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Anti Fatigue Nimonic 115 Rod For Demanding High Temperature Environments

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Anti Fatigue Nimonic 115 Rod For Demanding High Temperature Environments

MOQ:	150kgs
Price:	Negotiatable
Standard Packaging:	Wood box
Delivery Period:	2-30days
Payment Method:	L/C,D/A,D/P,T/T,Western Union,MoneyGram
Supply Capacity:	300 Ton per Month

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

NikTech

Certification

ISO 9001:2008

Model Number

Nimonic 115

Features:

Anti-oxidation And Anti-fatigue

Width:

Customized

Thickness Tolerance:

±0.01mm

Diameter:

0.1-200mm

Thermal Conductivity:

10.6 W/m-°C (20°C)

Cost:

Expensive

Specific Heat:

444J/kg•°C

Origin:

Jiangsu

Alloy Type:

Nickel-chrome-Cobalt Alloy

Hardness:

Modulus Of Elasticity:

188 GPa

Surface Treatment:

2B Or According To Customer Requirement

Creep Resistance:

Excellent

Electrical Resistivity:

139 µΩ Cm (20°C)

Coefficient Of Expansion:

12.0 10-6 / °C

Standard:

W. Nr. 2.4636

Highlight:

Anti Fatigue nimonic 115

200mm nimonic 115

0.1mm high temperature steel alloys

Product Description

Nimonic 115 Rod: High-Temperature Performance and Oxidation Resistance

Nimonic 115 is a nickel-chromium-cobalt-based superalloy, strengthened with additions of molybdenum, aluminum, and titanium. Developed for high-temperature applications, it maintains excellent mechanical properties and oxidation resistance up to approximately 1010°C. Originally designed for turbine blades in aircraft gas turbines, Nimonic 115 is now utilized in various demanding environments.

Chemical Composition

The chemical composition of Nimonic 115 is as follows:

Element	Content (%)
Nickel (Ni)	Balance*
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	13.0 - 15.5
Aluminum (Al)	4.5 - 5.5
Molybdenum (Mo)	3.0 - 5.0
Titanium (Ti)	3.5 - 4.5
Iron (Fe)	≤1.0
Manganese (Mn)	≤1.0
Silicon (Si)	≤1.0
Copper (Cu)	≤0.2
Zirconium (Zr)	≤0.15
Carbon (C)	0.12 - 0.20
Sulfur (S)	≤0.015
Boron (B)	0.01 - 0.025

*Balance indicates that nickel is the predominant element, with other elements present in minimal quantities. *

Mechanical Properties

In its precipitation-hardened condition, Nimonic 115 exhibits the following mechanical properties:

Property	Metric	Imperial
Tensile Strength	1300 MPa	189,000 psi
Yield Strength	850 MPa	123,000 psi
Elongation at Break	25%	25%

Physical Properties

The physical properties of Nimonic 115 include:

Property	Metric
Density	7.85 g/cm³
Melting Point	1260-1315°C
Coefficient of Thermal Expansion (20–100°C)	12.0 x 10⁻⁶/°C
Thermal Conductivity (20°C)	10.6 W/m·°C

Applications

Nimonic 115 is widely used in applications requiring high-temperature strength and oxidation resistance, including:

Gas Turbine Components: Turbine blades, vanes, and seals operating at elevated temperatures.
Aerospace Industry: Components subjected to high thermal stresses, such as afterburners and exhaust systems.
Power Generation: Parts exposed to high-temperature gases, like combustion chambers and heat exchangers.
Petrochemical Processing: Equipment facing corrosive and high-temperature environments, such as reactor cores and piping.

Frequently Asked Questions

Q1: What is the maximum operating temperature for Nimonic 115?

Nimonic 115 is designed for continuous service at temperatures up to 1010°C (1850°F), maintaining its mechanical integrity and oxidation resistance.

Q2: How does Nimonic 115 compare to other superalloys like Nimonic 90 and Nimonic 105?

While all these alloys are nickel-based superalloys suitable for high-temperature applications, Nimonic 115 offers a balanced combination of strength and oxidation resistance. Nimonic 90 provides higher strength at the expense of some ductility, and Nimonic 105 offers improved oxidation resistance but may have lower strength compared to Nimonic 115.

Q3: What are the heat treatment processes for Nimonic 115?

The recommended heat treatment for Nimonic 115 involves solution treatment followed by aging:

Solution annealing at 1190°C (2174°F) for 1.5 hours, followed by air cooling.
Aging at 1100°C (2012°F) for 6 hours, followed by air cooling.

Q4: Are there equivalent materials to Nimonic 115?

