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47 matching materials

Nickel AlloysUNS N07750View material details
Nickel AlloysUNS N07718View material details

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Compare Materials: Inconel X-750, Inconel 718
MaterialInconel X-750N07750Inconel 718N07718

Summary

Material familyNickel AlloysNickel Alloys
Grade / UNSN07750N07718
SummaryAn age-hardenable nickel-chromium alloy used for springs, fasteners and hot-section components.An age-hardenable nickel alloy for fasteners and components requiring strength and corrosion resistance.

Performance overview

Material focusStrength developed through agingStrength developed through aging
Physical referenceNot documented in this reference
Density
8.19 g/cm³
Melting range
1260–1336 °C
Supplied technical reference · Scanned PDF page 12 · printed page 24
Chemical composition
Chemical composition

Selected composition limits · wt.%

Ni + Co
≥70
Cr
14–17
Fe
5–9
Ti
2.25–2.75
Al
0.40–1.00
Nb + Ta
0.70–1.20
Special Metals · X-750 · Table 9 · Ø1/2 in hot-finished bar, treatment B ↗
Chemical composition

Composition limits · wt.%

Ni
50–55
Cr
17–21
Nb + Ta
4.75–5.50
Mo
2.80–3.30
Ti
0.65–1.15
Al
0.20–0.80
Fe
Balance
C
≤0.08
Mn
≤0.35
Si
≤0.35
P
≤0.015
S
≤0.015
B
≤0.006
Cu
≤0.30
Co
≤1.0
Supplied technical reference · Scanned PDF page 4 · printed page 16

Mechanical properties

Reference 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 strength1351 MPa
Typical reference sample
Solution treated + aged (treatment B)
Room temperature
Special Metals · X-750 · Table 9 · Ø1/2 in hot-finished bar, treatment B ↗
1389 MPa
Typical reference sample
Annealed + aged
Room temperature
Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗
0.2% yield strength1027 MPa
Typical reference sample
Solution treated + aged (treatment B)
Room temperature
Special Metals · X-750 · Table 9 · Ø1/2 in hot-finished bar, treatment B ↗
1207 MPa
Typical reference sample
Annealed + aged
Room temperature
Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗
Elongation24 %
Typical reference sample
Solution treated + aged (treatment B)
Room temperature
Special Metals · X-750 · Table 9 · Ø1/2 in hot-finished bar, treatment B ↗
20 %
Typical reference sample
Annealed + aged
Room temperature
Special Metals · Alloy 718 · SMC-045, September 2007 · Tables 1 & 8 ↗
Reference conditions
Data basis
Typical reference sample
Condition
Solution treated + aged (treatment B)
Sample form
Hot-finished bar
Sample size
Ø12.7 mm (1/2 in)
Test temperature
Room temperature
Test method
Not documented in this reference
Test direction
Not documented in this reference
Elongation gauge length
Not documented in this reference
Data basis
Typical reference sample
Condition
Annealed + aged
Sample form
Hot-rolled bar · Ø25.4 mm
Sample size
1.0 in diameter (25.4 mm)
Test temperature
Room temperature
Test method
Not documented in this reference
Test direction
Longitudinal
Elongation gauge length
Not documented in this reference

Temperature & corrosion

Evaluate the medium, concentration, impurities, temperature and loading together. A melting point or oxidation reference is not a safe working-temperature limit.

Service conditions to reviewSpecify the heat treatment; X-750 has several distinct property conditions.Specify the heat treatment and strength requirement.
Temperature-dependent dataNot documented in this reference
  • Strength and elongation vs temperaturePlate · mill annealed + aged
View material details

Heat treatment

Delivery condition and heat-treatment requirements are agreed for the requested product form and order.

ConditionSolution treated + aged (treatment B)Annealed + aged
Reference treatment1800°F / 1 h, air cool; 1350°F / 8 h, furnace cool to 1150°F; total aging 18 h.Special Metals · X-750 · Table 9 · Ø1/2 in hot-finished bar, treatment B ↗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 applications

Application examples provide context for review; suitability depends on the actual service conditions.

Reference applicationsGas-turbine assemblies · heat-treatment fixturesGas-turbine assemblies · cryogenic equipment

Standards & documentation

Confirm the edition, product form and condition. Material specifications do not establish finished-fastener compliance.

Material specifications by form
Sources
Sources
Sources

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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