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Home > Metallurgy, Mineral & Energy > Steel & Products > Steel Pipe & Tube > EU General Nickel Alloy Incoloy 825 (UNS N08825, Incoloy825)
EU General Nickel Alloy Incoloy 825 (UNS N08825, Incoloy825)
Negotiable
MOQ: 1 Ton (Price negotiable depending on order volume and customization)
Key Specifications
Get Latest Price
Type:
Seamless
Technique:
Cold Rolled
Surface Treatment:
Other
Payment & Shipping
Payment Methods:
Port of Shipment:
China
Delivery Detail:
8 days
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Type
Seamless
Technique
Cold Rolled
Surface Treatment
Other
Material
Stainless steel
Section Shape
Round
Basic Info.
Model NO.
incoloy 800 800h 800ht
Purity
30-46%
Alloy
Alloy
Type
Nickel Bar
Powder
Not Powder
Grade
Incoloy 800 800h 800ht 825 925
MOQ
20kg
Surface
Bright, Oxidized Color, Acid White
Density
8.19 G/Cm³
Dilatation Coefficient
13.0 μm/M °c
Melting Point
1336
Treatment
Hydrogen Annealing
Elongation
30%~46%
Ultimate Strength
462MPa
Types
Wire Sheet Bar Plate Foil Pipe
Transport Package
Spool+Carton Box
Specification
Customized
Trademark
DLX
Origin
Changzhou, Jiangsu, China
HS Code
7507120000
Production Capacity
1000kg Per Week
Product Description
ASTM AMSE B408 825 Flat Bar Incoloy 800 Incoloy 800h Incoloy 800 Ht Incoloy825 Inconel 600 Uns N08825 Rounds Rods
Incoloy Alloy is characterised by high temperature resistance combined with excellent corrosion resistance. it has excellent corrossion resistance, high strength, easy to fabricate. It can be found in a wide range of product forms across many industries.
| Item | Incoloy 800 | Incoloy 800H | Incoloy 800HT | Incoloy 825 | Incoloy 925 |
| C | ≤0.1 | 0.05 - 0.1 | 0.06 - 0.1 | ≤0.05 | ≤0.03 |
| Mn | ≤1.5 | ≤1.5 | ≤1.5 | ≤1 | ≤1 |
| Fe | rest | rest | rest | rest | rest |
| P | - | - | - | ≤0.02 | ≤0.03 |
| S | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.03 | ≤0.03 |
| Si | ≤1 | ≤1 | ≤1 | ≤0.5 | ≤0.5 |
| Cu | ≤0.75 | ≤0.75 | ≤0.75 | 1.5 - 3 | 1.5 - 3 |
| Ni | 30 - 35 | 30 - 35 | 30 - 35 | 38 - 46 | 42 - 46 |
| Al | 0.15 - 0.6 | 0.15 - 0.6 | 0.15 - 0.6 | 0.2 - 1.2 | 0.15 - 0.5 |
| Ti | 0.15 - 0.6 | 0.15 - 0.6 | 0.15 - 0.6 | 0.6 - 1.2 | 1.9 -2.4 |
| Cr | 19 - 23 | 19 - 23 | 19 - 23 | 19.5 - 23.5 | 19.5 - 23.5 |
| Mo | - | - | - | 2.5 - 3.5 | 2.5 - 3.5 |
Inconel alloys are oxidation corrion resistance materials well suited for service in extreme environments subjects to pressure and
heat.When heated,Inconel forms a rhick,stable,passivating oxide layer protecting the surface from further attack.Inconel retains
strength over a wide temperature range,attrative for high temperature applications where aluminum and steel would succumb to creap as a result of thermally induced crystal vacancies.Inconel's high temperature strength is developed by solid solution
strengthening or precipitation hardening,depending on the alloy.
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 718's composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy's matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Application field:
High temperature components, such as turbine blades, guide vanes, turbine disks, high pressure compressor disks,machine manufacturing and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines.
High temperature components, such as turbine blades, guide vanes, turbine disks, high pressure compressor disks,machine manufacturing and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines.
| Item | Inconel 600 | Inconel | Inconel 617 | Inconel 625 | Inconel | Inconel | Inconel | Inconel |
| 601 | 690 | 718 | X750 | 825 | ||||
| C | ≤0.15 | ≤0.1 | 0.05-0.15 | ≤0.08 | ≤0.05 | ≤0.08 | ≤0.08 | ≤0.05 |
| Mn | ≤1 | ≤1.5 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.35 | ≤1 | ≤1 |
| Fe | 6~10 | rest | ≤3 | rest | 7~11 | rest | 5~9 | ≥22 |
| P | ≤0.015 | ≤0.02 | ≤0.015 | -- | -- | -- | -- | -- |
| S | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.01 | ≤0.01 | ≤0.03 |
| Si | ≤0.5 | ≤0.5 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.5 |
| Cu | ≤0.5 | ≤1 | -- | ≤0.3 | ≤0.5 | ≤0.3 | ≤0.5 | 1.5-3 |
| Ni | ≥7.2 | 58-63 | ≥44.5 | 50-55 | ≥58 | 50-55 | ≥70 | 38-46 |
| Co | -- | -- | 10~15 | ≤10 | -- | ≤1 | ≤1 | -- |
| Al | -- | 1-1.7 | 0.8-1.5 | ≤0.8 | -- | 0.2-0.8 | 0.4-1 | ≤0.2 |
| Ti | -- | -- | ≤0.6 | ≤1.15 | -- | -- | 2.25-2.75 | 0.6-1.2 |
| Cr | 14-17 | 21-25 | 20-24 | 17-21 | 27-31 | 17-21 | 14-17 | 19.5-23.5 |
| Nb+Ta | -- | -- | -- | 4.75-5.5 | -- | 4.75-5.5 | 0.7-1.2 | -- |
| Mo | -- | -- | 8~10 | 2.8-3.3 | -- | 2.8-3.3 | -- | 2.5-3.5 |
| B | -- | -- | ≤0.006 | -- | -- | -- | -- | -- |
Send Inquiry to This Supplier
2Yrs
Main Markets
North America, South America, Eastern Europe, Southeast Asia, Africa, Oceania, Mid East, Eastern Asia, Western Europe, Central America, Northern Europe, Southern Europe, South Asia, Domestic Market
Location
Tianjin, China
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