Alloy 625
UNS N06625
Availability
- Welded Pipe 1/2″ – 8″
- Butt-Weld Fittings 1/2″ – 8″
- Flanges 1/2″ – 8″
- Bar 1″ – 4-1/2″
Specifications
- ASTM B443, B705, B366, B446, B564
- ASME SB443, SB705, SB366, SB446, SB564
Chemical Composition
| C | Cr | Fe | Ni | Al | Ti | Co + TA |
|---|---|---|---|---|---|---|
| Max | - | Max | Min | Max | Max | - |
| 0.10 | 20.0 – 23.0 | 5.0 | 58.0 | 0.40 | 0.40 | 3.15 – 4.15 |
Alloy 625 is a Nickel-Chromium alloy used for its high strength, excellent fabricability and outstanding corrosion resistance. Service temperatures range from cryogenic to 1800 ̊ F. Alloy 625 strength is derived from the stiffening effect of molybdenium and columbium on its Nickel-Chromium matrix; thus precipitation-hardening treatments are not required. This combination of elements also is responsible for superior resistance to a wide range of corrosive environments of unusual severity as well as to high-temperature effects such as oxidation and carburization.
- Outstanding resistance to pitting, crevice corrosion, impingement corrosion and intergranular attack.
- Almost complete freedom from Chloride- induced stress corrosion cracking.
- Good resistance to mineral acids, such as nitric, phosphoric, sulphuric and hydrochloric acids.
- Good resistance to alkalis and organic acids.
- Good mechanical properties.
- Used for structures in contact with seawater and subject to high mechanical stresses
- Flue gas scrubbers components
- Chimney linings
- Superphosphoric acid production equipment
- Sour gas production tubes
- Offshore industry, marine equipment
- High tensile, creep, rupture strength, outstanding fatigue and thermal-fatigue strength; oxidation resistance; and excellent weldability and brazeability make it a good choice in the aerospace industry
Tensile Strength
(KSI)
120
(KSI)
120
Yield Strength
(KSI)
60
(KSI)
60
KSI can be converted to MPA (Megapascals) by multiplying by 6.895.
