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Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine

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    Buy cheap Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine from wholesalers
     
    Buy cheap Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine from wholesalers
    • Buy cheap Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine from wholesalers
    • Buy cheap Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine from wholesalers

    Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine

    Ask Lasest Price
    Brand Name : DINGSCO
    Model Number : According to customers requirements
    Certification : ISO 9001:2015,PED 2014/68/EU,API 6A,API-20B,TSG,NORSOK
    Price : Negotiable
    Payment Terms : T/T
    Supply Ability : Negotiable
    Delivery Time : (Sample Order) 7 days
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    Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine

    Nickle Alloy Angle Bar Inconel 718 UNS NO7718


    Nickle Alloy Angle Bar​, or angle iron, is basically manufactured by hot-rolled high strength Nickle Alloy steel. It has L-cross shaped section with two legs - equal or unequal and the angle would be 90 degree. Structural steel angles have lots of dimensions to comply with your uses. In addition, bespoke sizes are available. I


    Many Uses:

    • Supporting & structural factors - bridges, warehouses, shelves, cable towers, power towers, communication towers, equipment, etc.
    • Everyday life uses - bed frames, chairs, benches, fencing posts, frames for supporting air conditioner, coffee tables and so on.

    Inconel 718(UNS NO7718) is a GammaPrime strengthened aloy with excelent mechanicalproperties at elevated temperatures, as wel as cryogenidtemperatures. Suitable for temperatures up to around1300 °F. Can be readily worked and age hardened. Excellent strength from -423 °Fto 1300°F(-253 'C to 705C).Age hardenable and may be welded in fully agedcondition, Excellent oxidation resistance up to 1800 °F(980 °C).Typically sold in the solution annealed temperbut can be ordered aged, cold worked, or cold worked &aged. Alloy 718 is a high strength, nickel base, superalloy usedfor cryogenic temperatures up to long term service at1200 °F. This alloy is readily fabricated and may be weldedin either the annealed or precipitation hardened(aged)condition.718 is annealed at 1700-1850 'F and air cooledor faster. lt is aged at 1325 °F for 8 hours, furnace cooledto hold at 1150 'F, for a total aging time of 18 hours, thenair cooled.Alloy 718 wil show a contraction of 0.0008inch/inch after precipitation hardening. Good mechanical properties: tensile,fatigue, and creep-rupture. Excelent welding characteristics and resistant to postweld age cracking. Oxidation resistant throughout its useful temperature range.


    Applications:

    Uses for this alloy tend to be in the field of gas turbine components and cryogenic storage tanks. Alloy 718 iscommonly used in jet engines, pump bodies and partsrocket motors and thrust reversers, and hot extrusiontooling.Other popular uses are high strength bolting anddown hole shafting.

    Mechanical Properties:
    The typical properties listed can usually be provided inrounds, sheet, strip, plate,& custom forgings. We havethe equipment to produce small quantities in special sizesto meet our customers’ specific needs. The table belowshows Special Metals' Nominal Room-TemperatureMechanical Properties of Alloy 718 Bars, Forgings, & Ringsand Sheet, Strip,& Plate. For most common forms andexceptions, check out the datasheet linked underneath the table.


    PropertiesYS(Ksi)TS(Ksi)EL(%)HRC
    Room Temperature1801501236
    1200℉(<0.025-in)140115--
    1200℉(>0.025-in )1451205-

    Chemical Composition:


    ElementNiCrSCMnSiMoCuCoAlNbBP
    Minimum(%)5017----2.8--0.24.75--
    Max(%)55210.0150.080.350.353.30.31.00.85.50.0060.015

    Our QC Activities and Test Methods:


    Chemical AnalysisASTM E1473ensileTestASTM E8
    Hardness TestASTM E 10,E 18PMl ExaminationDINGSCO SOP
    Ultrasonic NDTBS EN 10228Liquid Penetrant NDTASTM E 165
    Dimensional and inspectionDINGSCO SOPRoughness TestDINGSCO SOP
    Impact TestASTM E 23Low Temperature lmpact TestASTM E 23
    Creep and Stress Rupture TestASTM E 139Hydrogen Induced Cracking TestNACE TM-0284 *
    Inter Granular Corrosion TestASTM A 262 *Sulfide Stress Corrosion Cracking TestNACE TM-0177 *
    Pitting and Crevice Corrosion TestASTM G 48 *Macro Etching TestASTM E 340*
    Grain Size TestASTM E 112 *

    * Done by state own third party laboratory


    Processing Flow Chart:


    Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine


    Quality Nickle Alloy Angle Iron Bar Inconel 718 UNS NO7718 For Jet Engines Gas Turbine for sale
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