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GH3030 alloy - high-temperature resistant nickel-based superalloy

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GH3030 alloy - high-temperature resistant nickel-based superalloy

MOQ:	100KG
Price:	Price is negotiated based on the required specifications and quantity
Standard Packaging:	Standard export packaging, or packaging as required
Delivery Period:	5-8 working days, depending on the parameters required for negotiation
Payment Method:	Payment Terms: Mainly T/T.. L/C, D/A, D/P,
Supply Capacity:	5000 tons per month

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Zhonggong Special Metallurgy

Certification

ISO Certificate

Model Number

GH3030 alloy

Composition:

Nickel-based Superalloy Containing Chromium, Iron, And Nickel

Density:

8.08 G/cm³

Melting Point:

1370-1425°C (2498-2597°F)

Yield Strength (0.2% Offset):

700-900 MPa (at Room Temperature)

Elongation:

45-55%

Thermal Conductivity:

11.6 W/m·K (at 100°C)

Specific Heat Capacity:

424 J/kg·K (at 20°C)

Coefficient Of Thermal Expansion:

12.2 µm/m·K (20-100°C)

Electrical Resistivity:

1.15 µΩ·m (at 20°C)

1.15 µΩ·m (at 20°C):

Non-magnetic

Hardness:

HRB 95 (max)

Applications:

Gas Turbine Components, Aerospace Components, High-temperature Applications

Highlight:

temperature resistant nickel based alloys

temperature resistant nickel based superalloy

aerospace components nickel based alloys

Product Description

GH3030 alloy, also known as Inconel Alloy 718, is a nickel-based superalloy renowned for its exceptional combination of high-temperature strength, corrosion resistance, and oxidation resistance. It is widely used in various industries where reliability under extreme conditions is paramount.

Key Features:

High-Temperature Strength: GH3030 retains significant mechanical strength at elevated temperatures up to approximately 700°C (1300°F), making it suitable for applications in gas turbines, aerospace components, and high-temperature industrial environments.
Corrosion and Oxidation Resistance: The alloy exhibits excellent resistance to corrosion and oxidation in a wide range of aggressive environments, including aqueous and high-temperature gases.
Chemical Composition: GH3030 is composed primarily of nickel (about 52%), chromium (20-24%), iron (5-15%), and smaller amounts of niobium, titanium, and aluminum. This composition contributes to its superior mechanical and thermal properties.
Mechanical Properties: It offers high tensile and yield strength, with good ductility and toughness even after prolonged exposure to high temperatures.
Applications: Common applications include components for gas turbines, jet engines, aerospace parts, industrial furnaces, and high-temperature chemical processing equipment.
Processing and Fabrication: GH3030 can be processed using conventional methods such as forging, machining, and welding. Its weldability and formability allow for versatile manufacturing capabilities.
Non-Magnetic Properties: GH3030 is non-magnetic in the annealed condition, making it suitable for applications where magnetic interference must be minimized.

GH3030 alloy is recognized for its reliability and performance in demanding environments, offering a balance of strength, resistance to environmental degradation, and ease of fabrication that meets the stringent requirements of high-performance industries.

Here's a typical composition table for GH3030 alloy (Inconel Alloy 718):

Element	Composition (%)
Nickel (Ni)	Balance
Chromium (Cr)	19.0 - 21.0
Iron (Fe)	18.5 - 20.0
Niobium (Nb)	5.0 - 5.5
Molybdenum (Mo)	2.8 - 3.3
Titanium (Ti)	0.65 - 1.15
Aluminum (Al)	0.2 - 0.8
Cobalt (Co)	≤ 1.0
Manganese (Mn)	≤ 0.35
Silicon (Si)	≤ 0.35
Copper (Cu)	≤ 0.30
Carbon (C)	≤ 0.08
Sulfur (S)	≤ 0.015
Phosphorus (P)	≤ 0.015

This composition table outlines the typical ranges of key elements present in GH3030 alloy (Inconel Alloy 718), providing insight into its chemical makeup essential for its high-temperature strength and corrosion resistance properties.

