NiCr13Mo6Ti3 forgings W.Nr. 2.4662 · UNS N09901 · Alloy 901
NiCr13Mo6Ti3 is the DIN/EN designation for Alloy 901, an age-hardenable nickel-iron-chromium superalloy also catalogued as W.Nr. 2.4662, UNS N09901, Nimonic 901 and Incoloy 901. Molybdenum provides solid-solution strengthening. Titanium and aluminium form the gamma-prime precipitate that develops during ageing. The alloy holds high yield strength and creep resistance to about 600 °C (1110 °F). Its iron content, high for a nickel superalloy, is what makes the grade practical to forge.
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory in Jiangyin, Jiangsu Province, China. We produce NiCr13Mo6Ti3 seamless rolled rings, discs, shafts, flanges, sleeves, bushings and tube sheets to customer drawing, supplied with EN 10204 3.1 or 3.2 certification.
- Werkstoff
- 2.4662 · 2.4975
- UNS
- N09901
- Trade names
- Alloy 901 · Nimonic 901 · Incoloy 901 · Pyromet 901
- China GB
- GH2901 · GH901
- AMS
- 5660 · 5661 · 5830
- British
- HR 53 · HR 55
- AFNOR
- Z8 NCDT 42
- ISO
- 9723 · 9725 · NiFe35Cr14MoTi
- Type
- Ni-Fe-Cr, age-hardenable
- Max service
- approx. 600 °C / 1110 °F
What we can forge in NiCr13Mo6Ti3
Jiangyin Jiangnan Metal Co., Ltd. forges NiCr13Mo6Ti3 (Alloy 901) as seamless rolled rings up to 3,000 mm outside diameter, solid discs and blocks up to 1,500 mm diameter, and shafts up to 6,000 mm long, at single-piece weights from 20 kg to 8,000 kg. Lead time for a first-article Alloy 901 forging is normally 35 to 50 days from confirmed order. There is no minimum order quantity for prototype or single-piece work.
- Rolled ring OD
- 3,000 mm max
- Disc / block dia.
- 1,500 mm max
- Shaft length
- 6,000 mm max
- Single-piece weight
- 20–8,000 kg
- Lead time
- 35–50 days
- Minimum order
- 1 piece
The sizes above apply to this grade. Nickel superalloys have a narrower hot-working range than carbon or alloy steel, so the maximum section quoted in Alloy 901 is smaller than the carbon-steel maximum. Send the drawing and we will confirm feasibility before quoting.
NiCr13Mo6Ti3 chemical composition
The chemical composition of NiCr13Mo6Ti3 (Alloy 901, UNS N09901) to AMS 5660 and AMS 5661 is Ni+Co 40.0–45.0%, Cr 11.0–14.0%, Mo 5.0–6.5% and Ti 2.80–3.10%, with iron as the balance. The titanium addition of about 3% forms the gamma-prime Ni3(Ti,Al) precipitate that carries the strength of the alloy at temperature.
Swipe to see all columns
| Element | Min % | Max % | Function |
|---|---|---|---|
| Nickel + cobalt (Ni+Co) | 40.00 | 45.00 | Austenitic matrix, high-temperature stability |
| Chromium (Cr) | 11.00 | 14.00 | Oxidation and hot-corrosion resistance |
| Molybdenum (Mo) | 5.00 | 6.50 | Solid-solution strengthening, creep resistance |
| Titanium (Ti) | 2.80 | 3.10 | Forms gamma-prime, the principal strengthener |
| Carbon (C) | 0.02 | 0.06 | Grain-boundary carbides, held low for ductility |
| Boron (B) | 0.010 | 0.020 | Grain-boundary strengthening, stress-rupture life |
| Aluminium (Al) | — | 0.35 | Supports gamma-prime formation with titanium |
| Cobalt (Co) | — | 1.00 | Residual, counted within Ni+Co |
| Manganese (Mn) | — | 0.50 | Residual, deoxidation |
| Silicon (Si) | — | 0.40 | Residual, deoxidation |
| Copper (Cu) | — | 0.20 | Residual, restricted |
| Phosphorus (P) | — | 0.020 | Tramp element, restricted |
| Sulphur (S) | — | 0.008 | Tramp element, low sulphur protects hot ductility |
| Iron (Fe) | Balance | Base element, gives the alloy its forgeability | |
Limits follow AMS 5661. ISO 9723 and 9725, MSRR 7029 and 7031, and AECMA PrEN 2176 apply slightly different ranges, most often a wider carbon band up to 0.10%. Where a purchase order names a specification, material is melted and certified to that specification, and the mill test certificate governs.
