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Inconel 625 Flat Sheet/Plate Ideal for Aerospace, Marine & Chemical Processing
| Herkunftsort | China |
|---|---|
| Markenname | DELTA |
| Zertifizierung | ISO |
| Modellnummer | Inkonel 625 |
| Min Bestellmenge | 500 kg |
| Preis | 22 - 30 USD/Kg |
| Verpackung Informationen | Standardverpackung für den Exportieren |
| Lieferzeit | 5 - 12 Tage basierend auf der Menge |
| Zahlungsbedingungen | L/C, T/T, Western Union |
| Versorgungsmaterial-Fähigkeit | 3 Tonnen pro Woche |
Treten Sie mit mir für freie Proben und Kupons in Verbindung.
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x| Produkte | Nickel-Legierungs-Blatt u. Platte | Grad | Inkonel 625 |
|---|---|---|---|
| Dicke | 0.5 - 30.0mm | Standardgröße | 1000*2000mm 1219*2438mm |
| Standard | ASTM EN | Service | Schneiden |
| Ladehafen | Shanghai Hafen | Oberfläche | 2B Nein.1 |
Inconel 625 Flat Sheet/Plate Ideal for Aerospace, Marine & Chemical Processing
Products Specification
| Products Name | Inconel 625 Nickel Alloy Sheet Plate |
| Thickness | Cold rolled: 0.5 - 3.0mm Hot rolled 4.0 - 30.0mm |
| Standard Size | 1000*2000mm 1219*2438mm 1219*3048mm 1500*6000mm |
| Surface | 2B NO.1 |
| MOQ | 50 kgs |
| Service | Cutting, Surface Finishing |
| Packing | Waterproof paper and wooden pallets |
| Loading Port | Shanghai Port |
| Price term | FOB CFR CIF EXW |
| Payment term | 30% TT in advance , 70% TT balance against copy of B/L |
| Main Grade | Hastelloy C22 C4 X C276 G35 |
| Monel 400 K500 | |
| Incoloy 800 800H 800HT 825 925 | |
| Inconel 600 601 617 625 716 718 | |
| Stainless Steel Grade | 201 202 301 304L 309S 310S 316L 316Ti 317L 321 347 409L 410 410S 420J1 420J2 430 431 436L 439 440A/B/C 441 443 444 2205 2507 904L 254SMO 253MA |
Inconel 625 Flat Sheet/Plate Ideal for Aerospace, Marine & Chemical Processing
Key Chemical Composition of Inconel 625 Flat Sheet/Plate
|
Element
|
Content Range (%)
|
Key Function
|
|---|---|---|
|
Nickel (Ni)
|
≥58.0
|
Forms stable austenitic matrix; ensures cryogenic toughness
|
|
Chromium (Cr)
|
20.0-23.0
|
Creates protective oxide film; resists oxidation and scaling
|
|
Molybdenum (Mo)
|
8.0-10.0
|
Enhances pitting/crevice corrosion resistance; boosts strength
|
|
Niobium (Nb) + Tantalum (Ta)
|
3.15-4.15
|
Solid-solution strengthening; improves high-temperature creep resistance
|
|
Iron (Fe)
|
≤5.0
|
Minor alloying element; aids in processing
|
|
Cobalt (Co)
|
≤1.0
|
Impurity control; maintains alloy stability
|
|
Carbon (C)
|
≤0.10
|
Prevents carbide precipitation; ensures weldability
|
|
Manganese (Mn) / Silicon (Si)
|
≤0.50 each
|
Deoxidizers; support manufacturing processes
|
|
Phosphorus (P) / Sulfur (S)
|
≤0.015 each
|
Impurity limits; avoid intergranular corrosion and brittleness
|
Critical Physical & Mechanical Properties
|
Property
|
Value
|
Test Condition
|
|---|---|---|
|
Density
|
8.44 g/cm³
|
Room temperature
|
|
Melting Range
|
1290-1350°C (2354-2462°F)
|
—
|
|
Thermal Expansion Coefficient
|
13.1-13.4×10⁻⁶/°C
|
20-1000°C
|
|
Thermal Conductivity
|
9.8 W/(m·K)
|
Room temperature
|
|
Tensile Strength
|
≥760 MPa (110 ksi)
|
Room temperature, annealed
|
|
Yield Strength (0.2% offset)
|
≥345 MPa (50 ksi)
|
Room temperature, annealed
|
|
Elongation
|
≥30%
|
Room temperature, annealed
|
|
Brinell Hardness
|
≤220 HB
|
Room temperature
|
|
Tensile Strength (Retained)
|
≥550 MPa
|
600°C (1112°F)
|
|
Oxidation Resistance
|
≤0.025 mm/year
|
1000°C (1832°F)
|
Unmatched Corrosion Resistance
Industry-Specific Applications
Aerospace & Aviation
Marine & Offshore Engineering

