Inconel 617 alloy round bar price per kilogram
Inconel 617 alloy round bar price per kilogram is commonly about USD 45 to 90 per kg for standard industrial stock sizes. Large forged bars, small pre...
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 (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 |
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 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 |
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 |
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 |
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 |
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 |
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 |
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 |
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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