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625

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AVAILABILITY

SPECS

Welded Pipe 1/2" –8"

B444, B705

Butt-Weld Fittings 1/2" – 8"

B366

Flanges 1/2" – 8"

B444, B564, B16.5

Bar 1" – 6"

B446, B564

Forgings

B564

 

CHEMICAL COMPOSITION %

C

Cr

Fe

Ni

Al

Ti

Cb + TA

MAX

 

MAX

MIN

MAX

MAX

 

0.10

20.0-23.0

5.0

58.0

0.40

0.40

3.15-4.15

DESCRIPTION

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 molybdenum 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.

DESIGN FEATURES

  • 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.

TYPICAL APPLICATIONS

  • 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 braze-ability make it a good choice in the aerospace industry

TENSILE REQUIREMENTS

Tensile Strength
(KSI)
120

Yield Strength
(KSI)
60

KSI can be converted to MPA (Megapascals) by multiplying by 6.895.

MultAlloy stocks 321 with high carbon to meet 321/321H specifications.

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