Inconel X750 UNS N07750 Heat-Resisting Superalloy Bars and plates

This is a precipitation-hardened nickel-based superalloy strengthened by γ’ precipitates with titanium, aluminum and niobium on a nickel-chromium matrix. It delivers outstanding high-temperature rupture strength, creep resistance and high-temperature oxidation resistance, featuring excellent resistance to alternating high-low temperature load and stress relaxation. Meanwhile, it owns favorable hot & cold workability, forgeability and welding stability. The alloy can operate stably for long-term service below 700℃, with prominent resistance to high-temperature fatigue and flue gas corrosion.

Applications of Inconel X750

This material serves as the core raw material for aero-engine turbine disks, blade fasteners, combustion chamber bolts and load-bearing rings. It is widely applied to high-temperature elastic components of gas turbines, nuclear power high-temperature springs and high-temperature locking parts of steam turbines. Besides, it fits heat-resistant structural parts for aerospace vehicles, high-temperature and high-pressure equipment fasteners in petrochemical industry, and military high-temperature resistant sealing elastic components. It is a benchmark special alloy for high-end high-temperature load-bearing and anti-relaxation fastening parts.

Equivalent Grades and Commonly Used Specifications of Inconel X750

Steel Grade Specification Specification Name
GH4145/H07750/NS4102 GB/T 14996   Wrought superalloy—Cold-rolled sheets and strips
GB/T 14992  Superalloys and intermetallic compounds—Designation and chemical composition
GB/T 15007  Designations of corrosion-resisting alloy
UNS N07750 / Inconel X-750 ASTM B637 Standard Specification for Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service
AMS 5542 Nickel Alloy, Corrosion and Heat Resistant, Plate, Sheet, Strip, Solution Treated
AMS 5698 Nickel Alloy, Corrosion and Heat Resistant, Wire, Solution Treated
Products produced as per other specifications or technical agreements (if need) are available.

Typical Chemical Composition of Inconel X750

Elements

C Si Mn P S Cr Ni Co Cu Fe V Al Ti

Nb

Mass Fraction%

≤0.080 ≤0.50 ≤1.00 ≤0.015 ≤0.010 14.00~17.00 ≥70.00 ≤1.00 ≤0.50 5.00~9.00 ≤0.35 0.40~1.00 2.25~2.75

0.70~1.20

Products produced as per other specifications or technical agreements (if need) are available.

Typical Heat Treatment Condition and Mechanical Properties of Inconel X750

Delivery Condition

Mechanical Properties and Hardness of Heat-Treated Specimens
Rp0.2/(N/mm2) Rm/(N/mm2) A/% Zb/% Aku2d/J HBW

HRC

solution at 1149 °C + stabilize + precipitation harden

≥620 ≥965 ≥8 / / ≥262 ≥26
solution at 982 °C+ precipitation harden(≤63.5mm) ≥790 ≥1170 ≥18 ≥18 / 302~363

32~40

solution at 982 °C+ precipitation harden(63.5mm≤101.6mm)

≥790 ≥1170 ≥15 ≥15 / 302~363 32~40
solution anneal at 1093 °C + precipitation harden ≥689 ≥1103 ≥20 ≥20 / 267~363

27~40

Products produced as per other specifications or technical agreements (if need) are available.

Product Forms and Size Range of Inconel X750

Product forms

Size range

Bars

Diameter or side length: 5.0mm~1000mm
Flats

thickness: 4.0mm~1000mm

width: 300mm~2200mm

Produce as other form and size according to technical requirements are available.
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