Inconel 625 Explained

Inconel 625
Synonym:Werkstoff 2.4856
Type:Alloy
Uns:N06625
Alloy Type:Nickel-based superalloy
Specific Heat:0.096-0.160 BTU/(lb⋅°F)
(0.402-0.669 J/g⋅°C)
@
Permeability:1.006 @
Thermal Conductivity:50 BTU/(hr·ft⋅°F) @ – 175 BTU/(hr·ft⋅°F) @
Poissons Ratio:0.278-0.336 @ (annealed)
0.312-0.289 @ (solution treated)
Youngs Modulus:207.5-147.5 @ (annealed)
204.8-148.2 @ (solution treated)
Footnotes:Values displayed for tensile strength, elongation, and hardness are shown for various products under in size, and are measured at room temperature.
Tensile Strength:Rod, bar, plate: (as rolled), (annealed)
Elongation:Rod, bar, plate: 60-30% (as rolled and annealed)
Hardness Brinell:Rod, bar, plate: 175-240 (as rolled)

Inconel Alloy 625 (UNS designation N06625) is a nickel-based superalloy that possesses high strength properties and resistance to elevated temperatures. It also demonstrates remarkable protection against corrosion and oxidation. Its ability to withstand high stress and a wide range of temperatures, both in and out of water, as well as being able to resist corrosion while being exposed to highly acidic environments makes it a fitting choice for nuclear and marine applications.[1] [2] [3]

Inconel 625 was developed in the 1960s with the purpose of creating a material that could be used for steam-line piping. Some modifications were made to its original composition that have enabled it to be even more creep-resistant and weldable. Because of this, the uses of Inconel 625 have expanded into a wide range of industries such as the chemical processing industry, and for marine and nuclear applications to make pumps and valves and other high pressure equipment.[4]

Because of the metal's high Niobium (Nb) levels as well as its exposure to harsh environments and high temperatures, there was concern about the weldability of Inconel 625. Studies were therefore conducted to test the metal's weldability, tensile strength and creep resistance, and Inconel 625 was found to be an ideal choice for welding.[3] Other well known names for Inconel 625 are Haynes 625, Nickelvac 625, Nicrofer 6020, Altemp 625 and Chronic 625

Chemistry

Inconel 625 was designed as a solid solution strengthened material with no significant microstructure. This holds true at low and high temperatures, but there is a region (923 to 1148 K) where precipitates form that are detrimental to the creep properties, and thus the strength, of the alloy. Under any creep conditions (high temperature with an applied stress), M23C6-type carbides form at the grain boundaries. When tested at 973 K, γ” precipitates begin forming. These γ” phase precipitates are ordered A3 B type with a composition of Ni3(Nb, Al, Ti) and a tetragonal crystal structure. They form a disk-shaped morphology and are coherent with respect to the matrix. When tested at 998 K, a δ-phase precipitate begins forming which consist of Ni3(Nb, Mo) in an orthorhombic crystal structure. They form in a needle-like morphology and are incoherent with the matrix. Both of these precipitates can be completely dissolved back into the matrix when the sample is heated to 1148 K for 5 hours. This leads to the ability to recover creep properties of the alloy to prolong the materials lifetime.[5]

ASTM Specifications

ASTM (American Society for Testing and Materials) for various products made out of Inconel 625 are as follow:[6]

Markets

Markets for Inconel 625 include:

Applications

Product and technology applications of Inconel 625 include:[7]

Specifications

Specifications and certifications include:[8] [9]

See also

Notes and References

  1. Web site: Special Metals INCONEL® Alloy 625. ASM Aerospace Specification Metals Inc..
  2. Web site: High Temp Super Alloys. ASM Aerospace Specification Metals Inc..
  3. Book: Eiselstein . H.L. . Superalloys 718, 625 and Various Derivatives (1991) . Tillack . D.J. . TMS The Minerals, Metals and Materials Society . 1991 . 0-87339-173-X . 1–14 . The Invention and Definition of Alloy 625 . 10.7449/1991/Superalloys_1991_1_14.
  4. Book: Smith . G.D. . Superalloys 718, 625, 706 and Various Derivatives . Tillack . D.J. . Patel . S.J. . TMS The Minerals, Metals and Materials Society . 2001 . 0-87339-510-7 . 35–46 . Alloy 625 – Impressive Past/Significant Presence/Awesome Future . 10.7449/2001/Superalloys_2001_35_46.
  5. Mathew . M. D. . Microstructural changes in alloy 625 during high temperature creep . Materials Characterization . 59 . 5 . 2008 . 508–513. 10.1016/j.matchar.2007.03.007 .
  6. Web site: ASTM Specifications.
  7. Web site: Applications of Inconel 625.
  8. Web site: Alloy 625. Rickard.
  9. Web site: Inconel 625 Nickel Alloy . Service Steel Aerospace. 20 November 2020 .