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コンタクトパーソン : Roy
電話番号 : +86 18930254719
ワットスアップ : +8618930254719

Nickel Based Weldig Wire W. Nr. 2.4856 Uns No6625 (Inconel alloy 625)

Place of Origin CHINA
ブランド名 HUONA
証明 ISO9001
Model Number Inconel 625
Minimum Order Quantity 10KG
価格 DISCUSS
Packaging Details Carton or Wooden Case
Delivery Time 7-21 DAYS
Payment Terms L/C,T/T,Western Union,MoneyGram
Supply Ability 1000kg Per Week

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商品の詳細
Model NO. Inconel 625 Condition Soft Annealed
Purity >98% Surface Bright
Certificate ISO9001,ROHS Trademark HUONA
Type Wire
ハイライト

Inconel alloy 625 welding wire

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Nickel based alloy 2.4856 wire

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UNS No6625 welding wire with warranty

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製品の説明
Nickel Based Welding Wire W. Nr. 2.4856 Uns No6625 (Inconel Alloy 625)
Product Specifications
Attribute Value
Model NO. Inconel 625
Condition Soft Annealed
Purity >98%
Surface Bright
Certificate ISO9001, ROHS
Trademark HUONA
Type Wire
Product Description

Inconel 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
  • Combustion chambers used in the manufacture of aviation, naval and industrial gas turbines
Material Composition Comparison
Item Inconel 600 Inconel 601 Inconel 617 Inconel 625 Inconel 690 Inconel 718 Inconel X750 Inconel 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 -- -- -- -- --
Physical Properties
Density 8.40 g/cm³
Ultimate Strength (≥ MPa) 700
Tensile Strength σb/MPa 760
Elongation δ5 (%) 30
Yield Strength σp0.2/MPa 345
Melting point 1290-1350°C