210≈ 195
700 °C≈ 310≈ 225≈ 160≈ 140
750 °C≈ 240≈ 160≈ 108≈ 90
800 °C≈ 170≈ 105≈ 65≈ 52
850 °C≈ 110≈ 65≈ 38≈ 28
900 °C≈ 65≈ 36≈ 20≈ 14
950 °C≈ 35≈ 18≈ 9

These are representative values for solution-annealed 2.4663 NiCr23Co12Mo bar and forging. Heat-to-heat variation applies. For design-critical applications, we can perform creep testing on specimens from the actual production forging heat at specified conditions — please discuss at enquiry stage.

Alloy Selection Guide: 2.4663 vs Competing High-Temperature Alloys

The table below reflects decisions we have helped customers navigate across hundreds of projects. It is not a marketing comparison — it honestly identifies where 2.4663 is the right choice and where other alloys are better suited. Use this as a starting point for your material selection review:

Table 7 — Comparative Performance: 2.4663 NiCr23Co12Mo vs Key Competing High-Temperature Alloys
Performance Criterion2.4663 NiCr23Co12MoInconel® 625 (2.4856)Inconel® 718 (2.4668)Hastelloy® X (2.4665)Alloy 800H (1.4958)
Max Continuous Use Temp.1,100 °C980 °C700 °C1,200 °C900 °C
Creep Strength (> 800 °C)ExcellentLimitedLimitedModerateModerate
Oxidation ResistanceExcellentGoodModerateExcellentGood
Aqueous Corrosion ResistanceGoodExcellentModerateExcellentLimited
RT Yield Strength≥ 270 MPa≥ 275 MPa≥ 1,034 MPa (aged)≥ 275 MPa≥ 170 MPa
WeldabilityExcellentExcellentModerate (strain-age cracking risk)ExcellentGood
Sulphidation Resistance (< 900 °C)GoodModerateLimitedExcellentModerate
Carburisation ResistanceExcellentModerateLimitedGoodGood
Relative Material CostHighHighHighVery HighModerate
Best Fit ApplicationsGas turbines, nuclear, high-T valvesOffshore, seawater, cryogenicAerospace, aerospace fastenersCombustor liners, radiant tubesReformers, petrochemical furnaces
⚙ Our Engineering Recommendation

If your operating temperature is consistently above 800 °C and creep or oxidation is your main failure concern, 2.4663 (NiCr23Co12Mo) is almost always the right choice over Inconel® 625 or Alloy 800H. If your service temperature is below 700 °C and seawater, chloride, or acidic aqueous corrosion is the priority, Inconel® 625 (2.4856) or Hastelloy® C-276 (2.4819) will perform better than 2.4663 at a lower cost. We offer free, no-obligation material selection support. For detailed advice, contact our technical team at: sales@jnmtforgedparts.com.

Quality Control and Non-Destructive Testing (NDT)

We implement a full-process quality control system for all 2.4663 NiCr23Co12Mo forging parts, from raw-material incoming inspection to finished-product delivery, with 100% inspection coverage for all important process steps:

Microstructure & Grain Size Inspection

The microstructure of our 2.4663 forged discs and rings must be consistent, free from excessive segregation, inclusions, and other structural inhomogeneities.Grain size is evaluated in accordance with EN ISO 643, with a target grain size of Grade 1 for all rings; only random larger grains within a 0–1 class deviation are permitted.We verify the optimized microstructure using a high-precision metallurgical microscope.

100% Non-Destructive Testing (NDT)

Full-coverage NDT on all 2.4663 forged parts, strictly meeting EN 13018 and EN ISO 9712:

Compliance & Certification

All 2.4663 NiCr23Co12Mo forging parts manufactured in our ISO 9001:2015 certified facility, fully  meeting EN 10204, EN 10302, and ASTM. EN 10204 3.1 MTC is provided as standard; EN 10204 3.2 is available upon customer arrangement with an approved third-party inspector. Explore our full material range on our Materials Page.

Packaging, Documentation & Export Information

For international buyers, the completeness of shipping documentation and the quality of sea-freight packaging are as important as the forging itself. Here is what every Jiangsu Liangyi 2.4663 NiCr23Co12Mo forging delivery includes:

Packaging

Standard Documentation per Shipment

Trade Terms and Payment

Frequently Asked Questions about 2.4663 NiCr23Co12Mo Forgings

2.4663 NiCr23Co12Mo is the European EN standard designation. It shares identical chemical composition and mechanical property requirements with AMS 5888 / AMS 5664 (aerospace), DIN NiCr22Co12Mo (Germany), ISO NC22Co12Mo, and GH617 (China GB). All designations refer to the same Ni-Cr-Co-Mo superalloy. See our full equivalents table above for the complete cross-reference.
 The density of 2.4663 NiCr23Co12Mo is 8.36 g/cm³(0.302 lb/in³) at room temperature.This is slightly lower than Inconel® 625 (8.44 g/cm³) but falls within the same density range.For a 30‑tonne ring forging at maximum size (6,000 mm outer diameter), purchasers should account for this density in logistics planning.Our engineering team can provide estimated weight calculations for any proposed forging blank geometry upon request.
 The standard solution annealing temperature for 2.4663 NiCr23Co12Mo is 1,150–1,200 °C, with a holding time of at least  1 hour per 25 mm of maximum section thickness, followed by rapid water quenching within 60 seconds of removal from the furnace.This process dissolves the grain boundary carbide networks formed during forging.Temperatures below 1,150 °C result in incomplete carbide dissolution, while exceeding 1,220 °C risks grain coarsening beyond the EN ISO 643 Grade 1 requirement and, in severe cases, incipient melting in cobalt-rich grain boundary films.

