Jiangyin Jiangnan Metal Co., Ltd. Open-Die Forging Factory · Jiangsu, China · Est. 1997
Nickel Alloy · Low-Expansion Superalloy · Open-Die Forgings

Alloy 783 Forgings

Seamless rolled rings, discs, shafts, sleeves, seal rings and turbine casings forged to order in Alloy 783, the oxidation-resistant, low-thermal-expansion Ni-Co-Fe superalloy used for gas turbine clearance control.

UNS
R30783
AMS (billet)
AMS 5940
China grade
GH6783
Also called
Inconel 783
Density
7.81 g/cm³
Max service
≈704 °C

Overview

Alloy 783 (UNS R30783), also sold as Inconel 783 and designated GH6783 in China, is an age-hardenable nickel-cobalt-iron superalloy containing roughly 28% nickel, 34% cobalt, 26% iron, 5.5% aluminium, 3% niobium and 3% chromium. Its coefficient of thermal expansion is about 20% lower than Inconel 718, and its high aluminium content forms a protective alumina scale that resists oxidation and stress-accelerated grain-boundary oxidation at temperature. Gas turbine designers use that combination to hold tighter running clearances, which raises power output and fuel efficiency.

Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory in Jiangyin, Jiangsu Province, China that produces Alloy 783 forgings to customer drawings: seamless rolled rings, discs and blanks, stepped shafts, hollow sleeves and bushings, blocks and plates, turbine seal rings, shrouds and casing sections, supplied rough-machined or finish-machined with EN 10204 3.1 or 3.2 certification. Enquiries: 0086-189-2135-9659 · sales@steelforgepieces.com.

Section 01

What is Alloy 783?

Alloy 783 is a precipitation-hardening superalloy built on a nickel-cobalt-iron base rather than the nickel-chromium base used by most heat-resistant alloys. Chromium is held down to 2.5-3.5% because chromium raises thermal expansion. Oxidation protection comes instead from 5-6% aluminium, which forms a tenacious alumina scale. The alloy was developed by Special Metals Corporation and is protected by U.S. Patent 5,478,417.

Strengthening comes from three phases working together: the γ′ Ni3(Al,Nb,Ti) precipitate, a grain-boundary β-NiAl phase, and the solid-solution matrix itself. The β-NiAl at the grain boundaries is what gives Alloy 783 its resistance to SAGBO, the notch-sensitivity failure mode that limits earlier low-expansion alloys such as Incoloy 909 in oxidising service.

Why engineers specify it

  • Clearance control. A mean coefficient of thermal expansion roughly 20% below Inconel 718 means casings and seal rings grow less as the engine heats, so blade-tip clearances can be set tighter.
  • Oxidation resistance without chromium. The aluminium-rich scale survives cyclic exposure where a low-chromium alloy would normally be disqualified.
  • Notch ductility. Resistance to SAGBO removes the notch-sensitivity penalty that forces designers away from other Invar-type superalloys.
  • Lower mass. At 7.81 g/cm³ the alloy is about 5% lighter than Inconel 718, which matters on rotating and flight hardware.
  • Forgeable. Hot-working behaviour is comparable to Inconel 718 and less restrictive than Incoloy 909, so large open-die and ring-rolled shapes are practical.

Designations and equivalents

Table 1. Alloy 783 designations
SystemDesignationNotes
UNSR30783Primary unified number
Trade nameINCONEL® alloy 783Special Metals Corporation
Common usageAlloy 783 · Inconel 783 · IN 783Used interchangeably in enquiries
China (GB)GH6783Chinese high-temperature alloy designation
AMSAMS 5940Forging billet
PatentUS 5,478,417Original alloy patent

Naming note: INCONEL and INCOLOY are registered trademarks of Special Metals Corporation. Jiangyin Jiangnan Metal Co., Ltd. is an independent forging factory and uses these names only to identify the chemistry a customer has specified.

