Introduction
GH3039 Superalloy (GH39) is a single-phase austenitic solid-solution strengthened nickel-chromium based superalloy with moderate thermal strength and good thermal fatigue performance below 800°C, and excellent oxidation resistance up to 1000°C. It offers good cold formability, good weldability, and a stable microstructure for long-term service below 850°C. Ideal for aircraft engine combustion chambers, afterburner components, and gas turbine casings. Available in sheet, plate, bar, wire, tube, and forgings per GB/T, ASTM, AMS, or BS standards.

Chemical components(%)
Composition | C | Si | Mn | P | S | Cr | Ti | Mo | Al | Nb | Fe |
Min | \ | \ | \ | \ | \ | 19.00 | 0.35 | 1.80 | 0.35 | 0.90 | \ |
Max | 0.08 | 0.80 | 1.00 | 0.02 | 0.012 | 22.00 | 0.75 | 2.30 | 0.75 | 1.30 | 3.00 |
Mechanical properties
Rigidity | Tensile strength | Yield strength | Elongation |
280HBS | ≥900MPa | ≥600MPa | ≥40% |
Physical properties
Density | Melting points | Specific heat | Magnetism | Resistivity | Thermal conductivity | Linear expansivity |
8.3g/cm3 | 1415-1450℃ | 544J/(Kg.℃) | \ | 1.18×10-6Ω·m (20℃) | 13.8W/(m.k) (100℃) | 11.5×10-6/K (20-100℃) |
GH3039 Superalloy Available Products and Standard
1. GB/T 14992 (Superalloys – Classification and Specifications)
Type:
GH3039 Alloy Plate
GH3039 Alloy Sheet
GH3039 Alloy Round bar
GH3039 Alloy Strip
GH3039 Alloy Tube
GH3039 Alloy Pipes
GH3039 Alloy Wire
GH3039 Alloy Forgings
Size Range:
Wire: 0.1 – 15.0 mm dia
Strip: 0.05 – 5.0 mm thick × 5 – 500 mm wide
Bar: 8 – 355 mm dia
Sheet / Plate: 0.5 – 180 mm thick
Tube: Custom sizes available
Surface: Annealed, Bright, Pickled, Ground
Testing: Chemical analysis, mechanical test (tensile strength, yield strength, elongation), high-temperature oxidation test, dimensional inspection

2. ASTM B564 (Standard Specification for Nickel Alloy Forgings)
Grade: GH3039 / Ni-Cr based solid-solution strengthened alloy
Type: Bar / Forging / Rod
Size Range:
Bar: 8 – 355 mm dia (hot rolled or cold drawn)
Forging: Custom sizes available per customer drawing
Surface: Annealed, Pickled, Ground, Turned
Testing: Chemical analysis, mechanical test (tensile, yield, elongation), high-temperature oxidation test, ultrasonic test, dimensional inspection

3. Reference Standards (Available Upon Request)
ASTM B446 – Nickel-Chromium-Molybdenum Alloy Bar
ASTM B704 – Nickel Alloy Welded Tube
ASTM B705 – Nickel Alloy Welded Pipe
ASTM B751 – Nickel Alloy Tube General Requirements
ASTM B775 – Nickel Alloy Pipe General Requirements
Advantages
(1)High temperature strength: As a single-phase austenitic solid-solution strengthened nickel-chromium based superalloy, it offers moderate thermal strength and maintains reliable performance below 850°C.
(2)Excellent oxidation resistance: The alloy provides excellent oxidation resistance up to 1000°C, forming a stable protective layer that prevents surface degradation in high-temperature environments.
(3)Good thermal fatigue performance: With good thermal fatigue performance below 800°C, it withstands cyclic thermal stress without cracking, ensuring long-term reliability.
(4)Stable microstructure: After prolonged service at elevated temperatures, the material retains a stable microstructure, minimizing property degradation over time.
(5)Excellent workability: Featuring good cold formability and good weldability, it supports complex forming and joining operations, making it suitable for intricate component designs.
(6)Corrosion resistance: The Ni-Cr based composition provides good resistance to corrosive media, complementing its high-temperature capabilities.
Applications
(1)Aviation sector – Widely used in aircraft engine combustion chambers and afterburner components, where high temperature strength and oxidation resistance are critical for performance and safety.
(2)Aerospace field – Applied in gas turbine casings and high-temperature structural parts for rockets and spacecraft, benefiting from its thermal stability and good weldability.
(3)Industrial furnaces – Suitable for heat exchanger components, furnace fixtures, and other equipment operating in high-temperature environments up to 900°C.
(4)Power generation – Used in gas turbine components where thermal fatigue resistance and stable microstructure ensure reliable long-term service.
(5)General high-temperature applications – Ideal for any application requiring a solid-solution strengthened nickel-chromium alloy with good formability and oxidation resistance up to 1000°C.

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