Inconel X-750
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Inconel X-750

Similar grades: GH4145 (China), NiCr15Fe7TiAl (Germany), NC15FeTNbA (France), NCF750 (Japan)
Certification: ISO9001:2015
Alloy category: corrosion-resistant alloy
Substrate shape: axial wire/strip/straight bar
Alloy series: nickel-chromium alloy
Implementation standard: ASTM B637
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As a leading supplier and manufacturer in China, GNEE Steel provides cost-effective nickel-based alloy products.

Product Introduction

Gnee Super Alloy (Tianjin) Co., Ltd. is one of the most professional manufacturers and suppliers of inconel x-750 in China. If you're going to wholesale high quality inconel x-750 made in China, welcome to get free sample from our factory. Good service and reasonable price are available.

 

 

Inconel X-750 introduce

Inconel X-750
 
 

Gnee Alloy Inconel X-750 introduce

Inconel X-750 is a precipitation-hardening nickel-chromium superalloy renowned for its excellent high-temperature strength, outstanding oxidation resistance, and superior stress relaxation properties up to 700°C (1290°F). It is widely used in critical applications such as gas turbine springs, rocket engines, and nuclear reactor components.

Inconel X-750 equivalent grade 

Specification Equivalent
UNS N07750
AMS 5598, 5667, 5698, 5699
ASTM B637
DIN W.Nr. 2.4669

Inconel X-750 Available Shape

 

 

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Inconel X-750 Seamless Pipe

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Inconel X-750 Plate

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Inconel X-750 Pipe Fitting

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Inconel X-750 Bar

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Click to get a quote for Inconel 625 products

 

Rod ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
Bar ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
Forging Stock ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269
Plate ISO 6208, AMS 5542 and AMS 5598
Sheet ISO 6208, AMS 5542 and AMS 5598
Other UNS N07750, W.Nr 2.4669, Inconel X750 (tradename), UNS N07752

 

Inconel X-750 Specification

 

Inconel X750 Chemical Composition:
Grade C Mn Si S Cu Al Ti Co Nb+Ta Fe Cr Ni
Inconel X750 0.08 max 1.0 max 0.5 max 0.01 max 0.5 max 0.4 – 1.0 2.25-2.75 1.0 max 0.7 – 1.2 5.0 – 9.0 14.00 – 17.00 70.0 min

 

Inconel X-750 Mechanical Properties (by Product Type):

Product Form Tensile Strength (MPa) Yield Strength (MPa) Elongation (%)
Bar (≤ 25 mm) ≥ 1200 ≥ 850 ≥ 15
Bar (25 – 50 mm) ≥ 1170 ≥ 820 ≥ 12
Bar (50 – 100 mm) ≥ 1100 ≥ 750 ≥ 10
Plate (≤ 10 mm) ≥ 1100 ≥ 700 ≥ 15

 

Physical characteristics of Inconel X-750:

Property Value Unit Significance
Density 8.28 g/cm³ Weight calculation
Melting Range 1390 – 1430 °C Fire resistance margin
Thermal Conductivity (20°C) 11.5 – 12.5 W/m·K Heat dissipation
Thermal Conductivity (500°C) ~18.0 W/m·K High-temperature performance
CTE (20-100°C) 13.0 × 10⁻⁶ /°C Fitting compatibility
CTE (20-600°C) ~14.5 × 10⁻⁶ /°C High-temperature design
Specific Heat (20°C) 440 J/kg·K Thermal capacity
Specific Heat (600°C) ~520 J/kg·K High-temperature thermal capacity
Modulus of Elasticity (20°C) ~214 GPa Stiffness
Modulus of Elasticity (600°C) ~175 GPa Hot stiffness
Electrical Resistivity 1.22 µΩ·m -
Magnetic Properties Non-magnetic - -

 

Inconel X-750 high temperature and corrosion resistance

 

High-Temperature Mechanical Properties (Aged Condition)

Temp (°C) Tensile Strength (MPa) Yield Strength (MPa) Elongation (%) Strength Retention (%)
20 (RT) ≥ 1100 – 1200 ≥ 700 – 900 15-25 100%
300 ~1050 ~750 ~18 92%
400 ~1000 ~720 ~20 88%
500 ~950 ~680 ~22 83%
550 ~900 ~640 ~24 79%
600 ~850 ~600 ~26 74%
650 ~780 ~550 ~28 68%
700 ~700 ~500 ~30 61%
750 ~600 ~430 ~32 52%
800 ~500 ~360 ~35 44%

 

Corrosion Resistance

Environment Resistance Level Notes
Oxidizing Acids (HNO₃) Good -
Reducing Acids (H₂SO₄, HCl) Poor Not recommended
Chloride Pitting Moderate -
Chloride Stress Corrosion Cracking Moderate -
Seawater Limited -
High-Temperature Oxidation (to 980°C) Excellent -
High-Temperature Sulfidation Good -

 

Corrosion Resistance Rating (1-5, 5 = best)

Environment Inconel X-750
Nitric Acid 4
Sulfuric Acid 2
Hydrochloric Acid 1
Seawater 2
High-Temp Oxidation (980°C) 5

 

Inconel X-750 Heat Treatment Schedule

 

Step Treatment Temperature Time Cooling Purpose
1. Solution Treatment Full solution 980 – 1020°C 1-2 hours Rapid cool (water or air) Dissolve γ′
2. First Aging Age hardening 845°C (1550°F) 2-4 hours Air cool Coarsen γ′
3. Second Aging Age hardening 700°C (1290°F) 16-20 hours Air cool Fine γ′ precipitation

Alternative Heat Treatment (Springs)

Step Treatment Temperature Time Cooling
1. Solution Treatment Full solution 980 – 1020°C 1-2 hours Rapid cool
2. Aging Age hardening 730°C 16 hours Air cool

