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Applications and smelting of superalloy A286

I. Overview

The American standard superalloy A286 is an iron-chromium-nickel-based high-temperature alloy, developed through comprehensive strengthening by adding molybdenum, titanium, aluminum, vanadium, and trace amounts of boron. It is equivalent to the domestic grade GH2132 and the French grade ZbNCT25. Depending on the standard to which A286 belongs, there will be certain differences in chemical composition, mechanical properties, and heat treatment regimes.

1. Chemical Composition (Refer to standard SAE J467b) 

ComponentCSiMnCrNiMoTiVBAlMore
Nominal Value0.050.41.415261.32.150.30.0040.2Fe: Balance

2. Mechanical Properties (Refer to standard SAE J467b)

In the solution-treated state, the microstructure of A286 alloy consists of a γ-phase austenite matrix. It is strengthened by the precipitation of the intermetallic compound γ' phase Ni3(Ti, Al) during aging. After solution and aging treatment, it possesses good comprehensive properties, such as high yield strength, good hot hardness, and high creep strength

TemperatureHeat Treatment or ConditionTensile Strength (MPa)Yield Strength (MPa)Elongation after Fracture (%)Reduction of Area (%)HardnessImpact Absorption Energy (KV2/J)
Room Temp 21°C982°C, 718°C10006552445HBW: HRC 2687
Room Temp 21°C899°C, 718°C10827032546302-
64°C982°C, 718°C7106071314--
649°C899°C, 718°C7526211825--

Mechanical Properties after Heat Treatment per Other Common Standards


StandardRoom Temperature Properties



TemperatureStress Rupture Properties

Rm (MPa)Rp0.2 (MPa)A (%)Z (%)Hardness°CRm (MPa)
AMS 5726—200613791241815>40HRC--
AMS 5731—20068965861520248~341HBW649483
AMS 5732—20068965861520248~341HBW649483
AMS 5734—20069656551215277~363HBW649448
AMS 5737—20069656551215277~363HBW649448
AMS 5853—200611038271218≥32HRC--
3. Physical Properties (Refer to standard SAE J467b)


Density 70F (lb/in³)Specific Gravity (g/CC)Melting Point (F)Linear Expansion Coefficient (in./in./Fx10⁻⁶)










70-20070-40070-60070-80070-100070-120070-140070-160070-1800
0.2867.942500 - 26009.179.359.479.649.789.8810.32--

Elastic Modulus (E) 10⁶ psi
Shear Modulus (G) 10⁶ psi
Poisson's RatioThermal Conductivity
Electrical Resistivity
FEFEFGFG70F
7029.1150018.770111500680.306

4. Heat Treatment Regimes (Heat treatment regimes corresponding to each standard)

StandardStandard Recommended Heat Treatment Regime
AMS 5726—2006982°C ± 14°C Solution + 649°C ~ 704°C ± 14°C Aging not less than 8h
AMS 5731—2006982°C ± 14°C Solution + 718°C ± 8°C Aging not less than 16h
AMS 5732—2006982°C ± 14°C Solution + 704°C ~ 760°C Aging not less than 16h
AMS 5734—2006899°C ± 14°C Solution + 718°C ± 8°C Aging not less than 16h
AMS 5737—2006899°C ± 14°C Solution + 704°C - 760°C Aging not less than 16h
AMS 5853—2006982°C ± 14°C Solution 1 ~ 2h + 649°C ~ 704°C ± 14°C Aging not less than 8h

II. Application Fields

A286 possesses high yield strength, stress rupture strength, and creep strength below 650°C, as well as good processing plasticity and welding performance. It is suitable for manufacturing components working long-term below 650°C:

1. High-temperature load-bearing parts for aero-engines Such as turbine disks, compressor disks, and rotor blades.

2. Fasteners Such as various bolts, screws, self-locking nuts, aviation rivets, etc. Common material standards for A286 high-temperature alloy used in fasteners include AMS 5726/5731/5732/5734/5737/5853 (Bar and Wire standards). The main types of these products are concentrated in 900MPa class nuts, 1100MPa class aviation HB series bolts, 1300MPa class NAS series high-strength bolts, and test mandrels.

StandardMaterial TypeMaterial StateSize (mm)Property Class (MPa)Service ConditionRecommended Use
AMS 5726-2006
Solution + Cold Work≤31.81379Maintain strength under 538°C; Oxidation resistance under 649°C1300MPa class products
AMS 5731-2006
Solution-896Maintain strength under 704°C; Oxidation resistance under 816°C900MPa class products; products requiring forging
AMS 5732-2006BarSolution + Aging-896
900MPa class products; purely machined products
AMS 5734-2006WireSolution-965
900MPa class products; products requiring forging
AMS 5737-2006
Solution + Aging-965
900MPa class products; purely machined products
AMS 5853-2006
Solution + Cold Work≤31.81103Maintain strength under 538°C; Oxidation resistance under 649°C1100MPa class products

III. Melting Methods 

Most high-quality high-temperature alloys and corrosion-resistant alloy specialty materials both domestically and internationally are not produced using a single process. Instead, they are smelted using duplex or triplex methods, namely Vacuum Induction Melting + Electro-Slag Remelting (VIM+ESR) or Vacuum Induction Melting + Vacuum Arc Remelting (VIM+VAR).

Currently, domestic A286 alloy high-temperature material uses the VIM+VAR process for smelting to improve and guarantee the purity of the alloy, making the alloy's thermal strength and long-term service performance better.

1. Vacuum Induction Melting (VIM) This is a method of smelting in vacuum conditions using electromagnetic induction to generate eddy currents within the metal conductor to heat the charge. VIM provides maximum control over chemical composition and prevents the molten liquid from contacting hydrogen, oxygen, and nitrogen in the atmosphere. Electromagnetic stirring not only homogenizes the melt but also continuously brings reactants to the interface between the melt and the vacuum, thereby facilitating subsequent refining reactions. The volatilization and precipitation of gas content and non-metallic inclusions can greatly improve the mechanical properties of most high-temperature alloys. The VIM furnace is important smelting equipment for the production of nickel-based high-temperature alloys, corrosion-resistant alloys, and other special alloy materials. In particular, for alloys containing large amounts of reactive elements like aluminum and titanium, vacuum induction melting must be used.

2. Vacuum Arc Remelting (VAR) This is a process where, under vacuum conditions, a DC power source generates an arc between an electrode and a copper crucible base plate placed in a water jacket. The arc generates high heat, melting the electrode. The electrode continuously descends and melts, forming a molten pool within the water-cooled copper crucible. The molten metal completes rapid solidification, crystallization, and solidifies into an ingot. VAR is generally used for refining stainless steel, superalloys, and easily oxidized metals and alloys such as titanium, zirconium, tantalum, niobium, tungsten, and molybdenum. It reduces the loss of active elements (such as Al, Ti), makes the ingot solidification process controllable, and significantly improves the cleanliness, uniformity, fatigue resistance, and fracture toughness of the ingot. Therefore, its structural consistency and uniformity are better, the number of inclusions is small, and the purity of the alloy is further improved. VAR furnaces experience a phosphorus reversion phenomenon during pouring and cannot control the phosphorus content to a very low level. It is suitable for smelting special steels and reactive and refractory metals like titanium, molybdenum, and niobium. Different smelting processes cause slight differences in impurity elements like phosphorus (P), sulfur (S), manganese (Mn), and gas elements in the A286 alloy.



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