Section 02

Chemical composition

Cobalt is the balance element and typically lands near 34%. Every heat we forge is supplied with a certified ladle analysis and, on request, a product analysis taken from the forging itself.

Table 2. Limiting chemical composition, % by weight
ElementSymbolMinMaxNominal
NickelNi26.030.028.5
CobaltCoBalance34.0
IronFe24.027.025.5
AluminiumAl5.06.05.4
ChromiumCr2.53.53.0
NiobiumNb2.53.53.0
TitaniumTi0.10.40.3
BoronB0.0030.0120.005
CarbonC-0.030.02
ManganeseMn-0.50-
SiliconSi-0.50-
CopperCu-0.50-
PhosphorusP-0.015-
SulfurS-0.005-
Section 03

Physical properties

Table 3. Physical constants, Alloy 783
PropertyMetricImperial
Density7.81 g/cm³0.282 lb/in³
Melting range1336-1407 °C2437-2565 °F
Specific heat455 J/kg·°C at 25 °C0.109 Btu/lb·°F at 77 °F
Modulus of elasticity≈144 GPa at 560 °C≈20.9 × 10³ ksi at 1040 °F
Mean CTE (indicative)≈12.2 × 10⁻⁶ /°C to 560 °C≈6.8 × 10⁻⁶ /°F to 1040 °F
Max useful temperature≈704 °C≈1300 °F
Crystal structureFCC γ matrix with γ′ and grain-boundary β-NiAl
Magnetic responseFerromagnetic at room temperature

Thermal expansion needs one caveat. Like other Invar-type materials, Alloy 783 has an inflection temperature above which expansion climbs steeply toward normal alloy behaviour. Below the inflection the CTE is very low; above it the advantage narrows. Design against a CTE curve for your actual operating band rather than a single averaged number.

Section 04

Mechanical properties

Alloy 783 develops high room-temperature strength in the aged condition and holds a useful share of it to about 704 °C (1300 °F). The values below are typical for bar and forgings given the standard three-step heat treatment described in the next section.

Table 4. Typical tensile properties, fully heat treated
Test temperatureUTS0.2% yieldElongation
20 °C / 68 °F1140-1250 MPa790-890 MPa15-22%
427 °C / 800 °F1030-1120 MPa700-800 MPa15-22%
560 °C / 1040 °F-≈630 MPa-
649 °C / 1200 °F930-1030 MPa620-720 MPa12-20%
704 °C / 1300 °F830-950 MPa580-680 MPa12-20%

Note on these figures: they are typical published values for orientation and quotation, not specification minimums and not acceptance criteria. Section size, forging reduction, grain flow direction and test specimen location all shift results. Tell us the specification you are buying to, whether AMS 5940, a customer standard or your own drawing, and we will forge, heat treat and test to that document and report the certified numbers.

Section 05

Heat treatment cycle

Alloy 783 reaches its published properties only after a three-stage schedule: solution anneal, a high-temperature beta age that precipitates the grain-boundary β-NiAl phase, then a two-step age that develops the γ′ strengthening precipitate. The slow furnace cool between the two ageing holds controls the size distribution of the γ′ precipitate and cannot be shortened.

Standard heat treatment temperature profile for Alloy 783 Temperature versus process order with three stages: solution anneal at 1121 degrees Celsius for 1 hour then air cool; beta age at 845 degrees Celsius for 4 hours then air cool; age harden at 718 degrees Celsius for 8 hours, furnace cool at 55 degrees Celsius per hour to 621 degrees Celsius, hold 8 hours, then air cool. TEMPERATURE PROCESS ORDER (NOT TO SCALE) RT 1121 °C / 1 h 845 °C / 4 h 718 °C / 8 h 621 °C / 8 h AC AC AC FC 55 °C/h 1 · SOLUTION ANNEAL 2 · BETA AGE 3 · TWO-STEP AGE
Standard heat treatment for Alloy 783 (UNS R30783). AC = air cool, FC = furnace cool.
Table 5. Standard heat treatment schedule
StageTemperatureHoldCooling
1. Solution anneal1121 °C / 2050 °F1 hourAir cool
2. Beta age845 °C / 1550 °F4 hoursAir cool to room temperature
3a. Age harden718 °C / 1325 °F8 hoursFurnace cool at 55 °C/h (100 °F/h)
3b. Second age621 °C / 1150 °F8 hoursAir cool

