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DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718

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    Buy cheap DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718 from wholesalers
     
    Buy cheap DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718 from wholesalers
    • Buy cheap DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718 from wholesalers
    • Buy cheap DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718 from wholesalers

    DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718

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    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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    DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718

    Nickle Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718


    Welding wires are slim metallic wires that are usually coiled up in spools. These spools are loaded on a wire feeder and the welding wire is continuously fed through a welding gun into the molten weld pool. As a result, arc welding processes that use a welding wire tend to offer higher deposition rates and faster travel speeds, as compared to TIG and Stick welding where the welder must manually feed the filler metal into the weld puddle.


    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 turbinecomponents 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.


    Chemical Composition:


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

    Mechanical Properties:


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

    Thermal Properties:


    Temperature, °FThermal Conductivitya, BTU•in/ft2 •h•°FElectrical Resistivitya, ohm circ mil/ftMean Linear Expansionb,c, in/in/°F x 10-6
    Ann. 1800°F/1 hrAnn. + AgedAnn. 1800°F/1 hrAnn + Aged
    -320----5.9d
    707779753725-
    20086877627337.31
    400981007727557.53
    6001111127757687.74
    8001231247847757.97
    10001351367987888.09
    12001471488057948.39
    14001601618027978.91
    1600173173799796-
    1800185186801800-
    2000196199811796-

    aAnnealing was 1800°F/1 hr; aging was 1325°F/8 hr, F.C. 20°/hr to 1150°F, held at 1150°F for total aging time of 18 hr. Conductivity calculated from resistivity values.

    bFrom 70°F to temperature shown.

    cAnnealed 1750°F/1 hr and aged 1325°F/8 hr, F.C. to 1150°F/8 hr, A.C. d Samples tested were in both the annealed (1750°F/1 hr, A.C.) and annealed and aged (1750°F/1 hr + 1325°F/8 hr, F.C. to 1150°F, held at 1150°F for 10 hr, A.C.) conditions.


    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:


    DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718


    Quality DINGSCO Nickel Alloy Wires Inconel 718 Aircraft Turbines Fasteners Spacers UNS NO7718 for sale
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