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Alloy 617

UNS N06617

Description

617
NICKEL ALLOY

Alloy 617 is a solid-solution, nickel-chromium-cobalt-molybdenum alloy with an exceptional combination of metallurgical stability, strength, and oxidation resistance at high temperatures. The enhanced oxidation resistance is attributed to the aluminium in conjunction with the chromium. It also has excellent resistance to a variety of both reducing and oxidizing media due to the high nickel and chromium contents. And those elements with the molybdenum enable the alloy to withstand many wet corrosive environments. Alloy 617 is an excellent choice for high temperature applications in various industries such as aerospace and power generation markets, and petrochemical plants.

Chemical Component

Ni CrMoCoCuFeAlCTiMnSiSB
44.5% min20-24%8-10%10-15%0-0.5%0-3%0.8-1.5%0.05-0.15%0-0.6%0-1%0-1%0-0.015%0-0.006%

Basic Information

ItemsAlloy 617
CatalogACMA-Ni-A011
Density8.36 g/cm3
Electrical Resistivity1.22 µΩ.m
Specific Heat Capacity419 J/kg.°C
Poisson's Ratio0.3
Hardness172 HRB
Melting Range1332-1380 °C

Material Forms

Alfa Chemistry offers Alloy 617 in a variety of forms, including Sheet & Plate, Welding Wire, etc.

Mechanical & Physical Properties

Properties21.1 °C93.3 °C148.9 °C204.4 °C315.6 °C371.1 °C426.7 °C537.8 °C595 °C648.9 °C760 °C870 °C982 °C1093 °C
Ultimate Tensile Strength, Mpa734706669647628625624595-570--496-
0.2% Yield Strength, Mpa322301276258250248244246-260--109-
Reduction of area, %5650------------
Elongation, %6260595961626363-60--72-
Minimum Creep 0.0001% per hr--------344.73275.799027.5812.45.51
10,000 hr Rupture Strength--------344.73275.79120.6539.3615.75.51
Coefficient of Thermal Expansion, µm/m°C-11.611.612.613.113.613.613.9-14--16.3-
Thermal Conductivity, kcal/(hr.m.°C)11.52412.64212.64214.01815.2216.59816.59817.974-19.35--24.682-
Modulus of Elasticity, GPa211206206201194188188181-173--129-

Specifications

Sheet & Plate, Welding Wire: ASTM B166, B168, B546, B564, AMS 5887, 5888, 5889

Applications

Alloy 617 can be used in a variety of applications, including:

  • Combustion cans and ducting for aircraft and land-based gas turbines
  • Transition liners aircraft and land-based gas turbines
  • Industrial furnace components
  • Nitric acid catalyst grids
  • Casing for industrial aircraft and land-based gas turbines

* Technical data included herein should be used as a guideline only, and should not be construed as maximum or minimum values for specification or for final design, or for a particular use or application. The data may be revised anytime without notice.

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