Inconel 706 Heat Treated
VerifiedmetalInconel 706 is a nickel-iron-chromium precipitation-hardening superalloy with columbium and titanium additions, designed for high-strength applications in aerospace gas turbines and fasteners operating to approximately 1300°F (704°C). The heat-treated condition provides excellent tensile strength and bearing properties with good ductility, making it suitable for critical rotating and structural components requiring sustained elevated-temperature performance with reliable stress-rupture resistance.
aerospacestructural
Compliance & Regulations
?ITAR?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | — | ksi | 14 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | — | ksi | 14 entriesClick to expand | ||
Compressive Modulus(Ec) | Curve (15 pts) | ksi | — | — | |
Compressive Yield Strength(Fcy) | — | ksi | 7 entriesClick to expand | ||
Elongation at Break(εf) | — | - | 7 entriesClick to expand | ||
Poisson's Ratio(ν) | — | - | 22°C | — | |
Reduction of Area(RA)4 entries | — | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5701 · L · t=<2.500 in | — | |
| ↳ | — | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5701 · L · t=2.500-4.000 in | — | |
| ↳ | — | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5702 OR AMS 5703 · L · t=<2.500 in | — | |
| ↳ | — | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5702 OR AMS 5703 · L · t=2.500-4.000 in | — | |
Shear Modulus(G) | — | ksi | 22°C · Sheet/Strip/Plate | — | |
Ultimate Shear Strength(Fsu) | — | ksi | 7 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | — | ksi | 7 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | ksi | 7 entriesClick to expand | ||
Young's Modulus(E) | — | ksi | 22°C · Sheet/Strip/Plate | — | |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (25 pts) | µin/in·°F | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (24 pts) | BTU/(lb·°F) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (25 pts) | BTU/(hr·ft·°F) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
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RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.