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Nickel alloys
Alloy 625

Ni-Cr-Mo-Nb alloy (Inconel 625)

STANDARDASTM B446 / B443FORMBar, plate, forgingUNSN06625Material no.2.4856

Nickel-chromium alloy strengthened with molybdenum and niobium. Strength from cryogenic temperatures up to 980 °C and very high resistance in seawater and acids; also used as a weld overlay (cladding) material for valve seats and stems.

Rp0.2 · MPa
—
Rm · MPa
—
TEMPERATURE
−196 … +982 °C
COST
Representative sample of Alloy 625: machined top face and rolled side
REPRESENTATIVE IMAGE

Chemical composition

The values in this section are being verified.

Mechanical properties

The values in this section are being verified.

Service temperature

This is the limit of the material itself. A valve's service temperature is usually set by the seal and seat materials; product pages give it for each seal option.

Media suitability GENERAL TREND

Fresh water
Seawater
Steam
Hydrocarbons, oil
Dilute acid
Caustic
Air, gas
Low temperature

Emsal assessment. The final choice is made from corrosion tables, taking concentration, temperature, chloride content and flow velocity into account.

Strengths and weaknesses

Strengths

  • Very high resistance to pitting and crevice corrosion in seawater
  • Strength and oxidation resistance at high temperature
  • Ideal for weld overlay (cladding)

Weaknesses

  • Very expensive
  • Difficult to machine

Manufacturing and use

ECONOMY
Very high.
MANUFACTURING METHODS
Fabrication from bar and forging · Weld overlay cladding
TYPICAL VALVE PARTS
Stem · Seat overlay · Body (extremely corrosive service)

Source: ASTM B446 / B443. Values compiled and verified by Emsal Vana; for binding values, refer to the current edition of the standard and the material certificate.