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Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel Based Superalloy With Iron

Minimum Order Quantity : 1000kg Price : negotiable
Packaging Details : In bundles in woode box Delivery Time : 6-8 weeks
Payment Terms : L/C, T/T Supply Ability : 200 tons per year
Place of Origin: China Brand Name: Torich
Certification: CE PED Model Number: Alloy Steel Pipe HastelloyX

Detail Information

Similar Grade: GH3536, GH536,GH22, GH334, GH739, SG-5, UNS N06002, NC22FeD, NiCr22FeMo, Nimonic PE13 Material: Hastelloy C
Application: Used In The Manufacture Of Aircraft Engine Combustion Chamber Components And Other High Temperature Components Density: 8.28g/cm³
Melting Temperature: 1295℃-1381℃
High Light:

alloy steel seamless tube

,

seamless alloy steel pipe

Product Description

Alloy Steel Pipe HastelloyX

 

Hastelloy X is a kind of nickel-based superalloy with high iron content, which is mainly solution strengthened by chromium and molybdenum solution strengthening. It has good resistance to oxidation and corrosion resistance. It has good cold & hot formability and weldability because its moderate lasting and creep strength under 900℃. Used in the manufacture of aircraft engine combustion chamber components and other high temperature components. It can be long-term used under 900℃, and short-term working temperature can up to 1080℃.

 

Similar Grade of Hastelloy X:  GH3536, GH536,GH22, GH334, GH739, SG-5, UNS N06002, NC22FeD, NiCr22FeMo, Nimonic PE13, Hastelloy H

 

Application for Hastelloy X: Used in the manufacture of aircraft engine combustion chamber components and other high temperature components

 

Chemical Composition of Hastelloy X:

 

Chemical Composition (%)
C Cr Ni Co W Mo Al Ti Fe B Cu Mn Si P S
0.05-0.15 20.5-23.0 Margin 0.50-2.50 0.20-1.00

8.0-

10.0

≤0.50 ≤0.15 17.0-20.0 ≤0.010 ≤0.5 ≤1.00 ≤1.00 ≤0.025 ≤0.015

 

Hastelloy X Physical Properties:

 

Hastelloy X Density: ρ: 8.28g/cm³

 

Hastelloy X Melting Temperature Rage: 1295℃-1381℃

 

Coefficient of Thermal Conductivity of Hastelloy X:

 

coefficient of thermal conductivity
Temperature
100 200 300 400 500 600 700 800 900
λ/(w/(m.℃)) 13.38 17.97 20.27 22.4 24.62 26.79 29.05 31.14

33.44

 

Specific Heat Capacity for Hastelloy X:

 

Specific Heat Capacity
Temperature
17 100 200 300 400 500 600 700 800 900
C/J/( kg · K ) 372.6 372.6 389.4 456.4 427.1 452.2 464.7 515 535.9 561

 

Expansion Coefficient for Hastelloy X:

 

expansion coefficient
Temperature/℃ 20-100 20-200 20-300 20-400 20-500 20-600 20-700 20-800 20-900
α1/10-6℃-1 12.1 12.5 13.4 14 14.3 14.8 15.5 15.8 16.1

 

Resistivity of Hastelloy X:

 

resistivity
Temperature/℃ 100 200 300 400 500 600 700 800 900
Resistor
Ω·m
1.18 1.2 1.21 1.22 1.24 1.25 1.26 1.27 1.29

 

 

Hastelloy X is widely used in aircraft engine and the civilian industry in adroad, and in our country, it mainly used in the manufacture of hot end of combustion chamber parts and other components, and honeycomb structure, etc. Besides, long-term used at high temperature will have certain age hardening phenomenon.

 

Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel Based Superalloy With Iron 0 Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel Based Superalloy With Iron 1

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