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.

Available Tube Product form

Typical Applications

• Wellhead components
• Sheathing
• Downhole equipment for corrosive/ sour service
• Reactor core
• Control rod components
• Gas pipeline control lines
• Heat exchangers
• Oil refining
• Chemical processing
• Control and instrumentation tubes

Industries predominantly using this Grade

Typical Manufacturing Specifications

• ASTM B444
• AMS
• BS
• Also individual customer specifications.

Technical Data

Mechanical Properties

Temper Annealed (Grade1) Solution-annealed (Grade 2) Tensile Rm 120 ksi (min) 100 ksi (min) Tensile Rm 827 MPa (min) 690 MPa (min) R.p. 0.2% Yield 60 ksi (min) 40 ksi (min) R.p. 0.2% Yield 414 MPa (min) 276 MPa (min) Elongation (2&#; or 4D gl) 30 % (min) 30 % (min)

Physical Properties (Room Temperature)

Specific Heat (0-100°C) 460 J.kg-1.°K-1 Thermal Conductivity 14.8 W.m -1.°K-1 Thermal Expansion 12.4 μm/μm/°C Modulus Elasticity 207 GPa Electrical Resistivity 10.3

Ohm-cm

HPE supply professional and honest service.

Density 8.42 g/cm3

Chemical Composition (% by weight)

Element Min Max C - 0.1 Si - 0.5 Mn - 0.5 P - 0.015 S - 0.015 Al - 0.4 Cr 20 23 Cu 1 1.4 Fe - 5 Mo 8 10 Nb 3.15 4.15 Ni Balance Ti - 0.4

Alloy 625 is a nickel-chromium-molybdenum alloy used for its high strength, excellent fabricability and outstanding corrosion resistance. Service temperatures can range from cryogenic to 980°C (°F). Alloy 625 strength is derived from the solid solution strengthening effect of molybdenum and niobium 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.

Alloy 625 (AMS) (UNS N)

Alloy 625, often referred to as Inconel 625 (where Inconel is a trademark of Special Metals Corp) is a nickel-chromium-molybdenum-niobium alloy (NiCr22Mo9Nb).

Continue reading this page to find out more about Alloy 625 from Langley Alloys.

 

What Is Alloy 625 Used For?

Alloy 625 is perfectly suited to the most demanding applications, from sub-zero to extremely high-temperature environments. It achieves these levels of high strength as a result of the solid solution effects of molybdenum and niobium (also known as Colombium) from room temperatures up to 800°C. Alloy 625 is usually supplied in the hot worked and annealed condition.

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Alloy 625 is particularly useful in situations where oxidation resistance and avoidance of pitting are required. In the annealed condition, this Inconel Alloy is fully austenitic and suitable for machining. It provides excellent corrosion resistance in a wide variety of severely corrosive environments due to its high alloy content. With nearly 60% nickel composition it is virtually immune from stress corrosion cracking.

Alloy 625 is non-magnetic and able to operate over a wide temperature range, from cryogenic temperatures up to 980degC. This supports applications in jet engines, heat exchangers, furnace hardware and chemical plant equipment.

Alloy 625 From Langley Alloys

Langley Alloys can supply Alloy 625 in a variety of different industry specifications. It is primarily offered as ASTM B446 for applications within the chemical process and Oil and Gas industries.

Langley Alloys carries an extensive stock of Alloy 625 from 0.5&#; (12.7mm) to 10&#; (254mm) diameter solid bars that meet ASTM B446 Grade 1 and Grade 2 plus SAE AMS requirements.

The most common specification is Alloy 625 Grade 1, although Langley Alloys are also able to offer Alloy 625 Grade 2 when required. For aerospace-related applications, we can also provide Alloy 625 in compliance with SAE AMS .

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