+86-17335753350

Model No: Inconel® X-750 | UNS N07750 | W.Nr. 2.4669 | GH4145

Alloy X-750 High-Temperature Corrosion-Resistant Superalloy

Key Specifications at a Glance
Material Grade: Inconel® X-750 (UNS N07750 / W.Nr. 2.4669)
Density: 8.28 g/cm³
Melting Range: 1393 – 1427°C (2540 – 2600°F)
Key Strengthening Mechanism: Precipitation-hardened (γ' phase)
Available Forms: Bar, Sheet, Strip, Wire, Tube, Forging, Ring, Disc, Coil
Certifications: AS 9120B, ISO 9001:2015 (ZYTC Alloy)
Quantity :
Contact Now
Inconel® X-750 is a Nickel-Chromium alloy made precipitation hardenable by additions of Aluminium and Titanium, having creep-rupture strength at high temperatures to about 700°C (1290°F).
 
Alloy X-750 is widely used in aerospace engines, gas turbines, nuclear reactors, rocket engines, and high-temperature spring applications, where reliability under extreme stress and temperature conditions is non-negotiable. 
 
As a professional China nickel alloy supplier, ZYTC Alloy provides standardized Inconel® X-750 products including bars, plates, sheets, wires, forgings and custom machined parts. All materials comply with international industry standards, with complete heat treatment processes and full MTR certification, supporting global high-end equipment manufacturing and engineering procurement projects.

Why Choose ZYTC Alloy Inconel X-750 Superalloy?

Quality Assurance

We strictly adhere to ASTM B637,AMS 5598, AMS 5542,AMS 5582, AMS 5667 and AMS 5670 standards. Each batch undergoes chemical composition analysis, tensile testing, and hardness verification, with complete inspection reports provided to ensure full material traceability. Our AS 9120B and ISO 9001:2015 certifications guarantee supply chain quality management. 

Delivery Capability

We maintain stock for standard sizes across multiple forms (bar, sheet, wire, coil) and support custom length, diameter, and tolerance requirements, with a typical lead time of 4-6 weeks.

Technical Support

Our engineering team provides material selection guidance, heat treatment recommendations, and processing consultation to help you optimize product performance and cost.

 

Chemical Composition

ElementMinMax
Carbon--0.08
Manganese--0.30
Silicon--0.50
Sulfur--0.01
Nickel + Cobalt70.0 min
Chromium14.017.0
Iron5.009.00
Aluminum0.401.00
Titanium2.252.70
Copper--0.50
Cb + Ta0.701.20

Physical Properties

PropertyValue
Density8.28 g/cm³ 
Melting Range1393 – 1427°C 

Thermal Conductivity

TemperatureBtu-in/ft²-hr-°FW/m-K
°F°C
30014911716.9
60031614220.5
100053818426.5
120064919928.7
140076021831.4
160087124535.3

Electrical Resistivity

Conditionohm-cir mil/ftAt Room Temperaturemicrohm-mmAt Room Temperature
Hot Rolled7641270
Solution Treated7161190
Solution Treated and Aged7461240

Modulus of Elasticity

Temperaturepsi x 10⁶MPa x 10⁶
°F°C
8026.731.0213.7
500260.028.7197.9
1000538.025.0172.4
1350732.021.0144.8
1500816.018.5127.6

Coefficient of Thermal Expansion

Temperature Range10⁻⁶/°F10⁻⁶/°C
80°F to26.7°C to
200936.712.1
6003167.513.5
10005387.914.2
12006498.114.6
16008719.016.2
 
Specific Heat Temperature RangeBtu/lb-°FkJ/kg-K
77/212°F (25/100°C)0.10-0.110.42-0.46
77/1650°F (25/899°C)0.130.54

Heat Treatment

Heat Treatment MethodProcess StepTemperatureTimeCooling
Method 1 For maximum creep, relaxation and rupture strengthat temperatures above 1100°F (593°C)Solution Treatment1800°F (982°C)Commensurate with thicknessAir cool
Intermediate Age1550°F (843°C)24 hrsAir cool
Final Age1300°F (704°C)20 hrsAir cool
Method 2 For highest room temperature yield strengthand tensile ductilityStress Equalization1625°F (885°C)24 hrsAir cool
Precipitation Age1300°F (704°C)20 hrsAir cool