Hot working

The practical hot-working window for Alloy 783 runs from about 927 °C to 1121 °C (1700-2050 °F). We plan forging passes to keep the workpiece inside that band, with reheats scheduled so the final reduction still occurs above the lower limit. Finishing too cold is the usual cause of a rejected superalloy forging.

Section 06

Alloy 783 vs Inconel 718 vs Incoloy 909

These three alloys compete for the same turbine hardware, and the choice usually comes down to how much thermal growth the design can tolerate against how much oxidation the part will see.

Table 6. Selection comparison
CriterionAlloy 783Inconel 718Incoloy 909
UNSR30783N07718N19909
Base systemNi-Co-FeNi-Cr-FeFe-Ni-Co
Thermal expansionLow, about 20% below 718BaselineLowest of the three
Oxidation resistanceExcellent (alumina scale)Excellent (chromia scale)Poor, coating usually needed
SAGBO / notch sensitivityResistantResistantSusceptible
Room-temp strengthHighHighestModerate
Density7.81 g/cm³8.19 g/cm³8.30 g/cm³
ForgeabilityComparable to 718Well establishedMore restrictive
Relative costHigh (cobalt content)ModerateModerate
Typical choice whenClearance control in oxidising airMaximum strength matters mostLowest expansion, protected environment

Choose Inconel 718 when strength dominates, Incoloy 909 when expansion dominates and the part is protected, and Alloy 783 when a component needs both low expansion and bare-metal oxidation resistance. Jiangyin Jiangnan Metal forges all three. See Inconel 718 forgings and the full nickel alloy index.

Section 07

Alloy 783 forged products we make

Jiangyin Jiangnan Metal Co., Ltd. forges Alloy 783 to customer drawings on open-die presses and radial-axial ring mills. Everything below is made to order. There is no stock catalogue for this grade, because superalloy forgings are bought against a drawing and a specification.

Where the metal comes from

Most forging shops in China buy superalloy billet from a third party, which is what drives cost and lead time on grades like this one. Alloy 783 is melted here. The chemistry is aimed at the forging it will become, and the certificate traces back to a melt number rather than to a purchased billet.

Table 7. Melting and solution-treatment equipment used for Alloy 783
FurnaceCapacityRole for this grade
Vacuum induction melting (VIM)3 tPrimary melt; controls aluminium, niobium and titanium recovery and gas content
Vacuum arc remelting (VAR)6 tSecond melt for VIM + VAR double-melt specifications
Electroslag remelting (IGESR)3 t and 6 tProtective atmosphere; alternative or third melt for ingot cleanliness
High-temperature car-bottom furnace3500 x 1300 x 1100 mm, 3 offSolution anneal at 1121 °C and both ageing steps

Shapes and working envelope

The envelope below is the plant limit, set by the presses, ring mills and machine tools. For Alloy 783 the binding constraint usually sits further upstream: superalloy ingot comes from the 3 t vacuum induction furnace and the 6 t remelting furnaces, so practical single-piece weight for this grade follows ingot size rather than press capacity. Solution annealing is limited to the 3500 x 1300 x 1100 mm working chamber of the high-temperature furnaces.

