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Inconel X-750 Nickel Alloy Bar Manufacturer

2026-03-09

Inconel X-750 is a precipitation-hardenable nickel-chromium alloy known for its high tensile and creep-rupture strength at temperatures up to 1300°F (700°C). As a critical material for aerospace, power generation, and industrial applications, sourcing high-quality Inconel X-750 bars from a reliable manufacturer is essential for ensuring component performance and regulatory compliance. This article provides comprehensive information about Inconel X-750 nickel alloy bars, including specifications, available forms, mechanical properties, and manufacturing considerations.

Inconel X-750

Product Overview and Specifications

Inconel X-750 (UNS N07750) is manufactured to various specifications depending on the application and end-user requirements. Shanghai NC Metal Materials Co., Ltd. produces Inconel X-750 bars in compliance with multiple international standards to serve diverse industry needs.

Specification Title Typical Applications
ASTM B637 Standard Specification for Precipitation-Hardening Nickel Alloy Bars, Forgings, and Forging Stock General industrial, valve components, fasteners
AMS 5667 Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72.5Ni – 15.5Cr – 0.95Cb – 2.5Ti – 0.70Al – 7.0Fe Consumable Electrode or Vacuum Induction Melted Aerospace components, gas turbine parts
AMS 5668 Same as AMS 5667 but with different heat treatment Springs, bellows, specific aerospace applications
AMS 5698 Nickel Alloy, Corrosion and Heat-Resistant, Wire Spring wire, cold-formed components
AMS 5699 Nickel Alloy, Corrosion and Heat-Resistant, Wire, Spring Temper High-strength springs, fasteners
NACE MR0175/ISO 15156 Petroleum and natural gas industries – Materials for use in H2S-containing environments Oil and gas downhole tools, sour service components

Chemical Composition Requirements

The unique properties of Inconel X-750 derive from its carefully balanced chemical composition, which includes precipitation-hardening elements such as aluminum, titanium, and niobium. Shanghai NC Metal Materials Co., Ltd. ensures all bars meet the compositional requirements of applicable specifications.

Element UNS N07750 Requirement (%) Typical Analysis (%) Role in Alloy
Nickel (plus Cobalt) 70.0 min 73.0 Base element; provides austenitic structure and corrosion resistance
Chromium 14.0 – 17.0 15.5 Oxidation and corrosion resistance at elevated temperatures
Iron 5.0 – 9.0 7.0 Strengthening and cost control
Titanium 2.25 – 2.75 2.5 Primary precipitation hardening element with aluminum
Aluminum 0.40 – 1.00 0.7 Precipitation hardening and oxidation resistance
Niobium (plus Tantalum) 0.70 – 1.20 0.95 Strengthening and carbide formation
Manganese 1.00 max 0.5 Deoxidizer and sulfur control
Silicon 0.50 max 0.25 Deoxidizer
Carbon 0.08 max 0.04 Grain boundary strengthening through carbide formation
Sulfur 0.01 max 0.005 Kept low for hot workability and weldability
Copper 0.50 max 0.2 Residual element

Inconel X-750

Available Bar Sizes and Conditions

Inconel X-750 bars are available in a wide range of diameters and conditions to suit different manufacturing processes and final applications. Shanghai NC Metal Materials Co., Ltd. maintains inventory of standard sizes and can produce custom dimensions.

Diameter Range (inches) Diameter Range (mm) Available Conditions Typical Applications Reference Price Indicator
0.125″ to 0.500″ 3.2mm to 12.7mm Cold drawn, annealed, or precipitation hardened Small fasteners, springs, instrument components Higher per pound due to processing
0.501″ to 2.000″ 12.8mm to 50.8mm Hot rolled, centerless ground, annealed or aged Bolts, studs, valve stems, pump shafts Baseline reference
2.001″ to 4.000″ 51mm to 101.6mm Hot rolled or forged, rough turned, annealed Large fasteners, turbine components, die parts Moderate size premium
4.001″ to 8.000″ 102mm to 203mm Forged, rough machined, annealed Large shafting, seal rotors, heavy equipment Significant size premium
8.001″ to 12.000″ 203mm to 305mm Forged, rough machined, annealed Large rings, flanges, pressure vessel components Highest size premium

Mechanical Properties at Various Conditions

Inconel X-750 derives its strength from precipitation heat treatment. The mechanical properties vary significantly depending on the heat treatment condition and test temperature.

Condition Tensile Strength (ksi) min Yield Strength (ksi) min Elongation (%) min Hardness (typical)
Annealed (Solution Treated) 100 – 120 40 – 60 30 – 40 85 HRB
Precipitation Hardened (AMS 5667) 160 – 185 100 – 130 20 – 25 30 – 35 HRC
Precipitation Hardened (AMS 5668) 170 – 195 110 – 140 15 – 20 35 – 40 HRC
Spring Temper Wire (AMS 5699) 200 – 240 160 – 200 5 – 10 40 – 45 HRC

Elevated Temperature Properties

A key advantage of Inconel X-750 is its ability to maintain strength at elevated temperatures, making it suitable for gas turbine and high-temperature industrial applications.

Test Temperature (°F) Tensile Strength (ksi) Yield Strength (ksi) Elongation (%) 100-Hour Rupture Strength (ksi)
Room Temperature 170 115 22
1000°F (538°C) 150 100 18 95
1200°F (649°C) 130 90 12 60
1400°F (760°C) 85 70 8 25

Heat Treatment Options

Inconel X-750 can be heat treated to achieve different property combinations. The selection of heat treatment cycle depends on the intended application and required mechanical properties.

