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Comprehensive List of Common Nickel-Base Alloy Grades

14:38:04 07/17/2026

Nickel-base alloys are not a single material class but a structured family divided by strengthening mechanism (solid-solution vs. precipitation-hardened), service temperature band, and stress environment. Correct grade selection depends on whether the component sees ≤650°C high stress (rotating), 650–870°C creep, 900–1040°C oxidation-dominated static load, or aggressive aqueous corrosion. This article lists the commercially important wrought nickel-base grades with precise cross-references, strengthening type, and temperature ceiling — for engineering screening, not marketing claims.


1. Solid-Solution Strengthened Nickel-Base Alloys (No γ′/γ″, Weldable, Low Creep Strength)

These rely on Cr, Mo, W, Fe, Co in the FCC matrix. They are chosen for oxidation/corrosion resistance, fabricability, and low-stress high-temperature service, not for high creep strength.

Trade / UNS

W.Nr.

China (GB)

Key Chemistry

Continuous Oxidation Limit

Typical Long-Term Service T

Typical Use

Inconel 600 / N06600

2.4816

GH3600 / NS312

72Ni-16Cr-8Fe

~1000°C

≤ 800°C (low stress)

Furnace parts, nuclear steam-generator tubing, chlorination equipment

Inconel 601 / N06601

2.4851

GH6010

60Ni-23Cr-1.5Al

~1030°C

≤ 950°C

Heat-treat baskets, burner rings

Inconel 625 / N06625

2.4856

GH3625 / NS336

58Ni-21Cr-8Mo-3.5Nb

~980°C

≤ 900°C (low stress)

Marine exhaust, bellows, transition ducts

Inconel 617 / N06617

2.4663

52Ni-22Cr-12Co-9Mo

~1050°C

900–950°C static

Combustor liners, reformer internals

Hastelloy X / N06002

2.4665

GH3536

47Ni-22Cr-9Mo-1.5Co(low)

~1040°C

870°C loaded / 950°C static

Welded combustor liners, furnace rollers

Alloy 800H / 800HT / N08810-11

1.4958 / 1.4959

GH140 (near)

32Ni-21Cr-46Fe

~900°C

≤ 600°C pressure / ≤ 850°C furnace

Pyrolysis tubes, headers

Hastelloy C-276 / N10276

2.4819

NS334

57Ni-16Cr-16Mo-4W

~950°C (not a high-T creep grade)

≤ 650°C (corrosion priority)

FGD, acid mix, chlorinated reductive media

Rule: Solid-solution grades have no precipitation hardening. Above 650°C under load, their creep strength is 1/3–1/5 of γ′-hardened grades.


2. Precipitation-Hardened Nickel-Base Alloys (γ″ or γ′ Strengthened)

These require solution + aging (sometimes multi-stage). They carry rotating and high-stress hot-section parts.

Trade / UNS

W.Nr.

China (GH)

Strengthening Phase

(Al+Ti)/Nb

Creep-Primary Band

Representative Part

Inconel 718 / N07718

2.4668

GH4169

γ″(Ni₃Nb) + γ′

Nb 4.75–5.50%

≤ 650°C​ (γ″ dissolves >680°C)

Turbine disks, compressor disks, bolts

Inconel X-750 / N07750

2.4669

GH4145

γ′(Ni₃(Al,Ti))

Al+Ti ≈ 3.5%

600–700°C

Valve springs, lock rings, nuclear fasteners

Nimonic 75 / N06075

2.4630

GH3033 (near)

None (SS + carbide)

Ti 0.4%

≤ 800°C low stress

Flame tubes, furnace sheets (legacy)

Nimonic 80A / N07080

2.4631

GH4080A

γ′

Al+Ti 3.4–4.2%

650–800°C

Legacy blades, valve springs, nuclear supports

Nimonic 90 / N07090

2.4632

GH4090

γ′ (Co 18%)

Al+Ti 3.8–4.8%

650–870°C

Blades, NGVs, high-temp springs

Nimonic 263 / N07263

2.4650

GH5263 (ref.)

γ′ (low Ti, SAC-resistant)

Al+Ti ≈ 0.5%+Co20%

650–815°C welded sheet

Combustor liners, welded fabrications

Waspaloy / N07001

2.4654

GH4738 (old GH738)

γ′ (Co 13.5%, Mo 4.2%)

Al+Ti 4.0–4.8%

650–870°C (disk-grade)

HP turbine disks, shafts, seals

René 41 / N07041

GH4141

γ′ (high Al+Ti≈5%)

Al+Ti ≈ 5%

750–950°C

Legacy forged blades, space hot structures

Key physical anchors:

  • Inconel 718: density 8.19–8.24 g/cm³, melt 1260–1336°C, Rm ≥1275 MPa (aged), 650°C/415 MPa rupture ≈ 100–300 h.

  • Nimonic 90: density 8.18 g/cm³, melt ~1370°C, 750°C/240 MPa rupture ≈ 1000–2000 h, 870°C/100 MPa ≈ 500–1000 h.