Table 8. Forged shapes and working envelope
Product formEnvelopeSet by
Seamless rolled ringsOD 50-6000 mm1 m, 3 m and 6 m radial-axial ring mills
Forged ringsSections outside the ring-mill rangeUpset and punch route
Discs, blocks and platesto 5000 mm diameter machined5000 mm swing vertical turning lathe
Round, square and flat barsto 1600 mm diameterCNC lathe, 1600 x 3300 mm
Hollow bars, sleeves and bushingsto 1600 x 10000 mm boredCNC deep-hole drilling machine
Shafts and stepped shaftsto 14000 mm turned lengthC61160 lathe; 15 m well furnace for vertical quench
Cylinders, casings and shellsBy drawingBored from solid forged blanks
Single piece weight, plant10 kg to 30000 kg60 t maximum heat; 6300 t press
Single piece weight, Alloy 783Governed by ingot size3 t VIM and 6 t VAR / ESR route

Supply condition and testing

  • Condition: as-forged, solution annealed, or fully heat treated to the three-stage cycle in Section 05.
  • Melt route: VIM, VIM + VAR double melt, or VIM + ESR, as the specification requires.
  • Surface: black scale, shot blasted, rough turned or bored, or finish machined to drawing.
  • NDT: ultrasonic inspection, dye penetrant, dimensional report; hardness and mechanical testing per specification.
  • Certification: EN 10204 3.1 as standard; 3.2 with third-party witness (SGS, BV, TÜV, Lloyd's) on request.
  • Traceability: heat number stamped or vibro-etched on every piece, tied to the mill certificate.

Applications

Alloy 783 forgings go into aircraft and industrial gas turbines, steam turbines and rotating equipment where dimensional stability at temperature decides efficiency: compressor casings and shroud rings, turbine seal rings and clearance-control hardware, exhaust system components, high-temperature bolting, valve spindles and stems, and impeller and disc blanks.

Section 08

How to specify an Alloy 783 forging

Superalloy quotations stall on missing information more often than on price. Send these eight items and a firm quotation normally follows within two working days.

  1. Grade and specification. Alloy 783 / UNS R30783 / GH6783, plus the governing document: AMS 5940, a customer standard, or your own drawing.
  2. Drawing or dimensions. A finished part drawing is best; otherwise rough dimensions plus the machining allowance you want left on.
  3. Quantity and delivery date. Piece count now and expected annual volume, since melt sizing depends on it.
  4. Supply condition. As-forged, solution annealed, or fully aged.
  5. Heat treatment requirement. Confirm whether the standard three-stage cycle applies or a modified schedule is specified.
  6. Testing and NDT. Which tests, at what temperatures, and from which specimen location and orientation.
  7. Certification. EN 10204 3.1 or 3.2, and any third-party inspection required.
  8. Destination port. For an accurate FOB, CIF or DDP price.

Send your Alloy 783 drawing

Section 09

Frequently asked questions about Alloy 783

What is Alloy 783 used for?

Alloy 783 is used for gas turbine and steam turbine components where thermal growth must be controlled: seal rings, shroud rings, compressor and turbine casings, exhaust hardware, clearance-control rings, high-temperature bolting and valve spindles. Its low coefficient of thermal expansion lets designers set tighter running clearances, which improves power output and fuel efficiency.

Is Alloy 783 the same as Inconel 783?

Yes. INCONEL alloy 783 is the trade name used by Special Metals Corporation; Alloy 783, IN 783 and UNS R30783 all refer to the same chemistry. In China the equivalent designation is GH6783. Buyers use the names interchangeably, and a forging ordered under any of them is made to the same composition limits.

What is the UNS number for Alloy 783?

The UNS number for Alloy 783 is R30783. The R3 prefix places it among cobalt-base and cobalt-bearing heat-resistant alloys, which reflects the fact that cobalt is the balance element at roughly 34% rather than nickel. Forging billet is commonly ordered to AMS 5940.

What is the chemical composition of Alloy 783?

Alloy 783 contains 26.0-30.0% nickel, 24.0-27.0% iron, 5.0-6.0% aluminium, 2.5-3.5% chromium, 2.5-3.5% niobium and 0.1-0.4% titanium, with cobalt as the balance at about 34%. Carbon is held to 0.03% maximum and boron runs 0.003-0.012%. The full limiting composition is in Table 2 above.

What is the maximum service temperature of Alloy 783?