GH3030 alloy - high-temperature resistant nickel-based superalloy 0

GH3030 alloy - high-temperature resistant nickel-based superalloy 1

Tags:

Products

MOQ:	100KG
Price:	Price is negotiated based on the required specifications and quantity
Standard Packaging:	Standard export packaging, or packaging as required
Delivery Period:	5-8 working days, depending on the parameters required for negotiation
Payment Method:	Payment Terms: Mainly T/T.. L/C, D/A, D/P,
Supply Capacity:	5000 tons per month

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Zhonggong Special Metallurgy

Certification

ISO Certificate

Model Number

GH3030 alloy

Composition:

Nickel-based Superalloy Containing Chromium, Iron, And Nickel

Density:

8.08 G/cm³

Melting Point:

1370-1425°C (2498-2597°F)

Yield Strength (0.2% Offset):

700-900 MPa (at Room Temperature)

Elongation:

45-55%

Thermal Conductivity:

11.6 W/m·K (at 100°C)

Specific Heat Capacity:

424 J/kg·K (at 20°C)

Coefficient Of Thermal Expansion:

12.2 µm/m·K (20-100°C)

Electrical Resistivity:

1.15 µΩ·m (at 20°C)

1.15 µΩ·m (at 20°C):

Non-magnetic

Hardness:

HRB 95 (max)

Applications:

Gas Turbine Components, Aerospace Components, High-temperature Applications

Minimum Order Quantity:

100KG

Price:

Price is negotiated based on the required specifications and quantity

Packaging Details:

Standard export packaging, or packaging as required

Delivery Time:

5-8 working days, depending on the parameters required for negotiation

Payment Terms:

Payment Terms: Mainly T/T.. L/C, D/A, D/P,

Supply Ability:

5000 tons per month

Highlight

temperature resistant nickel based alloys

temperature resistant nickel based superalloy

aerospace components nickel based alloys

Product Description

Key Features:

High-Temperature Strength: GH3030 retains significant mechanical strength at elevated temperatures up to approximately 700°C (1300°F), making it suitable for applications in gas turbines, aerospace components, and high-temperature industrial environments.
Corrosion and Oxidation Resistance: The alloy exhibits excellent resistance to corrosion and oxidation in a wide range of aggressive environments, including aqueous and high-temperature gases.
Chemical Composition: GH3030 is composed primarily of nickel (about 52%), chromium (20-24%), iron (5-15%), and smaller amounts of niobium, titanium, and aluminum. This composition contributes to its superior mechanical and thermal properties.
Mechanical Properties: It offers high tensile and yield strength, with good ductility and toughness even after prolonged exposure to high temperatures.
Applications: Common applications include components for gas turbines, jet engines, aerospace parts, industrial furnaces, and high-temperature chemical processing equipment.
Processing and Fabrication: GH3030 can be processed using conventional methods such as forging, machining, and welding. Its weldability and formability allow for versatile manufacturing capabilities.
Non-Magnetic Properties: GH3030 is non-magnetic in the annealed condition, making it suitable for applications where magnetic interference must be minimized.

Here's a typical composition table for GH3030 alloy (Inconel Alloy 718):

Element	Composition (%)
Nickel (Ni)	Balance
Chromium (Cr)	19.0 - 21.0
Iron (Fe)	18.5 - 20.0
Niobium (Nb)	5.0 - 5.5
Molybdenum (Mo)	2.8 - 3.3
Titanium (Ti)	0.65 - 1.15
Aluminum (Al)	0.2 - 0.8
Cobalt (Co)	≤ 1.0
Manganese (Mn)	≤ 0.35
Silicon (Si)	≤ 0.35
Copper (Cu)	≤ 0.30
Carbon (C)	≤ 0.08
Sulfur (S)	≤ 0.015
Phosphorus (P)	≤ 0.015

GH3030 alloy - high-temperature resistant nickel-based superalloy 0

GH3030 alloy - high-temperature resistant nickel-based superalloy 1

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GH3030 alloy - high-temperature resistant nickel-based superalloy

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