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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
Alloy X-750 Nickel Base Alloy Inconel X-750 / UNS N07750 / EN 2.4669 Sheet and Plate
Products Specification
Product Name | Nickel Alloy Plate & Sheet |
Thinckness | Cold rolled:0.3mm-3mm Hot rolled: 3.0mm-30mm |
Standard Size | Cold Rolled 1000*2000mm 1219*2438mm 1500*3000mm |
Hot Rolled 1500*6000mm 1800*6000mm 2000*6000mm | |
Service | Cutting (laser cutting, plasma cutting, cutting machine), Bending, forged produce |
Surface Service | Raw finishing (2B NO.1) Finishing(HL 8K Checkered.etc) |
Standard | ASTM, AISI, DIN, EN, GB, JIS |
Mainly Grade | ASTM 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 |
Brand | TISCO 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:
The chemical composition of Inconel X750 is indicated in the table below:
Element | Min % | Max % |
---|---|---|
C | – | 0.08 |
Mn | – | 1.00 |
Si | – | 0.50 |
S | – | 0.01 |
Cr | 14.00 | 17.00 |
Ni | 70.00 | – |
Nb/Cb | 0.70 | 1.20 |
Ti | 2.25 | 2.75 |
Al | 0.40 | 1.00 |
Fe | 5.00 | 9.00 |
Co | – | 1.00 |
Ta | – | 0.05 |
Cu | – | 0.50 |
Inconel X750 density, melting point, coefficient of expansion, modulus of rigidity, and elasticity is indicated in the table below:
Density | Melting Point | Coefficient of Expansion | Modulus of Rigidity | Modulus of Elasticity |
---|---|---|---|---|
8.28g/cm³ | 1430 °C | 12.6 μm/m °C (20 – 100 °C) | 75.8 kN/mm² | 218.0 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/in³ | 2600 °F | 7.0 x 10-6 in/in °F (70 – 212 °F) | 10994 ksi | 31619 ksi (Spring Temper + Aged) 30806 ksi (Spring Temper + 3 Part Heat Treated) 30995 ksi (No.1 Spring Temper + Aged) |
Inconel X750 is known to be suitable for the following applications:
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X-750 Nickel Alloy UNS N07750 EN 2.4669 Images |