Product Code : AL-InX750-NN-PO
Inconel alloys are oxidation-corrosion-resistant materials well suited for service in extreme environments subjected to pressure and heat. When heated, Inconel forms a thick, stable, passivating oxide layer protecting the surface from further attack. Inconel retains strength over a wide temperature range, attractive for high-temperature applications where aluminium and steel would succumb to creep as a result of thermally-induced crystal vacancies. Inconel's high-temperature strength is developed by solid solution strengthening or precipitation hardening, depending on the alloy. X750 is a Nickel-Chromium alloy made precipitation hardenable by additions of Al and Ti, having creep-rupture strength at high temperatures to about 700℃ (1290℉). It is widely used for high-temperature conditions but is not as strong as Nimonic 90. Primary applications include bearing assembly, ballast, casting, step soldering, and radiation shielding.
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Product Information
Inconel alloys are oxidation-corrosion-resistant materials well suited for service in extreme environments subjected to pressure and heat. When heated, Inconel forms a thick, stable, passivating oxide layer protecting the surface from further attack. Inconel retains strength over a wide temperature range, attractive for high-temperature applications where aluminium and steel would succumb to creep as a result of thermally-induced crystal vacancies. Inconel's high-temperature strength is developed by solid solution strengthening or precipitation hardening, depending on the alloy. X750 is a Nickel-Chromium alloy made precipitation hardenable by additions of Al and Ti, having creep-rupture strength at high temperatures to about 700℃ (1290℉). It is widely used for high-temperature conditions but is not as strong as Nimonic 90. Primary applications include bearing assembly, ballast, casting, step soldering, and radiation shielding.
Synonyms
Inconel X-750 Powder Specification
Size：customized
Purity: customized
Per your request or drawing
We can customized as required
| Rod | ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269 |
| Bar | ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269 |
| Forging Stock | ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269 |
| Plate | ISO 6208, AMS 5542 and AMS 5598 |
| Sheet | ISO 6208, AMS 5542 and AMS 5598 |
| Strip | ISO 6208, AMS 5542 and AMS 5598 |
| Wire | BS HR 505, AMS 5698, AMS 5699 |
| Other | UNS N07750, W.Nr 2.4669, Inconel X750 (tradename), UNS N07752 |
Properties（Theoretical）
| Density | 8.28 g/cm³ | 0.299 lbs/in³ | |
| Modulus of elasticity | 214 GPa | 31 MPsi | |
| Electrical resistivity | 1.22 µohms/m | 734 µohms/ft | |
| Thermal conductivity | 12.0 W/m-K | 83 Btu-in/ft²hr-°F | |
| Melting Point | 1430°C | ||
| Coefficient of Expansion | 12.6 μm/m °C (20 – 100°C) | ||
| Modulus of Rigidity | 75.8 kN/mm² | ||
| Modulus of Elasticity | 218.0 kN/mm² | ||
| (Spring Temper + Aged) | 212.4 kN/mm² | ||
| (Spring Temper + 3 Part Heat Treated) | 213.7 kN/mm² | ||
| Cold worked % | Yield strength | Ultimate tensile strength | Elongation % |
| 0 | 393 MPa [57 ksi] | 855 MPa [124 ksi] | 38 |
| 20 | 655 MPa [95 ksi] | 1007 MPa [146 ksi] | 19.3 |
| 50 | 1193 MPa [173 ksi] | 1303 MPa [189 ksi] | 2.3 |
| 60 | 1289 MPa [187 ksi] | 1462 MPa [212 ksi] | 1.8 |
| 68 | 1310 MPa [190 ksi] | 1538 MPa [223 ksi] | 1.8 |
| 75 | 1310 MPa [190 ksi] | 1586 MPa [230 ksi] | 1.9 |
| Element | C | Mn | Si | S | Cr | Ni | Nb/Cb | Ti | Al | Fe | Co | Ta | Cu |
| Min % | – | – | – | – | 14 | 70 | 0.7 | 2.25 | 0.4 | 5 | – | – | – |
| Max % | 0.08 | 1 | 0.5 | 0.01 | 17 | – | 1.2 | 2.75 | 1 | 9 | 1 | 0.05 | 0.5 |
We can customized as required
Applications of Inconel X-750 Powder
Gas turbines
Jet engine parts
Nuclear power plant applications
Heat-treating fixtures
Forming tools and extrusion dies
Pressure vessels
Aircraft structures
Rocket engines
Inconel is often encountered in extreme environments. It is common in gas turbine blades, seals, and combustors, as well as turbocharger rotors and seals, electric submersible well pump motor shafts, high temperature fasteners, chemical processing and pressure vessels, heat exchanger tubing, steam generators and core components in nuclear pressurized water reactors, natural gas processing with contaminants such as H2S and CO2, firearm sound suppressor blast baffles, and Formula One, NASCAR, NHRA, and APR, LLC exhaust systems
Packing of Inconel X-750 Powder
Standard Packing:
Typical bulk packaging includes palletized plastic 5 gallon/25 kg. pails, fiber and steel drums to 1 ton super sacks in full container (FCL) or truck load (T/L) quantities. Research and sample quantities and hygroscopic, oxidizing or other air sensitive materials may be packaged under argon or vacuum. Solutions are packaged in polypropylene, plastic or glass jars up to palletized 440 gallon liquid totes Special package is available on request.
