Hastelloy X Alloy , Nickel Chromium Molybdenum Alloy For Aerospace Components

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

Hastelloy X Is A High-Performance Nickel-Chromium-Molybdenum Alloy For High-Temp Applications

Hastelloy X Alloy is a high-performance nickel-chromium-molybdenum superalloy designed to deliver exceptional performance in extreme environments. This alloy is engineered to maintain its mechanical strength and structural integrity at temperatures up to 2200°F (1200°C), making it ideal for high-temperature applications such as gas turbines, jet engines, and industrial heat exchangers.

Key Properties and Features:

Temperature Resistance: Capable of withstanding extreme temperatures while retaining excellent strength and resistance to thermal degradation.
Corrosion Resistance: Offers superior resistance to oxidation, carburization, and sulfidation, ensuring longevity and reliability in harsh environments.
Mechanical Strength: Maintains high tensile and yield strength, coupled with excellent creep and fatigue resistance, under severe operational conditions.
Applications: Commonly used in aerospace components, high-temperature gas turbines, jet engines, and other critical industrial processes requiring robust high-temperature performance.
Stability: Provides consistent performance and dimensional stability, even in the most demanding applications, reducing the need for frequent maintenance or replacement.

Hastelloy X’s combination of strength, resistance to thermal and chemical degradation, and reliability makes it a preferred choice for high-stress, high-temperature applications where durability and long-term performance are essential

Here’s a general composition table for Hastelloy X Alloy:

Element	Composition Range (%)
Nickel (Ni)	47.0 - 52.0
Chromium (Cr)	19.0 - 21.0
Molybdenum (Mo)	8.0 - 9.5
Iron (Fe)	Balance
Cobalt (Co)	1.0 - 2.5
Titanium (Ti)	0.6 - 1.0
Aluminum (Al)	0.2 - 0.8
Carbon (C)	≤ 0.1
Manganese (Mn)	≤ 1.0
Silicon (Si)	≤ 0.5
Sulfur (S)	≤ 0.01

Please verify with specific standards or suppliers for precise values as they may vary slightly.

Hastelloy X Alloy , Nickel Chromium Molybdenum Alloy For Aerospace Components 0

Element

Composition Range (%)

Nickel (Ni)

47.0 - 52.0

Chromium (Cr)

19.0 - 21.0

Molybdenum (Mo)

8.0 - 9.5

Iron (Fe)

Balance

Cobalt (Co)

1.0 - 2.5

Titanium (Ti)

0.6 - 1.0

Aluminum (Al)

0.2 - 0.8

Carbon (C)

≤ 0.1

Manganese (Mn)

≤ 1.0

Silicon (Si)

≤ 0.5

Sulfur (S)

≤ 0.01

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Hastelloy X Alloy , Nickel Chromium Molybdenum Alloy For Aerospace Components