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Size Custom Nickel Alloy Wires Inconel 718 Welding Wire UNS NO7718

Categories Nickel Alloy Wires
Brand Name: DINGSCO
Model Number: According to customers requirements
Certification: ISO 9001:2015,PED 2014/68/EU,API 6A,API-20B,TSG,NORSOK
Place of Origin: China
MOQ: Negotiable
Price: Negotiable
Payment Terms: T/T
Supply Ability: Negotiable
Delivery Time: (Sample Order) 7 days
Packaging Details: According to Customers' Requests
Product Name: Nickel Alloy Wires
Grade: Inconel 718
UNS: NO7718
Density of annealed alloy 718: 0.296 lb/in3
Density of annealed and aged alloy 718: 0.297 lb/in3
Melting Point: 1260-1336℃
Specific Heat at 70℉: 0.104 (435)
Curie Temperature annealed and aged alloy: -170℉ (-112℃)
Permeability at 200 oersted and 70oF of Annealed Material: 1.0013
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Size Custom Nickel Alloy Wires Inconel 718 Welding Wire UNS NO7718

Nickle Alloy Wires Inconel 718 UNS NO7718 Corrosion-Resistant Parts


Nickle Alloy Ring are the most common in forged metals. Through open die forging,the metal is formed into something that's shaped like a doughnubefore it's heated between 400 and 700'c. Next, it's placed on a mandrel or idler rol that increases the steel ring's diameters and reduces thethickness of its walls. You can find them in machinery and equipment, vehicles, pipes and valves, and other hardware. Almost all vehicles and otherheavy machinery make use of them because they are durable and easy to replace and look for.


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.

Mechanical Properties:
.

PropertiesYS(Ksi)TS(Ksi)EL(%)HRC
Room Temperature1801501236
1200℉(<0.025-in)140115--
1200℉(>0.025-in )1451205-
PropertiesYS(Ksi x 103)TS(Ksi(Ksi x 103)
1700'F18.87.1--
1800'F17.46.5--
1900'F15.95.8--
2000'F14.35.1--

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:



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