Ananka Fasteners is a premier manufacturer and global exporter of Nimonic 80A Fasteners (UNS N07080 / W.Nr. 2.4952 / 2.4631), a highly advanced, wrought, age-hardenable nickel-chromium superalloy. Occupying a critical position in high-temperature materials engineering, Nimonic 80A is specified for mission-critical mechanical assemblies where standard stainless steels and lower-tier nickel alloys rapidly degrade via creep-rupture, severe oxidation, or high-cycle thermal fatigue.
The defining engineering breakthrough of UNS N07080 is its precipitation-hardenable matrix. By incorporating controlled additions of titanium and aluminum, the alloy precipitates a finely dispersed gamma prime (γ') phase—Ni3(Ti, Al)—during artificial aging. This intermetallic network effectively pins atomic dislocations, halting plastic deformation and granting the alloy exemplary creep-rupture strength at continuous service temperatures up to 815°C (1500°F).
Every Nimonic 80A fastener manufactured by Ananka is produced utilizing precision CNC machining, cryogenic hybrid cooling techniques to mitigate tool wear, and rigorous multi-stage heat treatments. Backed by EN 10204 Type 3.1 Material Test Certificates and adherence to ASTM B637 and DIN EN 10090 standards, we supply these elite fastening systems to the aerospace, nuclear power generation, advanced motorsport, and petrochemical refining sectors worldwide.
| Material Type | Precipitation-Hardenable Nickel-Chromium Superalloy |
|---|---|
| UNS Number | N07080 |
| Werkstoff Number | 2.4952 / 2.4631 |
| Density | 8.19 - 8.25 g/cm³ (0.295 - 0.296 lb/in³) |
| Melting Range | 1320 – 1370 °C (2410 – 2500 °F) |
| Modulus of Elasticity | 183 - 222 GPa (26.5 - 32.2 × 10³ ksi) at 20°C |
| Thermal Conductivity | 11.2 W/m·K at 20°C (Requires advanced cooling during machining) |
| Magnetic Permeability | ≈ 1.001 (Essentially Non-magnetic) |
| Size Range | Metric: M1.2 to M140 | Imperial: #2 to 4" Custom machined lengths available. |
| Thread Types | UNC, UNF, Metric Coarse, Metric Fine, BSW, Acme |
The chemical composition is meticulously controlled within highly restrictive bands to achieve the necessary balance of high-temperature strength, cyclic oxidation resistance, and hot fabricability. The specific stoichiometric ratio of titanium to aluminum is calibrated to maximize the volume fraction of the γ' precipitate upon aging.
| Ni | Cr | Ti | Al | Fe | Co | Mn / Si | C | Zr / B | S / Pb |
|---|---|---|---|---|---|---|---|---|---|
| Balance (≥65.0) | 18.0 – 21.0 | 1.8 – 2.7 | 1.0 – 1.8 | 3.0 Max | 2.0 Max | 1.0 Max | 0.10 Max | 0.15 / 0.008 Max | 0.015 / 0.0025 Max |
Nimonic 80A delivers formidable mechanical strength that is custom-tailored through varying degrees of cold working and subsequent thermal precipitation treatments. In the fully aged state, it provides an optimal balance of sheer strength and toughness.
| Material Condition | Ultimate Tensile Strength | Yield Strength (0.2% Offset) | Elongation | Max Operating Temp |
|---|---|---|---|---|
| Annealed (Base) | < 1000 MPa (< 145 ksi) | - | High | - |
| Annealed + Aged (Standard) | 1200 – 1400 MPa (174 – 203 ksi) | ≥ 780 MPa (113 ksi) | 30% | 550°C (1020°F) |
| Spring Temper | 1300 – 1500 MPa (189 – 218 ksi) | - | Low | - |
| Spring Temper + Aged | 1500 – 1800 MPa (218 – 261 ksi) | - | - | 350°C (660°F) |
The paramount hallmark of Nimonic 80A is its stress-rupture strength. At continuous service temperatures up to 815°C (1500°F), the densely packed γ' precipitates physically prevent time-dependent failure. When tested rigorously at 600°C (1112°F), the alloy successfully maintains significant operational residual stress thresholds over tests extending up to 10,000 continuous hours, establishing its reliability for baseload power generation turbines.
| Standard / Region | Designation |
|---|---|
| UNS (Universal) | N07080 |
| Werkstoff / DIN / EN | 2.4952 / 2.4631 (DIN 17742, EN 10090) |
| British Standards (BS) | HR 1, HR 201, HR 401, HR 601, BS 3076 |
| AECMA (Aerospace) | PrEn 2188, 2189, 2190, 2191, 2396, 2397 |
| Common Trade Names | Nimonic® 80A, Nicrofer 7520 Ti, Pyromet 80A, Udimet 80A |
Nimonic 80A demonstrates extraordinary, class-leading resistance to high-temperature oxidation, scaling, and hot corrosion driven by molten salts and fuel impurities.
| Bolts & Screws | Nuts & Washers | Studs & Specialty |
|---|---|---|
| Heavy Hex Bolts / Hex Cap Screws | Heavy Hex Nuts / Standard Hex Nuts | Fully Threaded Studs |
| 12-Point Aerospace Flange Bolts | Prevailing Torque Lock Nuts | Double-Ended / Tap-End Studs |
| Socket Head Cap Screws | Belleville / Wave Spring Washers | Threaded Rods |
| Countersunk / Flat Head Bolts | Flat & Split-Lock Washers | Custom Machined Anchor Bolts |
| Finished Fasteners — Bolts & Studs | ASTM B637 / ASME SB637 |
|---|---|
| Metric Dimensional Standards | DIN 931 / 933 / 912 / 934 / 125 | ISO 4014 / 4017 |
| Imperial Dimensional Standards | ASME B18.2.1 (Bolts/Studs), ASME B18.2.2 (Nuts) |
| Aerospace Specifications | AIR 9165-37, MSRR 7095, MSRR 7011 |
The inherent metallurgical traits that grant Nimonic 80A its supreme high-temperature stability simultaneously render it exceptionally challenging to machine and fabricate.
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Every lot of Nimonic 80A fasteners shipped by Ananka is accompanied by a highly detailed EN 10204 Type 3.1 Manufacturer Test Certificate (MTC), ensuring absolute metallurgical pedigree traceable back to the originating mill.
Each MTC documents:
Unlike solid-solution alloys that rely on cold working, Nimonic 80A contains Titanium and Aluminum. These elements allow the alloy to be precipitation-hardened (age-hardened) by forming a microscopic gamma prime (γ') phase. This network pins atomic dislocations, providing massive creep-rupture strength at high temperatures.
Yes. The alloy features a strict, low Cobalt trace restriction (≤ 2.0%). This prevents the formation of highly radioactive Cobalt-60 isotopes under continuous neutron bombardment, making it ideal for reactor core restraints and primary coolant loop fasteners.
Nimonic 80A fasteners are designed to maintain exceptional structural stability, creep resistance, and tensile strength under extreme thermo-mechanical loads at continuous service temperatures up to 815°C (1500°F).
They typically undergo a two-step process: Solution Annealing at ≈1080°C followed by rapid cooling to homogenize the structure, and then Precipitation Aging at ≈700°C to 750°C for 16-24 hours to grow the strengthening intermetallic network.
The alloy combines high shear strength with very low thermal conductivity. During tightening, frictional heat cannot dissipate, causing bare metal threads to cold-weld and seize. Specialized coatings (PTFE, silver plating) or high-performance anti-seize lubricants are strictly required.