 

Applications of inconel X-750

 

Industry Application Operating Temperature Key Requirements
Aerospace Turbine blades, seals, fasteners, springs 500 – 750°C High-temp strength, creep resistance
Gas Turbines High-temperature springs, bolts, seals 500 – 700°C Relaxation resistance
Nuclear Reactor core springs, fasteners 300 – 600°C Creep resistance, non-magnetic
Automotive High-performance exhaust springs 500 – 650°C Relaxation resistance
Chemical Processing High-temperature fasteners 400 – 600°C Strength, oxidation resistance
Power Generation Turbine fasteners, springs 500 – 700°C Creep resistance
product-1000-666
Turbine blades
High-temperature springs
High-temperature springs
Reactor core components
Reactor core components
High-temperature fasteners
High-temperature fasteners

 

Comparison of Inconel X-750 with other alloys

 

Property Inconel X-750 Inconel 718 Inconel 625
Strengthening Mechanism γ′ (Ti+Al) γ″ + γ′ (Nb) Solid-solution
Tensile Strength (RT) 1100-1200 MPa 1275 MPa 830 MPa
Yield Strength (RT) 700-900 MPa 1035 MPa 415 MPa
Elongation 15-25% 12% 30%
Max Service Temp 700-750°C 650-700°C 600°C
Spring Application Excellent Good Fair
Relaxation Resistance Excellent Good Poor
Cost High High Moderate

 

Inconel X-750 Packaging 

GNEE Group Inconel X-750 Product Packaging

GNEE Group Nickel Alloy X-750 Product Suppliers
GNEE Group Inconel X-750 Product Suppliers
GNEE Group Nickel Alloy X-750 Packaging
GNEE Group Inconel X-750 Packaging

Inconel X-750 Non-Destructive Testing (NDT)

GNEE Group Inconel X-750 Testing

 

Test Method Requirement Standard Acceptance Criteria
Ultrasonic Testing (UT) As specified (bars ≥ 12mm) ASTM E2375 No defects exceeding 0.8mm
Eddy Current Testing (ET) As specified (wire/spring) ASTM E426 No relevant indications
Liquid Penetrant Inspection (LPI) As specified ASTM E1417 No relevant indications
Visual Inspection 100% - No surface defects
GNEE Group Alloy X-750 Testing
GNEE Group Inconel X-750 Testing
GNEE Group Inconel Alloy X-750 Production and processing
GNEE Group Inconel X-750 Production and processing    

Global Export Solutions for Inconel X-750

 

Target Market Key Requirements / Characteristics
European & American Aviation / Energy Markets Mandatory compliance with AMS series aviation standards; must provide aging heat treatment process reports, fatigue performance test data, and UT NDT reports; TUV 3.2 third‑party certification is a bidding requirement
Middle East Gas Turbine Projects Focuses on high‑temperature stress relaxation resistance and durability fatigue data; accepts UNS N07750 designation; mandatory EN10204 3.1 material certificate
Southeast Asian High‑End Industrial Markets Primarily ex‑stock precision wire and bar products; adapted to high‑end equipment supporting orders; short delivery lead times with high performance‑to‑price ratio stability

 

About Gnee Alloy

Gnee Alloy

 

Quick Inquiry Guide for Inconel X-750 Products

Provide the following key parameters to receive an accurate quote and a comprehensive technical compliance package, suitable for overseas project bidding and procurement planning:

1. Product Category: Wire, rod, plate, forgings, or precision-machined parts; include specific dimensional tolerances and surface finish requirements.
2. Operating Conditions: Working temperature, dynamic/static loads, and service environment (e.g., air, flue gas, or mildly corrosive media).
3. Processing Requirements: Precision grinding, cutting, forming, or customized aging parameters.
4. Certification Requirements: Standard 3.1 certificates, third-party aerospace-grade certification, or specific testing reports.
Premium Export Services: Free guidance on material selection based on operating conditions, complimentary sample testing, full process traceability, dedicated one-on-one technical support for overseas projects, and one-stop assistance with customs clearance documentation.

Contact us to create a tailored solution for your project

 

Gnee Alloy inconel X-750 certificate

Gnee Alloy inconel X-750 certificate

FAQ

 

Q1: What are the key differences in material selection between X-750 and Inconel 718?
A:
Inconel 718 excels in high-strength, high-pressure static applications, making it ideal for fixed structural components. X-750's unique advantages lie in its resistance to high-temperature relaxation, durability under dynamic fatigue, and elastic stability; it is the premier choice for high-temperature springs, dynamic seals, and components subject to repeated fastening. The two materials are not interchangeable.
 

Q2: Do finished X-750 products require secondary aging treatment by the customer?
A:
All exported finished products undergo standardized double-aging heat treatment, fully meeting mechanical and elastic performance standards. Customers can proceed directly to machining and assembly without further heat treatment, significantly reducing overseas construction costs.
 

Q3: What is the maximum operating temperature for X-750 in dynamic applications?
A:
It supports long-term, stable dynamic service at temperatures up to 650°C. Within this range, it maintains minimal elastic decay and excellent fatigue resistance, far outperforming standard stainless steels and conventional nickel-based alloys.
 

Q4: Which high-end export certifications can be met?
A:
We support AMS aerospace standard certification, ASME engineering compliance certification, EN10204 3.1/3.2 certification, and third-party witness testing by SGS/TÜV, making the products suitable for high-end project tenders in aerospace, nuclear power, and gas turbine sectors.
 

Q5: What are the delivery lead times for different product categories?
A:
7–15 working days for standard stock bars and plates; 10–18 working days for precision spring wire; 20–30 working days for custom precision-machined components and complex forgings. Expedited production is available for urgent, high-priority orders.

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