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X-750 Nickel Alloy UNS N07750 EN 2.4669

Categories Nickel Alloy
Brand Name: DELTA
Model Number: inconel X-750
Certification: ISO
Place of Origin: China
MOQ: 500 kgs
Price: 15-20 USD/Kg
Payment Terms: L/C, T/T, Western Union
Supply Ability: 3 Ton per week
Delivery Time: 5 - 12 days based on the quantity
Packaging Details: standard packing for export
Products: Nickel alloy plate
Grade: inconel X-750
Thickness: 0.6 - 30.0mm
Width: 1000mm 1219mm 1500mm
Standard: ASTM EN
Service: Cutting
Loading Port: Shanghai Port
Surface: 2B NO.1
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X-750 Nickel Alloy UNS N07750 EN 2.4669

Alloy X-750 Nickel Base Alloy Inconel X-750 / UNS N07750 / EN 2.4669 Sheet and Plate


Products Specification


Product NameNickel Alloy Plate & Sheet
Thinckness

Cold rolled:0.3mm-3mm

Hot rolled: 3.0mm-30mm

Standard SizeCold Rolled 1000*2000mm 1219*2438mm 1500*3000mm
Hot Rolled 1500*6000mm 1800*6000mm 2000*6000mm
ServiceCutting (laser cutting, plasma cutting, cutting machine), Bending, forged produce
Surface ServiceRaw finishing (2B NO.1) Finishing(HL 8K Checkered.etc)
StandardASTM, AISI, DIN, EN, GB, JIS
Mainly GradeASTM Grade: Incoloy 800 / 800H ,Incoloy 825,Inconel 600 , Inconel 625 ,Inconel 718, Inconel X-750,Inconel690,Hastelloy B , Hastelloy B-2 , Hastelloy C276 , Hastelloy C4, Hastelloy C2000,
ASME Grade: N08800 N08810 N08825 N06600 N06601 N06690 N10001 N10665 N10276 N06455 N06625
EN 1.4588 2.4858 2.4817 2.4642 2.4617 2.4819 2.461 2.4856
BrandTISCO BAOSTEEL ZPSS LISCO JISCO

INCONEL alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic termperatures. Composition is shown in Table 1. The economics of INCONEL alloy X-750 coupled with its availability in all standard mill forms has resulted in applications in a wide variety of industrial fields. In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL alloy X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL alloy X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL alloy X-750 is used from sub-zero to 1200°F


Inconel X750 offers the following key features:

  • Good creep rupture strength at high temperatures
  • Not as strong as Nimonic 90
  • Very good at cryogenic temperatures
  • Age hardenable
  • High temperature dynamic applications

Chemical Composition of Inconel X-750 Alloy

The chemical composition of Inconel X750 is indicated in the table below:

ElementMin %Max %
C0.08
Mn1.00
Si0.50
S0.01
Cr14.0017.00
Ni70.00
Nb/Cb0.701.20
Ti2.252.75
Al0.401.00
Fe5.009.00
Co1.00
Ta0.05
Cu0.50

Alloy Details

Inconel X750 density, melting point, coefficient of expansion, modulus of rigidity, and elasticity is indicated in the table below:

DensityMelting PointCoefficient of ExpansionModulus of RigidityModulus of Elasticity
8.28g/cm³1430 °C12.6 μm/m °C (20 – 100 °C)75.8 kN/mm²218.0 kN/mm² (Spring Temper + Aged)
212.4 kN/mm² (Spring Temper + 3 Part Heat Treated)
213.7 kN/mm² (No.1 Spring Temper + Aged)
0.299 lb/in³2600 °F7.0 x 10-6 in/in °F (70 – 212 °F)10994 ksi31619 ksi (Spring Temper + Aged)
30806 ksi (Spring Temper + 3 Part Heat Treated)
30995 ksi (No.1 Spring Temper + Aged)

Typical Applications

Inconel X750 is known to be suitable for the following applications:

  • Nuclear reactors
  • Gas turbines
  • Rocket engines
  • Pressure vessels
  • Aircraft structures

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