In the realm of high-temperature alloys, GH4169 (equivalent to Inconel 718) is widely recognized as the king of strength-but its strength is not limitless. For purchasing managers and design engineers, the biggest challenge lies in its microstructural stability above 700°C.
At Gnee Alloy, we help you bridge this gap. When GH4169 reaches its metallurgical limits, Inconel 617 (Alloy 617) becomes the preferred solution for industrial durability in the high-temperature "red zone."
GH4169 vs Inconel 617: Temperature Performance Comparison at 700°C and 900°C

GH4169 vs Inconel 617: Temperature Performance Comparison at 700°C and 900°C
GH4169 (similar to Inconel 718) and Inconel 617 have different advantages depending on the temperature. GH4169 performs better below 650°C, while Inconel 617 performs better above 900°C.
What is the operating temperature of Inconel 617?
Inconel 617 (IN617) is a nickel-based superalloy with excellent oxidation resistance, corrosion resistance, and weldability under high-temperature conditions. IN617 can be used continuously at temperatures of 750 °C or below, and its maximum operating temperature can exceed 950 °C.

1. GH4169 and Inconel 617 Material Overview
| Parameter | GH4169 (Inconel 718) | Inconel 617 |
|---|---|---|
| UNS Number | N07718 | N06617 |
| Material Type | Wrought Nickel-based Superalloy | Wrought Nickel-based Superalloy |
| Strengthening Mechanism | γ″ + γ′ precipitation hardening | Solid-solution strengthening (Co + Mo) |
| Product Forms | Bar, forging, plate, tube, strip | Bar, plate, tube, strip |
| Typical Applications | Turbine discs, fasteners, shafts, high-strength components | Gas turbine combustors, afterburners, high-temperature heat exchangers |
| Maximum Service Temperature | ~650 – 700°C | ~900 – 950°C |
2. Comparison of chemical composition of GH4169 and Inconel 617 (wt%)
| Element | GH4169 (Inconel 718) | Inconel 617 | Key Difference |
|---|---|---|---|
| Nickel (Ni) | 50.0 – 55.0 | 44.5 min (Balance) | Similar |
| Chromium (Cr) | 17.0 – 21.0 | 20.0 – 24.0 | Inconel 617 higher Cr |
| Cobalt (Co) | ≤ 1.00 | 10.0 – 15.0 | 617 contains significant Co |
| Molybdenum (Mo) | 2.80 – 3.30 | 8.0 – 10.0 | 617 has ~3x more Mo |
| Iron (Fe) | Balance (~18-20) | ≤ 3.0 | GH4169 has much higher Fe |
| Niobium (Nb) | 4.75 – 5.50 | – | GH4169 unique – γ″ former |
| Titanium (Ti) | 0.65 – 1.15 | ≤ 0.6 | GH4169 higher |
| Aluminum (Al) | 0.20 – 0.80 | 0.8 – 1.5 | Inconel 617 higher |
| Carbon (C) | ≤ 0.08 | 0.05 – 0.15 | Inconel 617 higher |
| Manganese (Mn) | ≤ 0.35 | ≤ 1.0 | – |
| Silicon (Si) | ≤ 0.35 | ≤ 1.0 | – |
| Phosphorus (P) | ≤ 0.015 | ≤ 0.015 | Similar |
| Sulfur (S) | ≤ 0.015 | ≤ 0.015 | Similar |
| Boron (B) | 0.002 – 0.006 | ≤ 0.006 | Similar |
| Copper (Cu) | ≤ 0.30 | ≤ 0.5 | – |
Click to download the GH4169 alloy PDF file now
3. Comparison of high-temperature mechanical properties of GH4169 and Inconel 617
| Temp (°C) | Property | GH4169 (718) | Inconel 617 |
|---|---|---|---|
| 500 | Tensile (MPa) | ~1150 | ~680 |
| Yield (MPa) | ~950 | ~320 | |
| 600 | Tensile (MPa) | ~1100 | ~650 |
| Yield (MPa) | ~900 | ~310 | |
| 650 | Tensile (MPa) | ~1000 | ~630 |
| Yield (MPa) | ~850 | ~300 | |
| 700 | Tensile (MPa) | ~850 | ~600 |
| Yield (MPa) | ~750 | ~290 | |
| 800 | Tensile (MPa) | ~500 | ~550 |
| Yield (MPa) | ~450 | ~270 | |
| 900 | Tensile (MPa) | – | ~450 |
| Yield (MPa) | – | ~240 | |
| 950 | Tensile (MPa) | – | ~350 |
| Yield (MPa) | – | ~180 |
High-Temperature Strength Retention:
| Temperature | GH4169 Retention | Inconel 617 Retention |
|---|---|---|
| 500°C | ~90% | ~91% |
| 600°C | ~86% | ~87% |
| 650°C | ~78% | ~84% |
| 700°C | ~65% | ~80% |
Performance Comparison of GH4169 and Inconel 617 at 700°C