For GTAW and GMAW welding of 2.4663, the standard filler metal is  ERNiCrCoMo-1 (AWS A5.14), a matching composition filler that retains high‑temperature creep performance.

Inconel® 625 filler (ERNiCrMo-3) should not be substituted for high‑temperature service — the lack of cobalt in 625‑type filler drastically reduces creep strength in the weld zone above 750 °C.
Interpass temperature must be kept below 150 °C  to avoid hot cracking in the heat‑affected zone (HAZ).

2.4663 NiCr23Co12Mo keeps stable oxidation resistance in continuous service up to 1,100 °C and can withstand intermittent service up to 1,150 °C. For long-term creep-controlled load-bearing applications (turbine discs, pressure-bearing nozzles), the practical design temperature limit is 850–900 °C, constrained by creep rupture life rather than oxidation.

The main difference is their chemical makeup and how they perform. 2.4663 NiCr23Co12Mo has 11–14% Co and 0.7–1.4% Al, which gives it better creep strength and resistance to oxidation above 800 °C — perfect for gas turbines and nuclear parts. Inconel® 625 (2.4856) has no cobalt and gets its strength from 3.15–4.15% Nb, providing better resistance to corrosion in water (seawater, chlorides, acids) below 700 °C. Choosing between them is easy: if you mainly need it to work above 800 °C, 2.4663 NiCr23Co12Mo is better; if you need protection against seawater corrosion or toughness in very cold temperatures, 2.4856 is better.

Yes. Haynes® 617 (manufactured by Haynes International) is a commercial brand name for 2.4663 NiCr23Co12Mo. Both meet the same EN 10302 and ASTM B564 chemical composition and mechanical property requirements. From an engineering performance standpoint, the brand is irrelevant — what matters is conformance to the EN 10302 / ASTM B564 specification, which our forgings fully comply with.
Yes. 2.4663 NiCr23Co12Mo is listed in ASME Section II Part B, SB-564 (forgings) and is approved for use in ASME-coded pressure vessels, reactor nozzles, and heat exchangers. We supply Material Test Reports formatted to ASME requirements. If your project requires ASME Code compliance, please specify this at enquiry stage and we will ensure the MTC includes all ASME-mandated data fields.
Yes. All our 2.4663 NiCr23Co12Mo forgings are produced to customer drawings and technical specifications. We provide full-process services from EAF/ESR smelting, open die forging, seamless ring rolling, solution annealing, CNC machining to100% NDT. We also  provide EN 10204 3.1 certification (3.2 on customer request). Our single-piece weight ranges from 30 kg to 30 tonnes. Please share your drawing, needed material standard, quantity, and delivery deadline for a formal quotation.
Factory: ISO 9001:2015. Per-delivery: EN 10204 3.1 Mill Test Certificate as standard; EN 10204 3.2 available upon customer arrangement with approved third-party inspector. Standards manufactured with reference to: EN 10302, ASTM B564, DIN 17742. Third-party inspection by SGS, Bureau Veritas, or TUV is available and can be pre-arranged before production begins. Nuclear-grade orders include full traceability and nuclear-grade inspection documentation.
Standard lead time: 25–35 working days. Urgent orders: 15–20 working days (subject to production schedule). Lead time depends on section thickness (larger sections require more heat treatment time), NDT scope, and whether third-party inspection is needed. We provide a confirmed delivery date with each order acknowledgement.
Maximum outer diameter: 6,000 mm. Maximum height: 1,500 mm. Single-piece weight up to 30 tonnes. For the largest rings (OD > 4,000 mm), we use our 5-metre radial-axial ring rolling machine in combination with 6,300 T press pre-forming. This combination allows us to maintain a minimum forging ratio of 4:1 even in the largest sections, ensuring grain refinement throughout the cross-section.
Yes. For nuclear-grade 2.4663 forgings we use the VIM + ESR (double-melt) process, getting O < 10 ppm, N < 30 ppm, and certified total inclusion cleanliness. All parts are fully traceable from raw material to finished product . We have supplied nuclear-grade 2.4663 reactor coolant pump parts for 3 major Asian nuclear power groups and have over 8 years of operational track record in nuclear-grade forging.
We supply 2.4663 NiCr23Co12Mo forgings in the following surface conditions: (1) As-forged with descaled/shot-blasted surface (Sa 2.5); (2) Pickled and passivated; (3) CNC turned/milled to Ra 1.6–3.2 µm as standard machining; (4) Ground to Ra 0.8 µm for sealing faces, bearing seats, and O-ring grooves; (5) Polished to Ra 0.4 µm for optical or ultra-clean applications. Surface finish must be specified on the customer drawing or purchase order.

Related High-Temperature & Corrosion-Resistant Alloy Forgings

If 2.4663 NiCr23Co12Mo does not precisely match your application's requirements, we manufacture forging parts in the following closely related high-performance alloys. Our Materials Page lists our complete material capabilities:

Request a Quote | China 2.4663 NiCr23Co12Mo Forging Expert

Jiangsu Liangyi Co., Limited is a top professional manufacturer of 2.4663 NiCr23Co12Mo open die forging parts and seamless rolled rings in Jiangsu Province, China. With over 25 years of forging experience, advanced production and inspection equipment, and a dedicated technical team, we provide high-quality, cost-effective custom forging solutions for global customers in nuclear power, power generation, oil and gas, petrochemical, and turbomachinery industries. Send us your drawings, material requirements, quantity, and application details to get a detailed quotation and technical solution. Our sales engineering team responds within 24 hours.

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Inquiry Email: sales@jnmtforgedparts.com

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Factory Address: Chengchang Industry Park, Jiangyin City, Jiangsu Province, China