Heat Treatment Cycle Description Resulting Properties Typical Applications
Solution Annealed Heat to 2050°F (1121°C), hold, rapid cool Softest condition, maximum ductility, lowest strength Extensive forming, cold working prior to aging
Standard Age (AMS 5667) Solution treat + 1300-1350°F (704-732°C) for 20 hours, air cool Good combination of strength and ductility General purpose aerospace and industrial
High Strength Age (AMS 5668) Solution treat + 1325°F (718°C) for 8 hours, furnace cool to 1150°F (621°C), hold 8 hours, air cool Maximum strength, reduced ductility Springs, high-stress fasteners
Dual Age Modified cycles with intermediate steps Optimized properties for specific applications Specialized aerospace and nuclear

Applications by Industry

Inconel X-750 bars find use across multiple industries where high strength at elevated temperatures and corrosion resistance are required.

Industry Applications Key Property Requirements
Aerospace Gas turbine blades, seals, locks, fasteners, springs, afterburner parts High temperature strength, creep resistance, fatigue life
Power Generation Gas turbine components, nuclear reactor internals, control rod mechanisms Radiation resistance, high temperature stability
Oil and Gas Downhole tools, subsurface safety valves, wellhead components, springs Sour service resistance, high strength, corrosion resistance
Industrial Heat treatment fixtures, furnace components, extrusion dies, forming tools Thermal stability, oxidation resistance, wear resistance
Automotive Turbocharger components, exhaust valves, high-performance engine parts High temperature strength, thermal fatigue resistance
Chemical Processing Reactor components, valve parts, pump shafts, springs Corrosion resistance, high strength

Manufacturing Capabilities

Shanghai NC Metal Materials Co., Ltd. offers comprehensive manufacturing capabilities for Inconel X-750 bars, ensuring consistent quality and timely delivery for global customers.

Process Capability Quality Control
Melting VIM (Vacuum Induction Melting) + VAR (Vacuum Arc Remelting) for aerospace grades Chemical analysis, inclusion rating
Hot Working Rolling, forging, extrusion up to 12″ diameter Temperature control, reduction monitoring
Cold Working Drawing, centerless grinding, polishing Dimensional inspection, surface finish
Heat Treatment Solution annealing, precipitation hardening, stress relieving Temperature uniformity, soak time verification
Testing Tensile, hardness, ultrasonic, microstructure, corrosion Certified laboratory, NIST traceable

Quality Assurance and Certification

Shanghai NC Metal Materials Co., Ltd. maintains rigorous quality assurance protocols to ensure every Inconel X-750 bar meets customer requirements and applicable specifications. All materials are supplied with complete traceability and certification.

Documentation Type Description Typical Requirements
Mill Test Certificate (MTC) Certifies chemical composition and mechanical properties Required for all shipments
Heat Traceability Individual heat identification and tracking Aerospace and nuclear applications
Third-Party Inspection Independent verification by customer-nominated agency Upon customer request
NACE Compliance Certification for sour service applications Oil and gas industry
Country of Origin Documentation of manufacturing location Customs and procurement requirements

Frequently Asked Questions About Inconel X-750 Bars

What are the key differences between Inconel X-750 and Inconel 625 for high-temperature applications?

Inconel X-750 and Inconel 625 serve different purposes in high-temperature applications. X-750 is precipitation-hardenable, allowing it to achieve significantly higher strength through heat treatment, with tensile strengths exceeding 180 ksi in the aged condition. It is preferred for components requiring high mechanical loads at temperatures up to 1300°F, such as turbine blades, springs, and fasteners. Inconel 625 is solid-solution strengthened and cannot be precipitation hardened, offering lower strength but superior fabricability and weldability. 625 also provides better resistance to pitting and crevice corrosion in seawater environments. The choice depends on whether strength or corrosion resistance is the primary requirement for the specific application.

How does the heat treatment process affect the properties of Inconel X-750 bars?

The heat treatment process fundamentally determines the final properties of Inconel X-750 bars. In the solution annealed condition, the alloy is relatively soft and ductile, suitable for forming operations. The precipitation hardening treatment causes the formation of fine gamma prime Ni3(Al,Ti) precipitates throughout the microstructure, which block dislocation movement and dramatically increase strength. The specific aging cycle influences precipitate size and distribution. Standard aging produces a balance of strength and ductility, while modified cycles with controlled cooling rates can optimize specific properties such as creep resistance or high-temperature fatigue life. Improper heat treatment can result in overaging, reduced strength, or undesirable grain boundary carbide networks.

What specifications should I require when ordering Inconel X-750 bars for aerospace applications?

For aerospace applications, Inconel X-750 bars should typically be ordered to AMS specifications rather than ASTM standards. The most common aerospace specification is AMS 5667 for bars and forgings in the precipitation hardened condition. For spring applications, AMS 5699 for spring temper wire is appropriate. Additionally, aerospace orders often require supplementary requirements such as ultrasonic inspection per AMS 2630, magnetic particle inspection per AMS 3040, and certification of melting practice requiring VIM+VAR processing. Purchasers should also specify whether the material requires AMS 5668 (high strength age) or AMS 5667 (standard age). Shanghai NC Metal Materials Co., Ltd. can supply Inconel X-750 bars to all applicable aerospace specifications with complete certification and traceability.

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