ATTs’ Inconel X-750 Powder is carefully handled to minimize damage during storage and transportation and to preserve the quality of our products in their original condition.
Inconel Alloys Include
· Inconel 188: Readily fabricated for commercial gas turbine and aerospace applications.
· Inconel 230: Alloy 230 Plate & Sheet mainly used by the power, aerospace, chemical processing and industrial heating industries.
· Inconel 600: Solid solution strengthened
· Inconel 601:
· Inconel 617: Solid solution strengthened (nickel-chromium-cobalt-molybdenum), high-temperature strength, corrosion and oxidation resistant, high workability and weldability.[66] Incorporated in ASME Boiler and Pressure Vessel Code for high temperature nuclear applications such as molten salt reactors
· Inconel 625: Acid resistant, good weldability. The LCF version is typically used in bellows.
· Inconel 690: Low cobalt content for nuclear applications, and low resistivity
· Inconel 713C: Precipitation hardenable nickel-chromium base cast alloy
· Inconel 718: Gamma double prime strengthened with good weldability
· Inconel X-750: Commonly used for gas turbine components, including blades, seals and rotors.
· Inconel 751: Increased aluminium content for improved rupture strength in the 1600 °F range
· Inconel 792: Increased aluminium content for improved high temperature corrosion resistant properties, used especially in gas turbines
· Inconel 907
· Inconel 909
· Inconel 706
· Inconel 939: Gamma prime strengthened to increase weldability.
· Inconel 925: Inconel 925 is a nonstabilized austenitic stainless steel with low carbon content.
In age hardening or precipitation strengthening varieties, alloying additions of aluminum and titanium combine with nickel to form the intermetallic compound Ni3(Ti,Al) or gamma prime (γ′). Gamma prime forms small cubic crystals that inhibit slip and creep effectively at elevated temperatures.
| Inconel | Element, proportion by mass (%) | ||||||||||||||
| Ni | Cr | Fe | Mo | Nb & Ta | Co | Mn | Cu | Al | Ti | Si | C | S | P | B | |
| 600 | ≥72.0 | 14.0–17.0 | 6.0–10.0 | — | ≤1.0 | ≤0.5 | ≤0.5 | ≤0.15 | ≤0.015 | ||||||
| 617 | 44.2–61.0 | 20.0–24.0 | ≤3.0 | 8.0–10.0 | 10.0–15.0 | ≤0.5 | ≤0.5 | 0.8–1.5 | ≤0.6 | ≤0.5 | 0.05–0.15 | ≤0.015 | ≤0.015 | ≤0.006 | |
| 625 | ≥58.0 | 20.0–23.0 | ≤5.0 | 8.0–10.0 | 3.15–4.15 | ≤1.0 | ≤0.5 | ≤0.4 | ≤0.4 | ≤0.5 | ≤0.1 | ≤0.015 | ≤0.015 | ||
| 690 | ≥58 | 27–31 | 7–11 | ≤0.50 | ≤0.50 | ≤0.50 | ≤0.05 | ≤0.015 | |||||||
| Nuclear grade 690 | ≥58 | 28–31 | 7–11 | ≤0.10 | ≤0.50 | ≤0.50 | ≤0.50 | ≤0.04 | ≤0.015 | ||||||
| 718 | 50.0–55.0 | 17.0–21.0 | Balance | 2.8–3.3 | 4.75–5.5 | ≤1.0 | ≤0.35 | ≤0.3 | 0.2–0.8 | 0.65–1.15 | ≤0.35 | ≤0.08 | ≤0.015 | ≤0.015 | ≤0.006 |
| X-750 | ≥70.0 | 14.0–17.0 | 5.0–9.0 | 0.7–1.2 | ≤1.0 | ≤1.0 | ≤0.5 | 0.4–1.0 | 2.25–2.75 | ≤0.5 | ≤0.08 | ≤0.01 |
