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GH4145 alloy is a high-strength nickel-based superalloy with excellent thermal stability and oxidation resistance

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GH4145 alloy is a high-strength nickel-based superalloy with excellent thermal stability and oxidation resistance

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

GH4145 alloy

Density:

~8.3 G/cm³

Melting Point:

~1390°C (2530°F)

Thermal Conductivity:

~11-12 W/m·K

Yield Strength:

~700 MPa (102 Ksi)

~700 MPa (102 Ksi):

900 MPa (130 Ksi)

Elongation:

Hardness (Rockwell):

~HRB 90-95

Applications:

Aerospace Components, Gas Turbines, And High-temperature Industrial Parts

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aerospace components nickel based alloys

aerospace components nickel based superalloy

Product Description

GH4145 Alloy

GH4145 is a high-performance nickel-based superalloy renowned for its exceptional strength, thermal stability, and resistance to oxidation and corrosion. It is designed for use in demanding high-temperature environments where reliability and durability are critical.

Key Features:

Composition: The alloy primarily consists of nickel, with substantial amounts of chromium, iron, and cobalt, alongside molybdenum, titanium, and aluminum. This composition provides a balance of mechanical strength, thermal stability, and corrosion resistance.
Temperature Resistance: GH4145 performs effectively at high temperatures up to approximately 1390°C (2530°F), maintaining its mechanical properties and structural integrity under extreme thermal conditions.
Mechanical Strength: It offers high yield and tensile strength, ensuring durability and performance under significant stress and load conditions.
Oxidation and Corrosion Resistance: The alloy is highly resistant to oxidation and high-temperature corrosion, which prolongs the life of components and minimizes maintenance needs.
Applications: GH4145 is commonly used in aerospace applications, including gas turbines, as well as in high-temperature industrial processes where its strength, stability, and resistance to harsh environments are essential.

GH4145 alloy’s superior combination of strength, thermal resistance, and corrosion protection makes it an ideal material for critical applications that require reliable performance in challenging conditions.

Here’s a detailed composition table for GH4145 alloy:

Element	Content Range
Nickel (Ni)	Balance
Chromium (Cr)	18.0-21.0%
Iron (Fe)	14.0-17.0%
Cobalt (Co)	8.0-10.0%
Molybdenum (Mo)	2.0-3.0%
Titanium (Ti)	1.5-2.5%
Aluminum (Al)	1.0-1.5%
Boron (B)	0.005-0.015%

This table provides a clear overview of the chemical composition of GH4145 alloy, detailing the content ranges of its key elements.

GH4145 alloy is a high-strength nickel-based superalloy with excellent thermal stability and oxidation resistance 0

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GH4145 alloy is a high-strength nickel-based superalloy with excellent thermal stability and oxidation resistance

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

GH4145 alloy

Density:

~8.3 G/cm³

Melting Point:

~1390°C (2530°F)

Thermal Conductivity:

~11-12 W/m·K

Yield Strength:

~700 MPa (102 Ksi)

~700 MPa (102 Ksi):

900 MPa (130 Ksi)

Elongation:

~10%

Hardness (Rockwell):

~HRB 90-95

Applications:

Aerospace Components, Gas Turbines, And High-temperature Industrial Parts

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

aerospace components nickel based alloys

aerospace components nickel based superalloy

Product Description

GH4145 Alloy

Key Features:

Composition: The alloy primarily consists of nickel, with substantial amounts of chromium, iron, and cobalt, alongside molybdenum, titanium, and aluminum. This composition provides a balance of mechanical strength, thermal stability, and corrosion resistance.
Temperature Resistance: GH4145 performs effectively at high temperatures up to approximately 1390°C (2530°F), maintaining its mechanical properties and structural integrity under extreme thermal conditions.
Mechanical Strength: It offers high yield and tensile strength, ensuring durability and performance under significant stress and load conditions.
Oxidation and Corrosion Resistance: The alloy is highly resistant to oxidation and high-temperature corrosion, which prolongs the life of components and minimizes maintenance needs.
Applications: GH4145 is commonly used in aerospace applications, including gas turbines, as well as in high-temperature industrial processes where its strength, stability, and resistance to harsh environments are essential.

Here’s a detailed composition table for GH4145 alloy:

Element	Content Range
Nickel (Ni)	Balance
Chromium (Cr)	18.0-21.0%
Iron (Fe)	14.0-17.0%
Cobalt (Co)	8.0-10.0%
Molybdenum (Mo)	2.0-3.0%
Titanium (Ti)	1.5-2.5%
Aluminum (Al)	1.0-1.5%
Boron (B)	0.005-0.015%

This table provides a clear overview of the chemical composition of GH4145 alloy, detailing the content ranges of its key elements.

GH4145 alloy is a high-strength nickel-based superalloy with excellent thermal stability and oxidation resistance 0

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