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Special Alloys/High-Temperature Alloy/

GH4105 / GH105 Nickel-Based Superalloy: High-Temperature Strength for Extreme Environments

1. About GH4105 GH4105, also designated GH105 or Nimonic 105 (W.Nr. 2.4634), is a premium precipitation-hardened wrought nickel-cobalt-chromium superalloy that delivers exceptional tensile strength, outstanding high-temperature oxidation resistance, and a stable microstructure under sustained thermal cycling. It is purpose-engineered to operate reliably at continuous service temperatures ranging from 750 °C up to 950 °C, serving core extreme-condition scenarios including commercial and military aerospace engines, heavy-duty industrial gas turbines, clean energy power generation units, and high-temperature petrochemical equipment. 2. Key Features Excellent mechanical performance at elevated temperatures up to 950 °C High resistance to thermal fatigue and oxidation Good formability for precision manufacturing processes Long service life in demanding high-temperature environments Precipitation-hardened microstructure for superior creep-rupture strength 3. Applications Aerospace: Turbine…

  • Product Details

1. About GH4105

GH4105, also designated GH105 or Nimonic 105 (W.Nr. 2.4634), is a premium precipitation-hardened wrought nickel-cobalt-chromium superalloy that delivers exceptional tensile strength, outstanding high-temperature oxidation resistance, and a stable microstructure under sustained thermal cycling. It is purpose-engineered to operate reliably at continuous service temperatures ranging from 750 °C up to 950 °C, serving core extreme-condition scenarios including commercial and military aerospace engines, heavy-duty industrial gas turbines, clean energy power generation units, and high-temperature petrochemical equipment.

2. Key Features

  • Excellent mechanical performance at elevated temperatures up to 950 °C
  • High resistance to thermal fatigue and oxidation
  • Good formability for precision manufacturing processes
  • Long service life in demanding high-temperature environments
  • Precipitation-hardened microstructure for superior creep-rupture strength

3. Applications

  • Aerospace: Turbine blades, discs, and hot-section fasteners in jet engines, where resistance to high stress and temperature is critical.
  • Power Generation: Hot gas path components in industrial gas turbines, including blades and combustion hardware.
  • High-Temperature Petrochemical: Internal supports, bolting, and structural parts in reformers, crackers, and hydrogenation units operating up to 950 °C.
  • Nuclear & Clean Energy R&D: Structural internals for high-temperature gas-cooled reactors and advanced supercritical CO₂ power cycles.

4. C&N’s Complete Product Supply Forms & Size Range

Product FormThickness / Diameter RangeMain Application Scenario
Ultra-Thin FoilCustom ultra-thin thicknessPrecision electronics, micro thermal components, heat conduction thin films
Precision Strip0.1 mm – 3 mmHigh-precision thin-wall parts, aerospace small components
Plate / Sheet3 mm – 100 mm+Large structural components, furnace lining, heat exchanger plates
Bar & Solid RodCustom diameterMachined turbine parts, bolt fasteners, shaft components

5.GH4105 Chemical Composition

ElementPercentage (%)
Nickel (Ni)Balance (approx. 51–54)
Chromium (Cr)14.0 – 15.5
Cobalt (Co)18.0 – 22.0
Molybdenum (Mo)4.5 – 5.5
Aluminum (Al)4.5 – 4.9
Titanium (Ti)0.9 – 1.5
Iron (Fe)≤ 1.0
Carbon (C)≤ 0.12
Boron (B)0.003 – 0.01
Other ElementsTrace (e.g., Zr, Cu)

6.Physical Properties Of GH4105

PropertyTypical Value
DensityApproximately 8.2 g/cm³
Melting PointApproximately 1320 °C
Maximum Service TemperatureUp to 950 °C
Thermal StabilityExcellent
Oxidation ResistanceExcellent at elevated temperatures
Magnetic PropertyGenerally non-magnetic

7.Mechanical Properties (Room Temperature, Typical Aged Condition)

PropertyValue
Tensile Strength≥ 1000 MPa
Yield Strength (0.2% Offset)≥ 800 MPa
Elongation≥ 20 %
Hardness280 – 370 HB
Creep-Rupture StrengthExcellent at 950 °C (high stress-rupture life)

8.Heat Treatment

Proper heat treatment is essential to achieve the optimum precipitation-hardened condition and full mechanical performance of GH4105.

ProcessTypical Condition
Solution Annealing1150 – 1180 °C
CoolingAir Cool
First Stage Aging1025 – 1060 °C / 15–16 h, Air Cool
Second Stage Aging850 °C / 16 h, Air Cool
Final ConditionPrecipitation Hardened

This two-stage aging treatment maximizes the formation of gamma-prime precipitates, improving tensile strength, creep resistance, and long-term thermal stability.

9.Comparison of Hot and Cold Forming

ItemHot FormingCold Forming
Processing Temperature1050 – 1150 °CRoom Temperature
Forming ForceLowerHigher
Dimensional AccuracyModerateExcellent
Work HardeningLimitedSignificant
Grain ControlBetter for large partsSuitable for thin products
Typical ProductsForgings, plates, barsStrip, foil, precision parts

Why Choose Our GH4105 Products?

  • Premium nickel-based superalloy manufactured under strict quality control
  • Available in strip, foil, sheet, plate, bar, wire, and custom forgings
  • Excellent high-temperature strength up to 950 °C
  • Outstanding oxidation, creep, and fatigue resistance
  • Custom dimensions and precision machining available
  • Complete inspection reports and third-party certification upon request
  • Worldwide export experience with fast delivery and professional technical support

Contact Us today for a fast, competitive quote and check real-time stock availability.
Want to see our manufacturing and quality control firsthand? Visit our YouTube Channel for factory tours, PMI testing, and field performance videos.

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