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Choose up to three materials. Compare their properties, reference conditions and specification requirements side by side.
47 matching materials
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| Material | Nimonic 80AN07080 | Inconel 718N07718 |
|---|---|---|
Summary | ||
| Material family | Nickel Alloys | Nickel Alloys |
| Grade / UNS | N07080 | N07718 |
| Summary | An age-hardenable nickel-chromium alloy used in turbine components and high-temperature bolting. | An age-hardenable nickel alloy for fasteners and components requiring strength and corrosion resistance. |
Performance overview | ||
| Material focus | Precipitation strengthening | Strength developed through aging |
| Physical reference | Not documented in this reference |
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| Chemical composition | Chemical compositionSelected composition limits · wt.%
| Chemical compositionComposition limits · wt.%
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Mechanical propertiesReference conditions vary or are incomplete. Read the basis, condition and source for each column; these values do not establish a performance ranking or finished-fastener acceptance values. | ||
| Tensile strength | ≥930 MPa Catalogue reference minimums Supplied technical reference · Scanned PDF page 5 · printed page 17Not documented in this reference Not documented in this reference | 1389 MPa Typical reference sample Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗Annealed + aged Room temperature |
| 0.2% yield strength | ≥620 MPa Catalogue reference minimums Supplied technical reference · Scanned PDF page 5 · printed page 17Not documented in this reference Not documented in this reference | 1207 MPa Typical reference sample Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗Annealed + aged Room temperature |
| Elongation | ≥20 % Catalogue reference minimums Supplied technical reference · Scanned PDF page 5 · printed page 17Not documented in this reference Not documented in this reference | 20 % Typical reference sample Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗Annealed + aged Room temperature |
| Reference conditions |
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Temperature & corrosionEvaluate the medium, concentration, impurities, temperature and loading together. A melting point or oxidation reference is not a safe working-temperature limit. | ||
| Service conditions to review | Confirm the aging condition and required strength. | Specify the heat treatment and strength requirement. |
| Temperature-dependent data | Not documented in this reference |
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Heat treatmentDelivery condition and heat-treatment requirements are agreed for the requested product form and order. | ||
| Condition | Not documented in this reference | Annealed + aged |
| Reference treatment | Not documented in this reference | 1750°F / 1 h, then 1325°F / 8 h; furnace cool to 1150°F for 18 h total aging.Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗ |
Reference applicationsApplication examples provide context for review; suitability depends on the actual service conditions. | ||
| Reference applications | Gas-turbine assemblies · high-temperature bolting | Gas-turbine assemblies · cryogenic equipment |
Standards & documentationConfirm the edition, product form and condition. Material specifications do not establish finished-fastener compliance. | ||
| Material specifications by form |
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| Sources | Sources
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Documents for your enquiry
Every BYBOLT delivery includes an MTC / EN 10204 3.1 certificate, heat-number traceability and mechanical testing. Threaded products include sampled GO / NO-GO gauging. Test methods and acceptance criteria follow the agreed specification; PMI, third-party inspection and additional records are agreed separately at quotation.
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