Mechanical properties
In the solution treated, stabilised and aged condition, NiCr13Mo6Ti3 meets a minimum room-temperature tensile strength of 1,130 MPa (164 ksi) and a minimum 0.2% proof stress of 810 MPa (117 ksi), with 10% minimum elongation on 5D. Strength is retained to about 600 °C, which is the practical ceiling for load-bearing service in this grade.
| Property | Metric | Imperial | Basis |
|---|---|---|---|
| Tensile strength, Rm | 1,130 MPa min | 164 ksi min | Specification minimum |
| Proof stress, Rp0.2 | 810 MPa min | 117 ksi min | Specification minimum |
| Elongation, A5D | 10 % min | 10 % min | Specification minimum |
| Reduction of area, Z | 15 % min | 15 % min | Specification minimum |
| Elastic modulus, E | 201 GPa | 29.2 x 106 psi | Typical, 20 °C |
| Hardness | approx. 302 HB | approx. 32 HRC | Typical, aged |
| Stress rupture | 552 MPa at 649 °C | 80 ksi at 1200 °F | 23 h minimum life, combination smooth and notched bar |
The figures above are acceptance minima that a forging has to meet. Production heats normally exceed them. Properties in heavy sections depend on forging reduction and quench rate. For sections over 200 mm, test location and property targets are agreed before the billet is cut.
Physical properties
- Density
- 8.14 g/cm³
- Density
- 0.294 lb/in³
- Elastic modulus
- 201 GPa
- Max service temp.
- 600 °C
- Structure
- FCC gamma + gamma-prime
- Magnetic
- Non- magnetic
Thermal conductivity, specific heat and mean coefficient of thermal expansion over 20–650 °C are available on request from sales@steelforgepieces.com.
Melting, forging and heat treatment
Melting route
NiCr13Mo6Ti3 is a double or triple melted grade. Titanium and aluminium oxidise readily, so air melting alone will not hold the 2.80–3.10% titanium band or the low sulphur limit. Billet is specified as VIM + VAR, VIM + ESR or EAF + VOD + ESR according to the end application. Aerospace rotating parts take VIM + VAR. Industrial and petrochemical parts are normally satisfied by ESR.
Forging window
Alloy 901 has a narrow hot-working range. Stock is heated to 1,120–1,150 °C and finished above 950 °C. Below that temperature the alloy work-hardens sharply and the risk of surface cracking rises. Reheats are built into the forging sequence, and each heat is soaked to temperature through the full section rather than timed from the surface. Deformation breaks down the as-cast structure and produces grain flow that follows the contour of the part.
Heat treatment
The standard cycle for NiCr13Mo6Ti3 has three stages: solution, stabilise, age. The stabilising step cannot be omitted. Without it the grain-boundary carbide distribution is wrong and stress-rupture life falls below specification.
| Stage | Temperature | Time | Cool |
|---|---|---|---|
| Solution treat | 1,080–1,100 °C 1,975–2,010 °F | 2 h | Oil or water quench |
| Stabilise | 790 °C 1,450 °F | 2 h | Air cool |
| Age | 720 °C 1,325 °F | 24 h | Air cool |
Furnace charts are recorded for every cycle and issued with the certificate. Where a customer specification calls for a different cycle, that cycle is run.
NiCr13Mo6Ti3 forged product forms
Each item below is open-die forged or ring-rolled to drawing in NiCr13Mo6Ti3 (Alloy 901). This grade is not held as standard-size stock. Superalloy is produced against the order, so a quotation needs the drawing.
Seamless rolled rings
Ring-rolled instead of cut from plate, so grain flow is circumferential and continuous. Turbine casing rings, bearing rings, retaining rings.
Forged discs and blanks
Gas-turbine discs, compressor wheels, blind blanks for later machining. Upset forged to control centre soundness.
Shafts and spindles
Stepped and straight shafts, turbine rotor shafts, pump and compressor spindles, eccentric shafts.
Flanges
Weld-neck, slip-on, blind and special-profile flanges for high-temperature pressure duty.
Sleeves and bushings
Forged hollow sections, wear sleeves, bushes and bearing housings with bores trepanned instead of drilled.
