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GH600 Wrought Superalloy
Overview of GH600 Wrought Superalloy
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GH600 alloy is a nickel-chromium-iron alloy with good resistance to corrosion and oxidation. It is a solid-solution alloy that can be hardened only by cold working and it has excellent mechanical properties with a desirable combination of high strength and good workability. Similar alloy's names in different standards:

Beiye designation

China Standard designation

America designation

GH600

GH600

Inconel 600



rhenium superalloy

The Typical Applications of This Alloy are

  • Furnace muffles

  • Electronic components

  • Heat-exchanger tubing

  • Chemical and food processing equipment

  • Fixtures and rotors

  • Reactor control rods

  • Nuclear reactors

  • Springs

  • Primary water piping


Typical Chemical Composition in Percent


C

0.03

Cr

15.50

Fe

8.00

Ni

bal.



Typical Mechanical Properties


Soft

Hard

Hardness

146 HV

314 HV

Yield Strength

380 MPa (55.15 ksi)

761 MPa (110.5 ksi)

Tensile Strength

718 MPa (104.21 ksi)

1013 MPa (147 ksi)

Elongation

43.5%

17.5%

* Typical values for material tested in accordance with GB/T 4340.3, GB/T 228, GB/T 22315.


Typical Physical Properties


Density

8.43 g/cm3 (0.304b/in3)

Melting Point

1400 ℃ (2552oF)

Curie temperature (annealed material)

-124 ℃ (-192oF)

Modulus of elasticity (21℃,Tension)

206.7GPa(30×103ksi)

(21℃,Torsion)

75.8GPa(11×103ksi)

Poisson's rato (21℃)

0.29



Heat Treatment

This solid-solution alloy can be hardened only by cold working and not by any heat treatment. Its behavior during heating is governed by a number of interacting variables: amount of cold work, grain size, chemical composition, and dimensions of the material. Consequently, times and temperatures for heat treatment are usually experimentally determined.

In-process annealing: To relieve all strains and restore the alloy to a soft condition suitable for further cold rolling or drawing, forming, bending or similar operations, anneal at 1050~1080℃ for not more than 1 hour. Since the high nickel, high permeability alloys readily absorb carbon, sulfur, oxygen and other contaminants from combustion furnace gasses, in-process annealing should be conducted in dissociated ammonia, hydrogen, vacuum or inert gas atmospheres.

Final annealing: In general, an annealing treatment of about 1010℃(1850℉) for 15 min. will produce soft material. Brief exposure to 1037℃(1900℉) will give soft material without producing a coarse grain structure. Grain growth does not occur until the alloy is heated to about 980℃(1800℉).

Oil, grease, lacquer and all other contaminants must be removed before annealing.


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