Typical Mechanical Properties

Room Temperature Mechanical Properties
TemperTensile Strength, psiYield Strength 0.2% offset, psiElongation in 2", %Hardness, Brinell
Hot-finished + 1300°F/20 hr,A.C170,000-206,000120,000-163,00025-15313-400
Hot-finished + Annealed1800°F/1 hr, A.C + 1350°F/8 hr, F.C. 100°F/hr to1150°F (total 18 hr), A.C.162,000-193,000115,000-142,00030-15300-390
Hot-finished + 1625°F/24 hr,A.C + 1300°F/20 hr, A.C.160,000-188,000100,000-135,00030-15302-363
Cold-rolled, annealed +1300°F/20 hr, A.C.160,000-197,000105,000-150,00030-20300-400

Applications & Industries

Inconel® X-750 delivers reliable performance across demanding industrial sectors:

✈️ Aerospace & Aviation

  • Gas turbine rotor blades, vanes, and structural components 

  • Aircraft thrust reversers and engine springs 

  • Rocket engine thrust chambers 

  • Bolts, fasteners, and ring components 

⚡ Energy & Power Generation

  • Gas turbine and steam turbine power plant components 

  • Nuclear reactor springs and core components 

  • High-temperature bolts and valve springs in petrochemical plants 

🔧 Industrial Manufacturing

  • High-temperature springs (flat, helical, compression) and spring clips 

  • Heat treatment fixtures, molding tools, and extrusion dies 

  • Pressure vessels and elastic sealing diaphragms 

  • Sensors and thermal air duct systems


Specifications

Product TypeStandards
RodASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
BarASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
Forging StockASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
PlateISO 6208, AMS 5542 and AMS 5598
SheetISO 6208, AMS 5542 and AMS 5598
StripISO 6208, AMS 5542 and AMS 5598
WireBS HR 505, AMS 5698, AMS 5699
OtherUNS N07750, W.Nr 2.4669, Inconel X750 (tradename), UNS N07752

Available Forms & Supply Condition

FormSupply Condition
Bar, Forging, RingAs-forged / hot-rolled, or solution-treated, with optional grinding/turning 
Sheet, Strip, PlateHot-rolled or cold-rolled, annealed or solution-treated, pickled/polished 
WireSolution-treated, or cold-drawn (up to 65% reduction) for smaller diameters 
Tube, Coil, DiscAs-rolled or annealed, available in multiple thicknesses and tempers
 
 

Workability

The furnace temperature should be 2100°F (1149°C)-for optimal starting temperatures of 1950/2000°F. For service below 1100°F (593°C), higher strength can be obtained by combining some cold work with heat treatment because the effects are additive.

Machinabiliy

Alloy X-750 work hardens quickly and is more difficult to machine than most standard ferritic and martensitic alloys. The alloy is most easily machined in the stress-equalized condition. Because specific cutting forces are high, the machine tools used must have ample power and the cutting speed should be slow. The tools must have smooth finishes, be sharp, and be very rigid. To avoid work hardening , a continuous, smooth cutting action should be maintained; thus, the machines must have a minimum of backlash and the tool and workpiece must be rigidly supported. If at all possible, avoid very small cuts and feeds.

Welding

Alloy X-750 should be welded in the stress-equalized condition, 1625°F (885°C) heat treatment, and solution treated and age hardened after welding has been completed. If this is not practical, the alloy should be welded in the solution-treated condition and age hardened after welding with or without the inclusion of a short-period stress-relieving treatment at 1625°F. Weld joints, because of softening of the alloy within the heat-affected zone, should be located where lower creep properties are required.

Certifications & Quality Assurance

  • ☑ AS 9120B – Aerospace quality management system certification
  • ☑ ISO 9001:2015 – International quality management standard
  • ☑ Full traceability – From melting through final delivery
  • ☑ Complete mill test reports – Available with every shipment

Request a Quote

Contact ZYTC Alloy for professional Inconel X-750 technical datasheets, custom specifications and factory competitive quotations.

📧 Email: daisy@zytcsteel.com
📲 WhatsApp: +86 17335753350

Inconel® is a registered trademark of Special Metals Corporation.


ZYTC Alloy – Your Partner in High-Performance Materials Since 1989.