Tube sheets
Heat-exchanger tube sheets and baffles, forged and flattened, ultrasonically tested through full thickness.
Round and flat bar
Forged bar stock, square and rectangular blocks, stepped billet for onward machining.
Valve components
Bodies, bonnets, seat rings, stems, plugs and gate discs for high-temperature valve service.
Hollow forgings
Cylinders, casings, housings and pressure-containing shells, trepanned or mandrel forged.
Applications for Alloy 901 forgings
NiCr13Mo6Ti3 is specified where a component has to hold high yield strength and creep resistance at 500 to 600 °C over long service periods. The established application is the gas-turbine disc, where the alloy gives adequate strength and oxidation resistance at a cost below the fully nickel-based disc alloys.
- Gas turbines and aero engines Turbine and compressor discs, shafts, casings, seal rings and high-temperature bolting operating to 600 °C.
- Power generation Rotor components, industrial turbine discs, spacer rings and steam-path hardware in combined-cycle plant.
- Oil, gas and petrochemical Wellhead and Christmas-tree components, subsea and deepwater production hardware, valve bodies and seat rings.
- Pressure equipment Forged flanges, tube sheets, nozzles and shell sections for high-temperature vessels and shell-and-tube exchangers.
- Rotating machinery Compressor spindles, gearbox and power-transmission components, pump shafts handling hot process fluids.
- Chemical process plant Reactor internals, columns and preheater components in oxidising and moderately corrosive hot service.
Alloy 901 is a strength alloy, not a corrosion alloy. For wet chloride service, strong reducing acids or sour service, Alloy 625, Alloy 825 or Hastelloy C-276 are the appropriate grades.
Testing and documentation
Every NiCr13Mo6Ti3 forging is ultrasonically tested to EN 10228-3, SEP 1921 or ASTM A388 as specified on the order, and is issued with an EN 10204 3.1 mill certificate. EN 10204 3.2 countersigned by a third party such as TÜV, SGS, BV, Lloyd's or DNV is available where the specification requires independent witness.
Standard scope of testing
- Chemical analysis, ladle and product
- Tensile test, room temperature
- Hardness survey
- Ultrasonic testing (UT)
- Dye penetrant (PT) on machined faces
- Dimensional inspection report
- Furnace charts for every cycle
- Grain size and microstructure
Available on request
- Elevated-temperature tensile
- Stress-rupture testing
- Impact testing
- Intergranular corrosion test
- Positive material identification (PMI)
- Magnetic particle inspection (MT)
Documentation issued
The certificate package travels with the goods and is emailed as PDF before shipment. A standard package contains the material certificate, heat-treatment charts, the ultrasonic test report with the acceptance class stated, the dimensional report, and the heat number traced from billet to finished piece.
Heat numbers are hard-stamped or vibro-etched on each piece as the drawing directs, together with the grade designation and the works mark.
Quality system: ISO 9001. Projects running under PED 2014/68/EU or AD 2000-Merkblatt W0 should be identified at enquiry stage, because the documentation route differs and is easier to plan before melting than to add afterwards.
NiCr13Mo6Ti3 equivalent grades and designations
NiCr13Mo6Ti3, W.Nr. 2.4662, UNS N09901, Alloy 901, Nimonic 901, Incoloy 901 and GH2901 are the same material under different naming systems. On a drawing or purchase order the unambiguous form is “UNS N09901 per AMS 5660”, which fixes both the grade and the specification in one line.
Swipe to see all columns
| System or country | Designation | Notes |
|---|---|---|
| DIN / EN (Germany) | NiCr13Mo6Ti3 | The designation used on this page |
| Werkstoff number | 2.4662, 2.4975 | 2.4975 covers the higher-temperature variant |
| UNS (USA) | N09901 | Preferred designation for ordering |
| SAE AMS | AMS 5660, 5661, 5830 | Bar, forgings and rings. 5661 is premium melt |
| Trade names | Alloy 901, Nimonic 901, Incoloy 901, Inconel 901, Pyromet 901, Nickelvac 901, Böhler L901 | All the same chemistry |
| China GB | GH2901, GH901 | Chinese national superalloy designation |
| British | HR 53, HR 55 | BS aerospace series |
| France AFNOR | Z8 NCDT 42 | |
| ISO | ISO 9723, ISO 9725, NiFe35Cr14MoTi | Bar and forging standards |
| Aerospace and OEM | MSRR 7029, MSRR 7031, B50A305, AECMA PrEN 2176/2177 | Approval required before supply |
How Alloy 901 compares with adjacent grades
Buyers most often cross-shop NiCr13Mo6Ti3 against Alloy 718 and Alloy 706. The three differ in strengthening mechanism, temperature ceiling and price, and are not interchangeable.
