Super Alloy Altemp 625™ (UNS N06625)

Topics Covered

Introduction
Chemical Composition
Physical Properties
Mechanical Properties
Other Designations
Fabrication and Heat Treatment
     Machinability
     Forming
     Welding
     Heat Treatment
     Forging
     Hot Working
     Cold Working
     Annealing
Applications

Introduction

Super alloys are also referred to as high performance alloys. They can function at high temperatures and mechanical stress, and are formed in different shapes. They are strengthened by work hardening, solid-solution hardening, and precipitation hardening. There are three groups of alloys, namely cobalt-based, nickel-based, and iron-based super alloys.

Altemp 625™ is a nickel-chromium-molybdenum wrought alloy. It has an ability to withstand stress-corrosion cracking and intergranular attack. The following sections with discuss about Altemp 625™ in detail.

Chemical Composition

The chemical composition of Altemp 625™ is displayed in the following table.

Element Content (%)
Nickel, Ni 60
Chromium, Cr 22
Molybdenum, Mo 9
Iron, Fe 4
Niobium, Nb 3.5
Titanium, Ti 0.3
Manganese, Mn 0.3
Aluminum, Al 0.3
Silicon, Si 0.25
Carbon, C 0.05
Sulfur, S 0.003
Phosphorous, P 0.01

Physical Properties

The physical properties of Altemp 625™ are highlighted in the following table.

Properties Metric Imperial
Density 8.44 g/cm³ 0.305 lb/in³
Melting point 1330°C 2425°F

Mechanical Properties

The following table shows the mechanical properties of Altemp 625™.

Properties Metric Imperial
Hardness, Rockwell B (typical annealed) 95 95
Tensile strength (for flat products (<4" thickness) and seamless tube and pipe) ≥ 827 MPa ≥ 120000 psi
Yield strength (for flat products (<4" thickness) and seamless tube and pipe) ≥ 414 MPa ≥ 60000 psi
Elongation at break (typical annealed) 45% 45%

Other Designations

Other designations that are equivalent to Altemp 625™ are included in the following table.

AMS 5581 AMS 5837 ASTM B443 ASTM B704 GE B50TF133
AMS 5599 AMS 5879 ASTM B444 ASTM B705 MIL E-21562 (RN625)
AMS 5666 ASTM B366 ASTM B446 DIN 2.4856  

Fabrication and Heat Treatment

Machinability

Altemp 625™ can be machined using conventional methods.

Forming

Altemp 625™ can be formed using conventional methods.

Welding

Altemp 625™ is welded using conventional methods.

Heat Treatment

Altemp 625™ is heat treated in the solution annealed condition at 1177°C (2150°F) for an adequate period of time depending on thickness of a section.

Forging

Altemp 625™ is forged at 1149 to 1177°C (2100 to 2150°F).

Hot Working

Altemp 625™ is hot worked at 1177°C (2150°F).

Cold Working

Cold working of Altemp 625™ is done using tooling and conventional methods

Annealing

Altemp 625™ is annealed at 983 to 1094°C (1800 to 2000°F) followed by cooling.

Applications

Altemp 625™ is suitable for high temperature applications such as gas turbine components and heat exchangers. It is also used in few acid process equipments and wet scrubbers due to its high corrosion resistance.

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