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Alloy X750,Inconel X750 Forgings,UNS N07752,E FORU

Product Code : NI-S218-CU-CU

Alloy X750,Inconel X750 Forgings,UNS N07752, is available in Bar (Round bar, Flat bar), Ribbon, Wire, Rods, Tube, Pipe, Foil, Plate, Sheet, Strip and Forging Stock.

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Product Product Code Purity Size Contact Us
Alloy X750,Inconel X750 Forgings,UNS N07752NI-S218-CU-CUCustomizedCustomized
British Specs:,American Specs:AMS 5542 Sheet, Strip and Plate AMS 5582 Seamless Tube AMS 5583 Seamless Tube AMS 5747 Bar and Forgings AMS 5779 Welding Electrodes AMS 5598 Sheet, Strip and Plate AMS 5667 Bar and Forgings AMS 5668 Bar and Forgings AMS 5669 Bar AMS 5670 Bar and Forgings AMS 5671 Bar and Forgings AMS 5698 Wire AMS 5699 Wire,German Specs:WS 2.4669
### **Product Introduction: Alloy X-750 / Inconel X-750 Forgings (UNS N07750)** #### **Overview** **Alloy X-750 Forgings** (commercially known as **Inconel® X-750 Forgings**) represent the premium form of this precipitation-hardenable nickel-chromium superalloy, specifically engineered for critical applications demanding exceptional high-temperature strength and reliability. The forging process significantly enhances the alloy's grain structure, mechanical properties, and metallurgical integrity throughout the component. Inconel X-750 forgings deliver outstanding strength retention, excellent creep rupture properties, and superior oxidation resistance at temperatures up to 700°C (1300°F), making them indispensable for aerospace, nuclear, and high-temperature industrial applications. The combination of specialized forging techniques and the alloy's unique precipitation-hardening capability through gamma prime [γ'-Ni₃(Al,Ti)] phase formation results in components with optimized grain flow, improved fatigue resistance, and enhanced mechanical properties for the most demanding service conditions. --- #### **Chemical Composition** The chemical composition of Alloy X-750 Forgings (UNS N07750) meets rigorous international standards: | Element | Content (%) | |---------|-------------| | **Nickel (Ni)** | 70.0 minimum | | **Chromium (Cr)** | 14.0 - 17.0 | | **Iron (Fe)** | 5.0 - 9.0 | | **Titanium (Ti)** | 2.25 - 2.75 | | **Copper (Cu)** | 0.50 maximum | | **Aluminum (Al)** | 0.40 - 1.00 | | **Niobium (Nb)** | 0.70 - 1.20 | | **Carbon (C)** | 0.08 maximum | | **Manganese (Mn)** | 1.00 maximum | | **Silicon (Si)** | 0.50 maximum | | **Sulfur (S)** | 0.01 maximum | *Note: The optimized composition enables superior precipitation hardening response through gamma prime [γ'-Ni₃(Al,Ti)] phase formation during controlled heat treatment cycles.* --- #### **Physical Properties** Critical properties for forged component design and performance: | Property | Metric Value | Imperial Value | |----------|--------------|----------------| | **Density** | 8.28 g/cm³ | 0.298 lb/in³ | | **Melting Range** | 1390 - 1430 °C | 2530 - 2600 °F | | **Specific Heat (20°C)** | 431 J/kg·K | 0.103 Btu/lb·°F | | **Thermal Conductivity (20°C)** | 11.8 W/m·K | 81.9 Btu·in/hr·ft²·°F | | **Thermal Expansion Coefficient (20-100°C)** | 12.8 μm/m·°C | 7.1 μin/in·°F | | **Modulus of Elasticity** | 214 GPa | 31.0 x 10⁶ psi | | **Electrical Resistivity** | 1.22 μΩ·m | - | --- #### **Mechanical Properties** Enhanced mechanical properties achieved through controlled forging and heat treatment: **Solution Annealed + Aged Condition (AMS 5668):** * **Ultimate Tensile Strength:** 1100-1270 MPa (160-184 ksi) * **Yield Strength (0.2% Offset):** 760-930 MPa (110-135 ksi) * **Elongation:** 15-25% * **Reduction of Area:** 25-40% * **Hardness:** 34-42 HRC **Elevated Temperature Performance:** * **0.2% Yield Strength at 650°C (1200°F):** ≥ 690 MPa (100 ksi) * **Stress Rupture Life at 700°C (1300°F):** ≥ 100 hours at 170 MPa (25 ksi) * **Creep Resistance:** Excellent up to 700°C (1300°F) --- #### **International Standards** Alloy X-750 Forgings comply with stringent international specifications: **Aerospace Material Specifications:** * **AMS 5668:** Bars, Forgings, and Rings * **AMS 5671:** High-Strength Springs **ASTM Standards:** * **ASTM