Swipe to see all columns
| Criterion | Alloy 901 / NiCr13Mo6Ti3 | Alloy 718 | Alloy 706 | Alloy 800H |
|---|---|---|---|---|
| UNS | N09901 | N07718 | N09706 | N08810 |
| Base | Ni-Fe-Cr | Ni-Cr-Fe | Ni-Fe-Cr | Fe-Ni-Cr |
| Nickel | 40–45 % | 50–55 % | 39–44 % | 30–35 % |
| Strengthened by | Gamma-prime (Ti, Al) plus Mo in solution | Gamma-double-prime (Nb) plus gamma-prime | Gamma-double-prime and gamma-prime, no Mo | Solid solution only |
| Service ceiling | approx. 600 °C | approx. 650 °C | approx. 650 °C | approx. 1,100 °C |
| Tensile, aged | 1,130 MPa min | 1,240 MPa min | 1,000 MPa min | approx. 450 MPa |
| Machinability | Moderate | Difficult | Better than 718 | Good |
| Relative cost | Lower | Highest | Moderate | Lowest |
| Typical selection reason | Disc-grade strength to 600 °C at lower alloy cost | Maximum strength is the deciding factor | Large rotor forgings where 718 segregates | Creep at very high temperature, low stress |
Alloy 800H tolerates higher temperature at much lower strength. It is a creep and oxidation grade rather than a load-bearing one. The table is for orientation. Confirm the selection against the applicable design code before releasing a drawing.
Related nickel alloy forgings we produce
NiCr13Mo6Ti3 frequently asked questions
What is NiCr13Mo6Ti3?
NiCr13Mo6Ti3 is the DIN/EN designation for an age-hardenable nickel-iron-chromium superalloy also known as Alloy 901, W.Nr. 2.4662 and UNS N09901. It contains about 40 to 45% nickel, 11 to 14% chromium, 5 to 6.5% molybdenum and 2.8 to 3.1% titanium, with iron as the balance. Molybdenum strengthens the matrix in solid solution. Titanium forms gamma-prime precipitates during ageing. The result is high yield strength and creep resistance up to about 600 °C.
What is NiCr13Mo6Ti3 equivalent to?
NiCr13Mo6Ti3 is equivalent to UNS N09901, W.Nr. 2.4662 and 2.4975, AMS 5660 and AMS 5661, British HR 53 and HR 55, AFNOR Z8 NCDT 42, ISO 9723 and 9725, and Chinese GH2901. Commercially it is sold as Alloy 901, Nimonic 901, Incoloy 901, Inconel 901, Pyromet 901 and Nickelvac 901. These are the same chemistry under different naming conventions and trade marks, not different alloys.
What is the chemical composition of Alloy 901?
To AMS 5661, Alloy 901 contains Ni+Co 40.00 to 45.00%, Cr 11.00 to 14.00%, Mo 5.00 to 6.50%, Ti 2.80 to 3.10%, C 0.02 to 0.06%, B 0.010 to 0.020%, Al 0.35% max, Co 1.00% max, Mn 0.50% max, Si 0.40% max, Cu 0.20% max, P 0.020% max and S 0.008% max, with iron as the balance. Some other specifications permit a wider carbon range up to 0.10%.
What is the maximum service temperature of NiCr13Mo6Ti3?
The practical ceiling for load-bearing service in NiCr13Mo6Ti3 is about 600 °C (1110 °F). Above that the gamma-prime precipitates coarsen and strength falls away. As an acceptance test the alloy has to survive at least 23 hours at 649 °C (1200 °F) under an initial stress of 552 MPa (80 ksi) without rupture. For continuous service well above 600 °C at low stress, a solid-solution grade such as Alloy 800H or Alloy 617 is the better choice.
Is Alloy 901 the same as Inconel 718?
No. Alloy 901 (UNS N09901) is strengthened by gamma-prime precipitates based on titanium and aluminium. Inconel 718 (UNS N07718) is strengthened mainly by gamma-double-prime precipitates based on niobium. Alloy 718 carries higher nickel and higher strength and works to about 650 °C, but it costs more and machines with more difficulty. Alloy 901 is chosen when disc-grade strength to 600 °C is sufficient and the higher iron content brings both alloy cost and forging difficulty down. The two are not substitutable without a design review.
