May 15, 2026 Leave a message

GH4169 Temperature Limits: Performance Guidelines from -253°C to 700°C

In high-risk fields such as aerospace, nuclear energy, and energy engineering, the material use window is a critical pain point. Purchasing managers often mistakenly believe that GH4169, with a melting point of 1260°C, is safe to use at 900°C.

 

The technical truth: The structural integrity of GH4169 (equivalent to Inconel 718) is closely related to its strengthening phase-γ′′ (γ′′). Once the temperature exceeds 750°C (1382°F), these precipitated phases begin to dissolve or transform. This is known as over-aging, which leads to a sharp drop in yield strength and component sagging.

 

At Gnee Alloy, we ensure your industrial durability by matching the material's metallurgical limits to your specific heat treatment profile.

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GH4169 Temperature Limits: Performance Guidelines from -253°C to 700°C
 

Gnee Alloy

 

GH4169 Temperature Limits: Performance Guidelines from -253°C to 700°C

GH4169 (similar to Inconel 718) is a precipitation-hardening nickel-based superalloy with high strength, excellent corrosion resistance, and good machinability. Its properties are optimized for applications ranging from extremely low temperatures to high temperatures (typically up to 650°C–700°C).

GH4169 Temperature Limits: Performance Guidelines from -253°C to 700°C

Gnee alloy

 

What is GH4169 equivalent to?

Inconel 718

GH4169 (equivalent to the American brand Inconel 718) is a precipitation-hardening nickel-based superalloy widely used in the aerospace industry due to its excellent mechanical properties (Lu et al., 2014).

GH4169 equivalent

1. GH4169 Temperature Limit Performance Guide

Optimal Operating Range (-253°C to 650°C): The alloy maintains high tensile strength, fatigue strength, creep strength, and fracture strength.

Maximum Operating Temperature (650°C to 700°C): Below 700°C, the long-term strength of the alloy begins to decrease, and the microstructure changes.

Structural Stability: The main strengthening phase γ′′ remains stable below approximately 650°C.

 

Performance of GH4169 over the temperature range
Cryogenic To Room Temperature (-253°C To 20°C)
02

Cryogenic to Room Temperature (-253°C to 20°C)

Performance: GH4169 exhibits excellent toughness and strength in cryogenic environments, including liquid hydrogen (-253°C) and liquid nitrogen (-196°C).

Application Guidelines: This alloy shows no tendency for brittle fracture at cryogenic temperatures, making it suitable for liquid-fueled rocket components.

03

Intermediate Temperature (20°C to 600°C)

Performance: This alloy maintains high strength and exhibits extremely high fatigue resistance and oxidation resistance.

Abrasion Resistance: Abrasion resistance increases slightly with temperature (e.g., at 525°C compared to room temperature).

Intermediate Temperature (20°C To 600°C)
High Temperature (600°C To 700°C)
04

High Temperature (600°C to 700°C)

Strength Limitation: Above 630°C, the material begins to soften.

Phase Transformation: Prolonged exposure to 650°C causes the γ" phase (strengthening phase) to transform into the stable β phase (δ phase), thus reducing the strengthening effect.
Creep Fracture: Excellent creep resistance is observed below 650°C/700 MPa, but this drops sharply at 700°C/660 MPa.

05

Extreme Temperatures (>700°C)

Oxidation: At 850°C, the surface oxide film becomes porous and easily peels off.
Usage Limitations: Long-term load-bearing applications above 700°C are not recommended as structural softening is accelerated.

Extreme Temperatures (>700°C)

 

6. GH4169 Temperature Range Matrix

Service Zone Temperature Range Performance Mode Typical Application
Cryogenic -253°C to 0°C Exceptional Toughness Liquid H2/O2 Storage.
Standard Heat Up to 650°C (1200°F) Peak Yield Strength Turbine discs, engine shafts.
Intermittent 700°C (1292°F) Critical Load Burst Short-term rocket motor service.
Oxidation Limit 980°C (1800°F) Resists Scaling; Zero Load Static thermal shields only.

 

7. Typical yield strength of GH4169 alloy (fully aged state)

Temperature (℃/°F) Yield Strength σp0.2 (MPa) Industrial Verdict
20°C (Room Temp) ≥ 1030 MPa Elite static load support.
540°C (1000°F) ≥ 950 MPa Highly stable structural integrity.
650°C (1200°F) ≥ 850 MPa Safe Limit for Continuous Load.
700°C (1292°F) ~ 700 MPa The "Danger Zone" (Over-aging begins).
850°C (1562°F) < 150 MPa FAILURE (Do not use for load).

 

8. Typical Applications of GH4169

Aerospace: Aircraft engine turbine disks, compressor shafts, and blades.

Power Generation: Critical components in ultra-supercritical (USC) systems.

Aircraft engine turbine disk
Aircraft engine turbine disk
Compressor shaft
Compressor shaft
Blade
Blade

 

Why Choose Gnee as Your Nickel-Based Alloy Supplier

✅️VIM + VAR melting: Eliminates trace impurities that lower the over-aging threshold, maximizing your Material Life Cycle.

✅️MTC 3.1 Traceability: Full heat-analysis and high-temperature tensile test results included.

✅️Ready-to-Ship Inventory: Large stock of solution-treated rods and sheets ready for immediate project dispatch.

✅️Custom Fabrication: We offer precision cutting and centerless grinding to match your assembly blueprints.

Gnee Alloy GH4169(inconel 718) Certificate

Gnee Alloy GH4169(inconel 718) Certificate

 

📦 Packaging and Shipping

All Nickel Based Alloy products are packaged using the following methods:

Wooden pallets or crates

Moisture-proof packaging

Labels with furnace number, standard, and size labels

Shipped worldwide by sea, air, or express

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 Gnee Alloy GH4169 Product Packing

Contact us for the latest export price quote for GH4169 Alloy

 

FAQ

 

Q1: Will GH4169 warp if it hits 800°C for only 10 minutes?
A: Short spikes are usually survivable without warping if the load is low. However, any exposure above 750°C triggers the irreversible Over-aging process. We recommend an NDT hardness check after such an event to verify remaining strength.

 

Q2: Is GH4169 better than 310S for 900°C furnace parts?
A: It depends. 310S is a basic heat-resistant steel better for non-load oxidation resistance up to 1000°C. GH4169 is a high-strength superalloy. If you need the part to hold its shape under pressure, GH4169 is superior up to 700°C, but neither is ideal for load-bearing at 900°C.

 

Q3: Does GH4169 maintain its properties at liquid nitrogen temperatures?
A: Absolutely. It is one of the premier Cryogenic Superalloys, maintaining excellent ductility and fracture toughness down to -196°C and even -253°C.

 

Q4: Do you offer bulk discounts for aerospace maintenance (MRO) projects?
A: Yes. As a leading Wholesale Supplier, we offer tiered pricing and priority inventory reserves for long-term contract partners.

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