  • Waspaloy: density 8.19 g/cm³, melt 1330–1365°C, 760°C/240 MPa rupture ≈ 1000 h class, 815°C/131 MPa ≈ 1000 h class; three-stage HT 1080°C→845°C×4–24h→760°C×16h mandatory.


3. Temperature-Band Selection Cut (Fast Screen)

  • ≤ 650°C, high stress, rotative:Inconel 718 (GH4169)​ — peak yield ~1035 MPa, weldable, thick-section quench capable.

  • 600–700°C springs/fasteners (non-rotating):​ Inconel X-750 or Nimonic 80A.

  • 650–815°C disks/shafts:Waspaloy (GH4738)​ — γ′ solvus ~1000–1020°C, needs 845°C stabilization to block η(Ni₃Ti).

  • 650–870°C blades/NGVs/springs:Nimonic 90​ — Co 18% raises γ′ solvus, double-age (700–750°C + 650°C).

  • 700–950°C welded thin-sheet, low stress:Hastelloy X​ (best weldability) or Nimonic 263​ (if post-weld age without SAC is required).

  • 900–1040°C static oxidizing:​ Inconel 617, Hastelloy X; above 1040°C cyclic → Co-base (Haynes 188) or Al₂O₃-former (Haynes 214) or TBC + single-crystal Ni.

  • Aqueous corrosion priority (≤200°C acid, ≤650°C sour):​ Hastelloy C-276 / C-22, not a high-T creep grade.


4. Cross-Grade Mapping Pitfalls

  • GH738 = GH4738 = Waspaloy (N07001); old drawings say GH738, new GB/T 14992 says GH4738 — same melt spec.

  • GH4169 = Inconel 718, GH3625 = Inconel 625, GH3600 = Inconel 600, GH3536 = Hastelloy X.

  • Nimonic 263 ≠ Nimonic 90: 263 is low-Ti, Co20Mo6, designed for welded sheet; 90 is high-Ti blade/spring grade, Co18 no Mo (or trace).

  • Inconel 718 ≠ X-750: 718 is Nb-γ″ dominated (dies above 650°C in creep); X-750 is Al+Ti γ′ spring grade.

  • Hastelloy X is Ni-base (GH3536); Haynes 188 is Co-base (GH5188)​ — do not pool by trade-name prefix.


5. Heat-Treatment State Must Be On The PO

Precipitation grades are undefined without HT state:

  • Inconel 718:​ Solution + 720°C×8h/F.C. to 620°C×8h (double-age).

  • Nimonic 90:​ 1080–1150°C solution + 700–750°C×16h + 650°C×16h (double-age).

  • Waspaloy:​ 1080°C solution (oil/water quench) + 845°C stabilization 4–24h​ + 760°C×16h. Omitting 845°C step risks η-phase embrittlement in 10⁴ h service.

  • Nimonic 80A:​ 1080°C solution + 700°C×16h single-age (no Co, lower γ′ solvus ~950°C).

  • Solid-solution grades: annealed only; no aging.


6. Summary Table — One-Line Grade Index

Grade

UNS

GH

Strengthening

Prime Band

Never Use For

Inconel 600

N06600

GH3600

SS

≤800°C corroding

High creep load >600°C

Inconel 625

N06625

GH3625

SS+Mo/Nb

≤900°C static

Rotating disk >650°C

Hastelloy X

N06002

GH3536

SS

870°C loaded

Blade with 870°C centrifugal stress

Inconel 718

N07718

GH4169

γ″+γ′

≤650°C

750°C turbine disk

Nimonic 80A

N07080

GH4080A

γ′

650–800°C

>815°C sustained

Nimonic 90

N07090

GH4090

γ′+Co

650–870°C

Welded combustor liner

Nimonic 263

N07263

GH5263

γ′ low-Ti

650–815°C welded

High centrifugal disk

Waspaloy

N07001

GH4738

γ′+Co/Mo

650–870°C disk

Large thin-wall weldment

Inconel 617

N06617

SS+Co

900–950°C static

High-stress rotor

Hastelloy C-276

N10276

NS334

SS (corrosion)

≤650°C sour

Oxidizing 900°C


Nickel-base alloy selection is a 3-axis cut: metal temperature × sustained stress × atmosphere. No single grade covers 650–1100°C with high stress. Inconel 718 owns ≤650°C rotative; Waspaloy and Nimonic 90 own 650–870°C creep; Hastelloy X / Inconel 617 own 900–1040°C static oxidizing; beyond that, coating or Co-base/CMC takes over.

Shanghai COCESS Special Alloys Co., Ltd. supplies Inconel 600/625/617/718/X-750, Hastelloy X/C-276, Nimonic 80A/90/263, Waspaloy (GH4738) in bar, forging, plate, wire with EN 10204 3.1 MTR and AMS/ASTM/GB cross-compliance.

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