Yes, equivalent materials include British Standard BSHR4 and German Standard DIN 2.4636.

Conclusion

Nimonic 115 rods are engineered to perform under extreme conditions, offering exceptional high-temperature strength and oxidation resistance. Their unique combination of properties makes them ideal for demanding applications in aerospace, power generation, and petrochemical industries.

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Anti Fatigue Nimonic 115 Rod For Demanding High Temperature Environments

MOQ:	150kgs
Price:	Negotiatable
Standard Packaging:	Wood box
Delivery Period:	2-30days
Payment Method:	L/C,D/A,D/P,T/T,Western Union,MoneyGram
Supply Capacity:	300 Ton per Month

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

NikTech

Certification

ISO 9001:2008

Model Number

Nimonic 115

Features:

Anti-oxidation And Anti-fatigue

Width:

Customized

Thickness Tolerance:

±0.01mm

Diameter:

0.1-200mm

Thermal Conductivity:

10.6 W/m-°C (20°C)

Cost:

Expensive

Specific Heat:

444J/kg•°C

Origin:

Jiangsu

Alloy Type:

Nickel-chrome-Cobalt Alloy

Hardness:

High

Modulus Of Elasticity:

188 GPa

Surface Treatment:

2B Or According To Customer Requirement

Creep Resistance:

Excellent

Electrical Resistivity:

139 µΩ Cm (20°C)

Coefficient Of Expansion:

12.0 10-6 / °C

Standard:

W. Nr. 2.4636

Minimum Order Quantity:

150kgs

Price:

Negotiatable

Packaging Details:

Wood box

Delivery Time:

2-30days

Payment Terms:

L/C,D/A,D/P,T/T,Western Union,MoneyGram

Supply Ability:

300 Ton per Month

Highlight

Anti Fatigue nimonic 115

200mm nimonic 115

0.1mm high temperature steel alloys

Product Description

Nimonic 115 Rod: High-Temperature Performance and Oxidation Resistance

Chemical Composition

The chemical composition of Nimonic 115 is as follows:

Element	Content (%)
Nickel (Ni)	Balance*
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	13.0 - 15.5
Aluminum (Al)	4.5 - 5.5
Molybdenum (Mo)	3.0 - 5.0
Titanium (Ti)	3.5 - 4.5
Iron (Fe)	≤1.0
Manganese (Mn)	≤1.0
Silicon (Si)	≤1.0
Copper (Cu)	≤0.2
Zirconium (Zr)	≤0.15
Carbon (C)	0.12 - 0.20
Sulfur (S)	≤0.015
Boron (B)	0.01 - 0.025

*Balance indicates that nickel is the predominant element, with other elements present in minimal quantities. *

Mechanical Properties

In its precipitation-hardened condition, Nimonic 115 exhibits the following mechanical properties:

Property	Metric	Imperial
Tensile Strength	1300 MPa	189,000 psi
Yield Strength	850 MPa	123,000 psi
Elongation at Break	25%	25%

Physical Properties

The physical properties of Nimonic 115 include:

Property	Metric
Density	7.85 g/cm³
Melting Point	1260-1315°C
Coefficient of Thermal Expansion (20–100°C)	12.0 x 10⁻⁶/°C
Thermal Conductivity (20°C)	10.6 W/m·°C

Applications

Nimonic 115 is widely used in applications requiring high-temperature strength and oxidation resistance, including:

Gas Turbine Components: Turbine blades, vanes, and seals operating at elevated temperatures.
Aerospace Industry: Components subjected to high thermal stresses, such as afterburners and exhaust systems.
Power Generation: Parts exposed to high-temperature gases, like combustion chambers and heat exchangers.
Petrochemical Processing: Equipment facing corrosive and high-temperature environments, such as reactor cores and piping.

Frequently Asked Questions

Q1: What is the maximum operating temperature for Nimonic 115?

Nimonic 115 is designed for continuous service at temperatures up to 1010°C (1850°F), maintaining its mechanical integrity and oxidation resistance.

Q2: How does Nimonic 115 compare to other superalloys like Nimonic 90 and Nimonic 105?

Q3: What are the heat treatment processes for Nimonic 115?

The recommended heat treatment for Nimonic 115 involves solution treatment followed by aging:

Solution annealing at 1190°C (2174°F) for 1.5 hours, followed by air cooling.
Aging at 1100°C (2012°F) for 6 hours, followed by air cooling.

Q4: Are there equivalent materials to Nimonic 115?

Yes, equivalent materials include British Standard BSHR4 and German Standard DIN 2.4636.

Conclusion

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