| Brand Name: | DLX |
| Model Number: | Superalloy Sheet Nimonic 75 |
| MOQ: | 5kg |
| Payment Terms: | L/C,D/A,D/P,T/T,VTB |
| Supply Ability: | 1200 tons per month |
Engineered for demanding thermal environments, our precision cold rolled Nimonic 75 superalloy sheet (thickness 0.5–3.0mm) delivers exceptional oxidation resistance up to 1000°C, high mechanical durability, and superior cold formability for aerospace combustion flame tubes, gas turbine casings, and industrial furnace ducting.
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Nimonic 75 (Ni-Cr-Ti solid solution alloy) is engineered to maintain high structural integrity and creep-rupture resistance under continuous thermal cycles. Produced via advanced Vacuum Induction Melting (VIM) coupled with Electroslag Remelting (ESR), our superalloy sheet exhibits exceptional metallurgical cleanliness, uniform grain structure, and minimal non-metallic inclusions.
The addition of titanium, combined with a high chromium matrix (~20% Cr), forms a dense, self-healing chromium oxide passive layer that resists oxidation, carburization, and thermal degradation at sustained temperatures reaching 1000°C (1832°F). Through multi-pass precision cold rolling and protective-atmosphere bright annealing, our Nimonic 75 sheets offer superior surface finish, tight flatness tolerances, and optimal ductility for complex deep drawing, rolling, and automated welding operations in aerospace manufacturing.
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| Element | Content (%) | Element | Content (%) |
|---|---|---|---|
| Nickel (Ni) | Balance (~70.0–75.0) | Titanium (Ti) | 0.20 – 0.60 |
| Chromium (Cr) | 18.0 – 21.0 | Carbon (C) | 0.08 – 0.15 |
| Iron (Fe) | ≤ 5.00 | Manganese (Mn) | ≤ 1.00 |
| Silicon (Si) | ≤ 1.00 | Copper (Cu) | ≤ 0.50 |
| Aluminum (Al) | ≤ 0.50 | Sulfur (S) | ≤ 0.015 |
| Property Parameter | Metric Value | Imperial Value |
|---|---|---|
| Density | 8.37 g/cm³ | 0.302 lb/in³ |
| Melting Range | 1340 – 1390 °C | 2444 – 2534 °F |
| Thermal Conductivity (20°C) | 12.5 W/(m·K) | 86.8 BTU·in/(hr·ft²·°F) |
| Specific Heat Capacity (20°C) | 460 J/(kg·K) | 0.110 BTU/(lb·°F) |
| Electrical Resistivity (20°C) | 1.15 µΩ·m | 45.3 µΩ·in |
| Thermal Expansion Coefficient (20–1000°C) | 16.5×10−6 K−1 | 9.17×10−6 in/in/°F |
| Mechanical Property | Guaranteed Value | Typical Measured Range |
|---|---|---|
| Tensile Strength (Rm) | ≥ 700 MPa | 740 – 820 MPa |
| Yield Strength (Rp0.2) | ≥ 300 MPa | 320 – 380 MPa |
| Elongation at Break (A50mm) | ≥ 30 % | 35 – 45 % |
| Hardness | ≤ 210 HV / 95 HRB | 170 – 195 HV |
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Superior High-Temperature Oxidation Resistance:
Forms an adherent, protective chromium-rich oxide film that prevents scaling, hot-gas erosion, and internal oxidation in continuous thermal exposure up to 1000°C.
Exceptional Cold Workability & Ductility:
With elongation exceeding 35%, our cold rolled sheets allow severe deep drawing, spinning, roll-forming, and edge bending without intermediate annealing or micro-cracking.
High Thermal-Mechanical Fatigue Strength:
Engineered to withstand cyclic thermal shocks and rapid temperature variations without structural distortion, crucial for aerospace propulsion combustion zones.
Outstanding Weldability & Fabrication Versatility:
Readily joinable using standard TIG (GTAW), MIG (GMAW), resistance spot welding, and laser welding methods with zero post-weld heat treatment cracking tendencies.
Strict Dimensional Uniformity & Surface Integrity:
Multi-stand precision rolling ensures consistent gauge across the entire sheet width, clean edges free from burrs, and defect-free surfaces meeting cleanroom aerospace inspection standards.
Aerospace Flame Tubes & Combustion Chamber Liners:
Serving as the primary thermal shielding material in aircraft turbojets, turboprops, and gas turbine flame cans exposed to direct combustion flames and thermal gas streams.
Gas Turbine Exhaust Ducts & Transition Pieces:
Used in turbine exhaust fairings, thermal baffles, annular ducting, and afterburner components subjected to cyclic thermal stresses.
Industrial Furnace Fixtures & Heat Shielding:
High-temperature muffle tubes, annealing furnace retorts, radiant tube baffles, and heat-treatment basket liners.
Nuclear & Petrochemical Thermal Systems:
Specialized heat exchangers, high-temperature gas piping, and catalyst support grids operating under continuous corrosive heat.
Laser & High-Temperature Sensor Enclosures:
Thermal sensor protective shielding, thermocouple protection sleeves, and high-temperature diagnostic housing components.
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Q1: What makes Nimonic 75 ideal for aerospace flame tubes compared to standard stainless steels?
A: Unlike heat-resistant stainless steels that suffer from rapid oxidation and sigma-phase embrittlement above 750°C, Nimonic 75 maintains high tensile stability, thermal fatigue resistance, and a self-regenerating chromia layer that operates reliably under continuous combustion gas flow up to 1000°C.
Q2: Can Nimonic 75 sheet be cold-formed into complex aerospace contours?
A: Yes. In the bright annealed condition, Nimonic 75 possesses an elongation rate of 35%–45% and moderate initial hardness, making it exceptionally ductile for deep drawing, roll forming, and pressing into intricate flame tube segments and annular combustion rings.
Q3: What thickness tolerances can DLX provide for 0.5mm–3.0mm sheets?
A: We provide high-precision thickness tolerances controlled within ±0.015 mm for thinner gauges (0.5–1.0mm) and within ±0.03 mm for heavier gauges (1.2–3.0mm), ensuring consistent weight and uniform thermal performance across stamped parts.
Q4: What welding procedures are recommended for Nimonic 75 sheet fabrications?
A: Nimonic 75 exhibits excellent weldability using TIG (GTAW) or resistance welding. Matching filler metals (such as Nimonic filler wire) are typically utilized to guarantee identical high-temperature corrosion and mechanical properties across the weld joint.
Q5: What are your minimum order requirements (MOQ) and lead times for custom orders?
A: As a dedicated B2B manufacturer, our minimum order quantity (MOQ) is dynamically aligned with your required thickness, width, and processing state. Standard production lead times range from 2 to 4 weeks depending on the degree of customization and batch specifications.
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