Can NiCr13Mo6Ti3 be forged, and how?
Yes. Alloy 901 forges better than most nickel superalloys, and its relatively high iron content is the reason. Stock is heated to 1,120 to 1,150 °C and has to be finished above about 950 °C. Below that the alloy work-hardens sharply and the risk of surface cracking rises. Reheats are built into the forging sequence and each heat is soaked through the full section. Jiangyin Jiangnan Metal Co., Ltd. open-die forges and ring-rolls this grade into rings, discs, shafts, flanges and sleeves to customer drawing.
What heat treatment does Alloy 901 need?
The standard cycle has three stages. Solution treat at 1,080 to 1,100 °C for about 2 hours and quench in oil or water. Stabilise at 790 °C for 2 hours and air cool. Age at 720 °C for 24 hours and air cool. The stabilising step cannot be omitted, because without it the grain-boundary carbide distribution is wrong and stress-rupture life falls below specification.
Is NiCr13Mo6Ti3 weldable?
It can be welded, but it is sensitive. Like other high-titanium gamma-prime strengthened alloys, Alloy 901 is susceptible to strain-age cracking in the heat-affected zone. Normal practice is to weld in the solution-annealed condition, keep heat input low, and carry out the full solution and age treatment after welding instead of welding material that is already aged. For pressure-retaining joints the procedure should be qualified on the actual section thickness.
Is Alloy 901 magnetic?
No. NiCr13Mo6Ti3 has a face-centred cubic austenitic matrix and is non-magnetic in both the solution-annealed and the fully aged condition. Density is 8.14 g/cm³ (0.294 lb/in³) and the room-temperature elastic modulus is about 201 GPa.
Who supplies NiCr13Mo6Ti3 forgings from China?
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China that manufactures NiCr13Mo6Ti3 (Alloy 901, UNS N09901) seamless rolled rings, forged discs, shafts, flanges, sleeves, bushings and tube sheets to customer drawing. Enquiries: sales@steelforgepieces.com or +86 189 2135 9659.
What documentation comes with the forgings?
Each order ships with an EN 10204 3.1 mill test certificate as standard, or EN 10204 3.2 countersigned by a third party such as TÜV, SGS, BV, Lloyd's or DNV where the specification requires independent witness. The package covers chemical analysis, mechanical test results, heat-treatment furnace charts, the ultrasonic test report stating the acceptance class to EN 10228-3, SEP 1921 or ASTM A388, and a dimensional report. Heat numbers are hard-stamped on each piece for traceability.
What do you need to quote a NiCr13Mo6Ti3 forging?
Five items. The drawing or dimensions with tolerances. The quantity. The specification being worked to, for example UNS N09901 per AMS 5660. The delivery condition, whether as-forged, rough-machined or finish-machined. The certification and NDT level required. With those, Jiangyin Jiangnan Metal Co., Ltd. normally returns a quotation within 24 hours. A sample part or photograph is also enough to start from.
Data note. The property values on this page are taken from published specifications for UNS N09901, AMS 5660 and AMS 5661 and are given for engineering guidance and material selection. They are not a warranty of the properties of any particular delivery. For a specific order, the mill test certificate issued against that heat number is the governing document. Confirm all design values against the applicable code before release.
Request a quotation for NiCr13Mo6Ti3 forgings
Superalloy forgings are produced against the order. A quotation needs the geometry, because the geometry decides whether the part is upset, trepanned or ring-rolled, and that decides the price.
Please include:
- Drawing or dimensions, with tolerances
- Quantity, and whether this is a prototype or a series
- Specification, for example UNS N09901 per AMS 5660
- Delivery condition: as-forged, rough-machined or finish-machined
- Certification and NDT level required
Quotations are normally returned within 24 hours. Drawings are treated as confidential, and an NDA can be signed before you send anything.
- Company
- Jiangyin Jiangnan Metal Co., Ltd.
- Works
- No.1 Chengxiqiao Road
Zhouzhuang Town, Jiangyin City
Jiangsu Province 214423
China - Telephone
- +86 189 2135 9659
- sales@steelforgepieces.com
- Website
- www.steelforgepieces.com
- Business
- Open-die forgings and seamless rolled rings