Alloy A286

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Alloy A286


A-286 alloy is an age-hardenable iron base superalloy for applications requiring high strength from -320°F up to 1000°F long time, 1300-1500°F short time. Oxidation resistance is high for continuous service to 1500°F, intermittent to 1800°F. Aqueous corrosion resistance is comparable to 316/316L stainless. Heat treatment according to AMS 5525 requires a solution anneal at 1800°F, air cool. Age at 1325°F for 16 hours and then air cool.

Applications


Valve parts, Paper mills, aircraft and power generation, chemical processing, nuclear and space craft.

Heat Treatment


Solution heat treatment, heat at 1875/1925f (1024/1052c cool to below 90f (32c) to allow material to fully martensite. Material can be air cooled, but should be rapidly quenched for best response to aging.

Aging


All solution treated materials: Condition H-900 4hrs and air cool. H-900 offers the best combination of ductility, strength and toughness. H-1150 increases ductility but decreases strength.

Mechanical Properties

* 70°F to indicated temperature.

Representative Tensile Properties, Sheet

Temperature, °F 70* 70 400 800 1000 1200 1400
Ultimate Tensile Strength, ksi 95* 145 143 138 131 103 64
0.2% Yield Strength, ksi 50* 95 93 93 87 88 62
Elongation, % 40* 24 21 18 18 13 18

Chemical Composition(%)

Cr Ni Mo Co Va Al Ti B C Fe Mn Si Ph S
MIN 13.5 24.0 1.0 - 0.1 - 1.9 0.003 - - - - - -
MAX 16.0 27.0 1.5 1.0 0.5 0.35 2.35 0.01 0.08 Balance 2.0 1.0 0.025 0.025

Specifications

AMS 5525, AMS 5732, AMS 5737, AMS 5804
EN 1.4980
GE B50T1181, GE B50T12, GE B50T81
UNS S66286
Werkstoff 1.4980

Inventory

A-286 Coil, A-286 Hex Bar, A-286 Round Bar, A-286 Sheet

Common Trade Names

A286 Stainless, A286 Alloy

Features

  • High strength to 1000°F
  • Oxidation resistant to 1500°F
  • Applications

  • Jet engine components
  • High temperature fasteners, springs
  • Non-magnetic cryogenic equipment
  • Physical Properties

    Density: 0.303 lb/inch3
    Melting Range: 2350-2460°F

    Temperature, °F 200 800 1000 1200 1400
    Coefficient of Thermal Expansion, in/in°F x 10-6 9.2 9.6 9.8 9.9 10.3
    Thermal Conductivity
    Btu • ft/ft2 • hr • °F
    8.0 9.8 13.0 14.1 -
    Modulus of Elasticity,
    psi X 106
    - - 24 22 23

    * Annealed

    Typical Stress-Rupture Strength 1800°F/1325°F Heat Treat

    Temperature, °F 1000 1100 1200
    100 Hours, ksi 99 81 61
    1,000 Hours, ksi 88 71 46

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