Nickel Alloy Nimonic 80A UNS N07080

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Short Introduction:

HY N80A/Nimonic 80A /UNS N07080 /SEW VDIUV W. Nr. 2.4952 /AFNOR NC20TA  is a nickel-chromium alloy similar to alloy 75 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures to 1500°F (815°C). Used for gas-turbine components (blades, rings, and discs), bolts, tube supports in nuclear steam generators, die-casting inserts and cores, and exhaust valves in internal-combustion engines.

 


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  • Product Detail

    Product Tags

    HY 80A Material grades and equivalents
    Nimonic 80A /UNS N07080 / SEW VDIUV W. Nr. 2.4952 / AFNOR NC20TA

    HY N80A Chemaical composition:

    Alloy

    %

    Ni

    Cr

    Fe

    Mn

    Si

    P

    S

    Al

    Ti

    C

    Co

    B

    Zr

    Cu

    80A

    Min.

    Balance

    18

    1.0

    1.8

    Max.

    21

    3.0

    1.0

    1.0

    0.02

    0.015

    1.8

    2.7

    0.1

    2.0

    0.008

    0.15

    0.2

    HY N80A Physical properties:

    Density

    8.19 g/cm3

    Melting point

    1320-1365℃

    HY N80 A minimum mechanical properties in the room temperature :

    Status

    Tensile strength
    Rm N/mm2

    Yield strength
    RP0.2N/mm2

    Elongation
    A5 %

    HY N80A

    930

    620

    20

    Characteristic as below:

    A nickel-chromium alloy similar to NIMONIC alloy 75 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures to 1500°F (815°C).
    Used for gas-turbine components (blades, rings, and discs), bolts, tube supports in nuclear steam generators, die-casting inserts and cores, and exhaust valves in internal-combustion engines.

    Specification

    Rod, Bar, Wire and Forging Stock

    BS 3076 HR1, ASTM B 637, AECMA PrEn2188, AECMA PrEn2189, AECMA PrEn 2190, AECMA PrEn 2396, AECMA PrEn2397, AIR 9165-37

    Plate, Sheet and Strip

    BS HR 201, AECMA PrEn2191 

    Pipe and Tube

    BS HR 401

     

    Regular shape for all kinds of alloys
    Form Specification Supply Form Others
    Sheet Thickness:0.40-4.75mm,General Width:1000、1219、1500mm Whole Coil or piece of it Cold Annealed,Surface 2B、2E
    Plate Thickness:4.76-60mm,Width:1500、2000、2500mm,Length:3000、6000、8000、8500mm(Under 10mm plate can be coiled) Whole Coil or piece of it Single hot rolling,Solid solution annealed state,Surface 1D
    Belt Thickness:0.10-3.0mm,Width:50-500mm Whole Coil or Specified size Cold Annealed,Surface 2B、2E
    Bar & Rod Rolled barΦ5-45mm,Length≤1500mm Polished Bar(circle、Square) Solution annealing,descaling
    Forged barΦ26-245mm,Length≤4000mm
    Weld tube Outer diameterΦ4.76-135mm,Wall Thickness0.25-4.00mm,Length:≤35000 mm Base on your requirement
    Seamless Tube Outer diameterΦ3-114mm,Wall Thickness0.2-4.5mm Base on your requirement
    Wire Outer diameterΦ0.1-13mm Base on your requirement Ni & Ni alloy, Ti & Ti alloy
    Forged piece discs,rings,squares,blocks,slabs Base on your requirement Steel, Alloy
    Flangs All kinds of Flangs Base on your requirement Steel, Alloy
    Welding Material Coil wire Φ0.025mm-1.6mm Base on your requirement Certificate of Origin:America, Sweden, Britain, Germany, Austria, Italy, France.
    Straight WireΦ1.6mm-4.0mm
    Welding rodΦ1.2mm-4.0mm
    Tube Elbow, three links, four links, different diameter size Base on your requirement Ni & Ni alloy, Ti & Ti alloy
    Explosive bonded laminate Raw Sheet Thickness≥2mm Base on your requirement Ni & Ni alloy, Ti & Ti alloy





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