GH4169 (similar to IN718)
Strength: GH4169 exhibits excellent strength below 650°C, but at 700°C, the (Ni3Nb) strengthening phase begins to transform into the stable β phase, leading to significant softening and a decrease in creep resistance.
Oxidation: At this temperature, the protective oxide film remains largely intact, but it begins to show a tendency to accelerate oxidation under stress.
Inconel 617
Strength/Stability: As a solid solution strengthened alloy, 617 is stable at this temperature, exhibiting excellent strength and creep resistance.
Wear/Oxidation Resistance: 617 forms a very stable Cr,O2 oxide layer, exhibiting high resistance to sliding wear and oxidation at 700°C-750°C.

Conclusions at 700°C: Inconel 617 exhibits better long-term stability and creep resistance, while GH4169 can also be considered as an alternative. For cases with high initial yield strength, this is contingent on long-term phase instability not being a problem.
Performance Comparison of GH4169 and Inconel 617 at 900°C
At 900°C, Inconel 617 performs significantly better than GH4169 because GH4169 enters a temperature range that its structure cannot withstand.

GH4169
Failure Mechanism: At 900°C, the reinforcing phase of GH4169 rapidly coarsens and dissolves, leading to a significant decrease in mechanical strength.
Oxidation: The high iron (Fe) content in GH4169 hinders the formation of a continuous protective film at this temperature, resulting in the formation of loose, porous, and easily peeling oxides.
Inconel 617
Strength/Stability: Due to solid solution reinforcement (Mo, Co, Al), 617 maintains excellent structural integrity at 900°C.
Oxidation/Corrosion: 617 forms a dense, continuous NiO and Cr₂O₃ oxide layer. In corrosive solid oxide fuel cell (SOFC) environments, Inconel 617 is considered the preferred material for long-term service at 900°C, with performance significantly exceeding that of GH4169.

8. Summary of Temperature Performance of GH4169 and Inconel 617
700℃: GH4169 maintains high strength, but begins to show microstructural instability (softening) and decreased oxidation resistance. Inconel 617 is very stable and provides better long-term creep strength.
900℃: Inconel 617 performs better. GH4169 rapidly loses strength and oxidation resistance due to the dissolution of the γ'' phase, while 617 maintains its structural stability.
Why choose Tier 1 manufacturer Gnee Alloy?
Whether you need the peak power of GH4169 or the thermal endurance of 617, we ensure Zero-Defect quality:
✅️VIM + VAR Melting: Ensuring ultra-pure chemistry to eliminate trace impurities that trigger early over-aging.
✅️MTC 3.1 Traceability: Full heat analysis and creep-rupture test data included with every order.
✅️Wholesale Pricing: Benefit from Direct Factory Price on bulk tonnage for energy and aerospace overhauls.
✅️Global Logistics: Optimized logistics for Fast Global Shipping to major industrial hubs.

Contact us now to get the latest export price for GH4169 in 2026
FAQ
Q1: Can I weld Inconel 617 to GH4169?
A: Yes. Both have excellent weldability. We recommend using matching Inconel 617 (ERNiCrCoMo-1) filler metal to ensure the joint maintains high-temperature stability across the thermal gradient.
Q2: Why is Inconel 617 often chosen for nuclear applications?
A: Due to its extreme stability and resistance to corrosion in high-temperature helium or salt environments, 617 is the primary choice for next-generation nuclear reactor internals.
Q3: Does GH4169 offer better fatigue life than 617?
A: Below 650°C, yes. GH4169's precipitation-hardened matrix is designed specifically for High-Cycle Fatigue (HCF). Only switch to 617 when the heat crosses the 750°C over-aging threshold.
Q4: Do you offer trial orders for non-standard thicknesses?
A: Absolutely. We support prototype development and offer Flexible MOQs for both GH4169 and Inconel 617 tubing and sheets.




