USD1000.00 - USD4000.00
- Place of Origin:CN;ZHE
- Grade:1Cr13Mn9Ni1N
- Thickness:1 - 50 mm
- Outer Diameter(Round):6 - 420 mm
- Grade Group:CrNi alloy
- Secondary Or Not:Non-secondary
- Technique:Cold Drawn
- Application:Structure Pipe
- Standard2:ASTM A312M-2007
- Section Shape:Round
- Standard:ASTM
- Alloy Or Not:Is Alloy
- Surface Treatment:oil
- Certification:ISO
- Special Pipe:Alloy steel pipes
- Product name:Aircraft Engine Hastelloy X Alloy Steel Pipe
- Keywords:Hastelloy X Alloy Steel Pipe
- Brand Name:Torich
- Model Number:ASTM A312
- Type:SMLS
- Length:1-12m
- End protector:Plain
- Shape:Round Shape
- Usage:Aircraft Engine
- MTC:En10204.3.2B
Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel - Based Superalloy With Iron
Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel - Based Superalloy With Iron
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℃
Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel - Based Superalloy With Iron
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
Detailed Images
QUALITY CONTROL
1~ Incoming Raw Material Inspection
2~ Raw Material Segregation to avoid steel grade mix-up
3~ Heating and Hammering End for Cold Drawing
4~ Cold Drawing and Cold Rolling, on line inspection
5~ Heat Treatment, +A, +SRA, +LC, +N, Q+T
6~ Straightening-Cutting to specified length-Finished Measuring Inspection
7~ Machanical Testing in own labs with Tensile Strength, Yield Strength, Elongation, Hardness, Impact, Mictrostruture etc
8~ Packing and Stocking.
Q: Are you trading company or manufacturer ?
A: A professional steel pipes materials inventor, manufacturer and solution provider
Q: How long is your delivery time?
A: Generally it is 7-14 days if the goods are in stock. or it is 30-60 days if the goods are not in stock, it is according to quantity.
Q: Do you provide samples ? is it free or extra ?
A: Yes, we could offer the sample of Aircraft Engine Hastelloy X Alloy Steel Pipe Nickel - Based Superalloy With Iron for free charge but need pay the cost of freight.
Q: What is your terms of payment ?
A: Payment<=1000USD, 100% in advance. Payment>=1000USD, 30% T/T in advance ,balance before shippment.
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