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Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy

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Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy

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Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy Specification

Thickness
0.0201.00 mm Millimeter (mm)

Application
Gas Turbines, In-Vehicle Sensors, Heat-Resistant Springs, and Other High-Temperature Components

Temper
Annealed, Skin Passed, As Rolled (Hard)

Width
3.0300 mm Millimeter (mm)

Shape
Coil, Sheet, (Wire)

Surface
Bright, Dull

Grade
Alloy X750 (Inconel X750 Equivalent)

Chemical Composition
Refer to the image

Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy Trade Information

Payment Terms
Telegraphic Transfer (T/T)

Packaging Details
Our Standard Packing for Export

Main Export Market(s)
Asia, North America, South America, Eastern Europe, Western Europe, Middle East

About Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy

Grade	Alloy X750 (Inconel X750 Equiv.)
Reference Standards (for reference only)	UNS N07750 B637 AMS 5542 (Strip, Sheet) JIS NCF750 - G4901 (Bar), G4902 (Strip, Sheet) ISO NW7750, NiCr15Fe7Ti2Al GB NW7750, NiCr15Fe7Ti2Al
Shape	Coil, Sheet, (Wire)
Thickness	0.020-1.00(Strip, Sheet) Millimeter (mm)
Width	3.0-300(Strip, Sheet) Millimeter (mm)
Length	Strip or Sheet(Length less than 2,000mm)
Technique	Cold Rolled
Temper	Annealed, Skin passed, As Rolled(Hard)
Surface	Bright, Dull
Application	Gas TurbineIn-vehicle Sensors, Heat Resistant Springs,etc.
Coil I.D.	300, 400, 541mm
Chemical Composition	Refer to the image
Density	8.28 g/cm
Specific Heat	431 J/(kgK) (21)
Electrical Resistivity	122 cm (21)
Thermal Expansion	12.010^-6/K(20100)
Thermal Conductivity	12.0 W/(mK) (21)
Minimum Order Quantity	Please contact us.
Country of Origin	Japan
Payment Terms	Telegraphic Transfer (T/T)
Delivery Terms	EXW, FOB, CIF, DAP etc.
Packaging Details	Our Standard Packing for Export
Main Export Market(s)	Asia, Muddle East, North America, South America, Europe etc.

Alloy X750 (Inconel X750 Equiv.) - UNS N07750 Description:

Standard "UNS N07750 ASTM B637 AMS 5542 (Strip, Sheet) JIS NCF750 - G4901 (Bar), G4902 (Strip, Sheet) ISO NW7750, NiCr15Fe7Ti2Al GB NW7750, NiCr15Fe7Ti2Al"

Alloy X750 is a precipitation (age) hardening nickel-chromium alloy equivalent to Inconel X750. It is specifically designed to provide excellent mechanical strength, oxidation resistance, and corrosion resistance at elevated temperatures.

Through age-hardening heat treatment, Alloy X750 develops high tensile strength, creep resistance, and stress-rupture properties, making it suitable for demanding applications operating at temperatures up to approximately 815C.

The alloy maintains good resistance to oxidation and corrosion while retaining its mechanical integrity under cyclic thermal and mechanical loading conditions.

Typical applications include gas turbine components, automotive and industrial sensors, heat-resistant springs, reactor components, aerospace hardware, and high-temperature fastening systems.

We can supply Inconel X750 or equivalent materials according to customer requirements.

Superior High-Temperature Performance

Alloy X750 is engineered to maintain exceptional mechanical properties and oxidation resistance in environments with temperatures up to 704C (1300F). Its unique composition makes it suitable for components such as turbine blades, springs, and sensors in both aerospace and automotive industries. Its reliability under thermal stress has made it a trusted material for critical high-temperature systems.

Versatile Forms and Finishes

Available as coils, sheets, and wires, Alloy X750 comes in a range of customizable dimensions to suit complex engineering needs. Surfaces can be supplied in bright or dull finishes, and tempers include annealed, skin passed, or as rolled hard. This flexibility accommodates specific design requirements across diverse industries.

FAQ's of Alloy X750 (Inconel X750 Equiv.) - UNS N07750 | Nickel Alloy:

Q: How is Alloy X750 commonly processed for use in high-temperature applications?

A: Alloy X750 is typically processed by annealing, skin passing, or rolling to tailor its mechanical properties for demanding environments. These processes enhance its strength, ductility, and heat resistance, ensuring reliability in gas turbines, heat-resistant springs, and sensors.

Q: What are the main benefits of using Alloy X750 coils, sheets, and wires?

A: The primary advantages include superior resistance to oxidation and corrosion at high temperatures, excellent mechanical strength, and stability in demanding conditions. These properties make Alloy X750 ideal for critical components in turbines, vehicles, and other heat-intensive applications.

Q: Where is Alloy X750 (Inconel X750 Equivalent) primarily manufactured and supplied?

A: Alloy X750 is manufactured, exported, and supplied by companies based in Japan, serving clients around the globe in aerospace, automotive, and power generation industries.

Q: What applications benefit most from using Alloy X750?

A: Industries that demand durability in extreme environments, such as aerospace, automotive (in-vehicle sensors), and energy (gas turbines, springs), benefit greatly from Alloy X750 due to its high-temperature performance and longevity.

Q: How do the surface finishes, bright and dull, impact the use of Alloy X750 products?

A: Surface finishes are selected based on application requirements. Bright surfaces offer a polished look and can be easier to inspect, while dull finishes may be preferred for their reduced glare or for applications where aesthetic appearance is secondary to function.

Q: When should I consider using annealed versus as rolled (hard) Alloy X750 material?

A: Annealed Alloy X750 is chosen for applications requiring enhanced ductility and ease of fabrication, while as rolled (hard) material is preferred when maximum strength and wear resistance are required in service.

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