Shanghai Tankii Alloy Material Co.,Ltd

Shanghai Tankii Alloy Material Co.,Ltd

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Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

    • Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial
    • Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial
  • Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

    Product Details:

    Place of Origin: China
    Brand Name: Superalloys
    Certification: ISO 9001 and RoHS
    Model Number: GH3030/ Nimonic 75

    Payment & Shipping Terms:

    Minimum Order Quantity: 50KG
    Price: USD 25~50 / KG
    Packaging Details: Wooden case
    Delivery Time: 25-30 days
    Payment Terms: T/T, Western Union, L/C
    Supply Ability: 50000
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    Detailed Product Description
    Shape: Bar Condition: Soft And Hard
    Diameter: 5-150 Density (g/cm3): 8.4
    Melting Point (℃): 1374~1420 Feature: Good Resistance To Oxidation

     Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

     

     

    Application:

     

    This alloy be used for turbine engine combustor components operating below 800 degrees Celsius and in 1100 degrees Celsius under load requirements antioxidant but small high temperature components.

    High temperature alloy cold drawn rod is cold drawn into a diameter of 8 ~ 45mm circular edge length of 8 ~ 30mm square, inscribed circle diameter of 8 ~ 36mm simple hexagonal cross section superalloy bars, used in the manufacture fasteners in aviation industrial and other industries.

     

    Physical properties

     

    >Density (g/cm3): 8.4

    >Melting point (℃): 1374~1420

     

    Feature: At 800 degrees Celsius with a satisfactory heat resistance and high ductility, and has good resistance to oxidation, thermal fatigue, cold stamping and welding performance. For single-phase austenitic alloys course after solution treatment and stable organization.

     

    Description:

    Chemical composition(%)

     

    Grade

    C

    Si

    Mn

    Ti

    S

    Ni

    Cr

    Cu

    Fe

    GH3030

    ≤0.12

    ≤0.8

    ≤ 0.7

    0.15~0.35

    ≤0.015

    Bal.

    19~22

    ≤0.2

    ≤1.5

     

     

     

     

     

    Yield Strength (Mpa)

    Tensile Strength (Mpa)

    Elongation, %

    Hardness, HB

    GH3030

    Solution treatment

    270

    650

    ≤30

     

     

     

     

     

     

     

     

     

     

     

    If you have any questions, pls write email to us: zlz@tankii.com

    Looking forward to your inquiry!

     

    Contact Details
    Shanghai Tankii Alloy Material Co.,Ltd

    Contact Person: tankii

    Tel: +8615000002421

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