B637:** Precipitation-Hardening Nickel Alloy Bars, Forgings, and Forging Stock * **ASTM B564:** Standard Specification for Nickel Alloy Forgings **Quality & Testing Standards:** * **AMS 2269:** Chemical Check Analysis Limits * **ASTM E112:** Grain Size Determination * **ASTM A388:** Ultrasonic Examination of Heavy Steel Forgings --- #### **Product Applications** Alloy X-750 forgings serve in the most critical applications across industries: **Aerospace & Defense:** * **Gas Turbine Engines:** Turbine disks, compressor disks, shafts, blades, and spacers * **Rocket Systems:** Turbopump components, thrust chambers, nozzle parts * **Aircraft Structures:** Landing gear components, engine mounts, wing fittings * **Spacecraft:** Critical structural components and propulsion elements **Nuclear Industry:** * **Reactor Components:** Core support structures, control rod mechanisms * **Reactor Vessel Internals:** Bolting, springs, and fastening systems * **Nuclear Fuel Assemblies:** Spacer components, support structures **Power Generation:** * **Gas Turbines:** Rotor disks, blade rings, shaft components * **Steam Turbines:** High-pressure rotor sections, valve stems * **Turbine Generators:** Rotor end rings, retaining rings **Industrial Applications:** * **High-Temperature Fasteners:** Large bolts, studs, and special fasteners * **Tooling & Fixtures:** High-temperature processing fixtures * **Test Equipment:** High-temperature test components * **Chemical Processing:** Reactor components, valve bodies --- #### **Key Advantages** * **Superior Grain Structure:** Refined, uniform grain size with optimized grain flow * **Enhanced Mechanical Properties:** Improved strength, ductility, and toughness compared to cast products * **Excellent High-Temperature Strength:** Maintains mechanical properties up to 700°C (1300°F) * **Outstanding Creep Resistance:** Superior stress rupture properties * **Improved Reliability:** Reduced incidence of internal defects and improved structural integrity * **Excellent Fatigue Resistance:** Superior performance under cyclic loading conditions * **Better Microstructural Control:** Controlled precipitation and phase distribution * **Optimized Grain Flow:** Grain structure aligned with component stress patterns **Forging Capabilities:** * **Open Die Forgings:** Large, complex shapes and custom configurations * **Closed Die Forgings:** Precision forgings with minimal machining requirements * **Ring Rolled Forgings:** Large diameter rings for rotational components * **Press Forgings:** High-tonnage press forgings for critical components **Heat Treatment Specifications:** * **Solution Treatment:** 1150-1200°C (2100-2200°F) followed by rapid cooling * **Aging Treatment:** 705-730°C (1300-1350°F) for 16-20 hours, air cool * **Double Aging:** Optional second aging at 650°C (1200°F) for enhanced properties **Quality Assurance:** * **Ultrasonic Testing:** Full component scanning for internal defects * **Chemical Analysis:** Complete composition verification * **Mechanical Testing:** Tensile, impact, and hardness testing * **Microstructural Examination:** Grain size and phase distribution analysis * **Dimensional Inspection:** Comprehensive measurement and verification **Note:** *Inconel® is a registered trademark of Special Metals Corporation. Alloy X-750 forgings are typically supplied in the solution treated and aged condition (STA) with comprehensive certification including chemical analysis, mechanical properties, microstructural examination, and non-destructive testing reports. Special quality requirements such as enhanced ultrasonic testing, grain size control, and specific heat treatment protocols are available to meet unique application demands. Proper machining and handling procedures are essential to maintain the integrity of these high-performance components.* *Correction: The correct UNS designation for Inconel X-750 is N07750, not N07752 as mentioned in the request. All technical information provided corresponds to UNS N07750.*
Packing of 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 1841 gallon liquid totes Special package is available on request.
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