| Brand Name: | DLX |
| Model Number: | Nimonic 75 |
| MOQ: | 10kg |
| Payment Terms: | L/C,D/A,D/P,T/T,VTB |
| Supply Ability: | 1200 tons per month |
DLX supplies high-integrity Nimonic 75 nickel-chromium superalloy round bars in diameter range 20-150mm. Specifically formulated for extreme thermal loads, gas turbine combustor components, and high-stress industrial furnace environments.
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Nimonic 75 is an 80/20 nickel-chromium alloy with controlled additions of titanium and carbon, tailored for high-temperature service where exceptional fabricability and thermal endurance are required. The dense, self-healing chromium oxide (Cr2O3) scale developed on the alloy surface shields structural components from aggressive combustion gases, cyclic thermal shock, and carburizing atmospheres.
Our precision-forged and hot-rolled round bars (Dia 20–150mm) undergo full-length ultrasonic testing and surface finishing (peeled, ground, or bright-turned) to ensure zero internal voids, inclusions, or micro-cracks. With high ductility in cold and hot forming alongside reliable weldability, Nimonic 75 round bars reduce downtime and extend maintenance intervals in high-thrust turbines and heavy industrial heating systems.
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| Element | Content Range (wt%) | Function & Metallurgical Role |
|---|---|---|
| Nickel (Ni) | Balance (≥ 72.0%) | Austenitic matrix stability & corrosion resistance |
| Chromium (Cr) | 18.00 – 21.00% | High-temperature oxidation & scaling resistance |
| Titanium (Ti) | 0.20 – 0.60% | Controlled carbide precipitation & grain stability |
| Carbon (C) | 0.08 – 0.15% | Creep-rupture strength enhancement |
| Iron (Fe) | ≤ 5.00% | Residual restriction for thermal stability |
| Silicon (Si) | ≤ 1.00% | Deoxidation & fluidity control |
| Manganese (Mn) | ≤ 1.00% | Hot workability promoter |
| Copper (Cu) | ≤ 0.50% | Trace impurity minimization |
| Sulfur (S) | ≤ 0.015% | Ultra-low boundary embrittlement control |
| Property Parameter | Typical Value / Range | Engineering Note |
|---|---|---|
| Density | 8.37 g/cm³ | High mass density for structural rigidity |
| Melting Range | 1340°C – 1390°C | High incipient melting point |
| Tensile Strength (Rm) | ≥ 750 MPa | Room temperature mechanical strength |
| Yield Strength (Rp0.2) | ≥ 300 MPa | Elastic limit threshold |
| Elongation (A5) | ≥ 30% | High ductility for cold/hot deformation |
| Hardness | ≤ 220 HB / ~95 HRB | Optimized for downstream machining |
| Max Service Temperature | 1000°C (Continuous) | Long-term high-temperature oxidation resistance |
| Thermal Expansion Coefficient | 13.0 × 10⁻⁶ /K (20–100°C) | Dimensional stability under thermal cycling |
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Q1: What makes Nimonic 75 particularly suited for gas turbine combustion chambers?
A1: Gas turbine combustors operate in extreme conditions involving high thermal gradients, cyclic fatigue, and oxidizing combustion gases. Nimonic 75 combines high creep strength, reliable ductility, and an exceptionally protective chromium-oxide layer, preventing premature structural deformation and scale spalling up to 1000°C.
Q2: What diameter range and surface finishes are available for DLX Nimonic 75 round bars?
A2: We supply Nimonic 75 round bars from Dia 20mm up to 150mm. Available surface finishes include peeled, precision-turned, centerless ground, and polished surfaces with tight dimensional tolerances (up to h9/h10).
Q3: How does DLX ensure internal soundness and defect-free quality in superalloy bars?
A3: All bars are produced through Vacuum Induction Melting (VIM) followed by Electroslag Remelting (ESR). We conduct 100% volumetric ultrasonic inspection, metallurgical grain size analysis, and full chemical spectroscopy on every production heat to ensure zero internal voids or inclusions.
Q4: Can Nimonic 75 round bars be welded easily for complex combustor assemblies?
A4: Yes. Due to its solid-solution strengthened single-phase matrix, Nimonic 75 possesses excellent weldability compared to gamma-prime precipitation-hardened superalloys. It can be joined using conventional GTAW (TIG) and GMAW (MIG) methods without susceptibility to strain-age cracking.
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