Alloy 783 retains a useful share of its strength to about 704 °C (1300 °F), which is the normal upper limit quoted for load-bearing service. Above that temperature the γ′ strengthening precipitate begins to coarsen and the low-expansion advantage narrows. Long-term exposure also produces a small dimensional shrinkage that should be accounted for in clearance-critical designs.

How is Alloy 783 heat treated?

The standard schedule has three stages: solution anneal at 1121 °C (2050 °F) for 1 hour and air cool; beta age at 845 °C (1550 °F) for 4 hours and air cool to room temperature; then age harden at 718 °C (1325 °F) for 8 hours, furnace cool at 55 °C per hour (100 °F per hour) to 621 °C (1150 °F), hold 8 hours and air cool.

Why does Alloy 783 have such low chromium?

Chromium raises the coefficient of thermal expansion, so low-expansion alloys built on Ni-Fe-Co compositions must keep it low. Alloy 783 holds chromium to 2.5-3.5%. Oxidation protection is provided instead by 5-6% aluminium, which forms a stable alumina scale. That substitution is what allows the alloy to be both low-expansion and oxidation-resistant in bare-metal service.

Can Alloy 783 be forged into large rings?

Yes. Alloy 783 has hot-working characteristics comparable to Inconel 718 and less restrictive than Incoloy 909, so it is routinely open-die forged and ring rolled. Jiangyin Jiangnan Metal Co., Ltd. produces seamless rolled Alloy 783 rings and discs to customer drawings, working within the 927-1121 °C (1700-2050 °F) hot-working window with scheduled reheats.

Do you melt Alloy 783 in-house or buy the billet?

It is melted on site. The works runs a 3 t vacuum induction furnace, a 6 t vacuum arc remelting furnace and 3 t and 6 t protective-atmosphere electroslag furnaces, so VIM, VIM + VAR double-melt and VIM + ESR routes for Alloy 783 are available without subcontracting. Most forging shops in China import superalloy billet for this grade, which adds both cost and lead time.

Who supplies forged Alloy 783 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, operating since 1997. It melts, forges, heat treats, machines and certifies Alloy 783 (UNS R30783 / GH6783) rings, discs, shafts, sleeves, blocks and casings on one site, with EN 10204 3.1 or 3.2 certification and CCS, BV, DNV, LR and NK approvals. Contact 0086-189-2135-9659 or sales@steelforgepieces.com.

What is the minimum order quantity for Alloy 783 forgings?

The minimum order is 10 kg by weight, with no minimum piece count, so a single prototype forging is quotable. Alloy 783 is made to order rather than stocked. Normal lead time runs 20 to 60 days from order confirmation, with superalloys at the upper end because the remelting cycle and the long solution and ageing treatments both add days.

Section 10

About the forging factory

Jiangyin Jiangnan Metal Co., Ltd. is an integrated melting works and open-die forging factory in Zhouzhuang Town, Jiangyin City, Jiangsu Province, operating since 1997. The plant employs 460 people, including 9 senior engineers, 32 intermediate engineers and 140 technicians, and holds CCS, BV, DNV, LR and NK approvals. We forge carbon steel, alloy steel, tool steel, stainless steel and nickel-base superalloys into rings, discs, shafts, sleeves, blocks and near-net-shape parts, working to customer drawings and international specifications.

For Alloy 783 we control the process from the furnace through forging, heat treatment, non-destructive testing and machining, and issue a mill certificate traceable to the melt number on every piece.

Company
Jiangyin Jiangnan Metal Co., Ltd.
Melting works and open-die forge
Established 1997
Address
No.1 Chengxiqiao Road
Zhouzhuang Town, Jiangyin City
Jiangsu Province, China
Telephone / WhatsApp
0086-189-2135-9659
Enquiries answered
Mon-Sat, 08:00-17:30 CST (UTC+8)

Technical data reviewed by the engineering team at Jiangyin Jiangnan Metal Co., Ltd. · Last updated