Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations

China Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations, Find details about China Uns No7718 Plate, Inconel 718 Price from Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations

Model NO.
Inconel 718
Thickness
0.4-8mm
Width
1000/1219/1500mm
Length
2000-6000mm
MOQ
100kgs
Sample
Free-Sample
Surface
2b, No.1
Technique
Cold Rolled, Hot Rolled
Mtc
En 10204 Type 3.1
Stock
in Stock
T.S.(≥ MPa)
827
Key Words
625 Nickel Alloy Sheet
Trademark
ZYTC
Transport Package
Wooden Package
Specification
Inconel 718
Origin
China
HS Code
7502200000
Model NO.
Inconel 718
Thickness
0.4-8mm
Width
1000/1219/1500mm
Length
2000-6000mm
MOQ
100kgs
Sample
Free-Sample
Surface
2b, No.1
Technique
Cold Rolled, Hot Rolled
Mtc
En 10204 Type 3.1
Stock
in Stock
T.S.(≥ MPa)
827
Key Words
625 Nickel Alloy Sheet
Trademark
ZYTC
Transport Package
Wooden Package
Specification
Inconel 718
Origin
China
HS Code
7502200000

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
 

MaterialMonel/Inconel/Hastelloy/Duplex Steel/PH Steel/Nickel Alloy
ShapeRound,Forging,Ring,Coil,Flange,Disc,Foil,Spherical,Ribbon,Square,Bar,Pipe,Sheet
 GradeDuplex: 2205(UNS S31803/S32205),2507(UNS S32750),UNS S32760(Zeron 100),2304,904L
 Others:253Ma,254SMo,654SMo,F50(UNSS32100)F60,F61,F65,1J22,N4,N6 etc
 Alloy : Alloy 20/28/31
 Hastelloy:HastelloyB/ -2/B-3/C22/C-4/S/ C276/C-2000/G-35/G-30/X/N/g
 Hastelloy B / UNS N10001,Hastelloy B-2 / UNS N10665 / DIN W. Nr. 2.4617,Hastelloy C,
Hastelloy C-4 / UNS N06455 / DIN W. Nr. 2.4610,Hastelloy C-22 / UNS N06022 / DIN W. Nr. 2.4602,
Hastelloy C-276 / UNS N10276 / DIN W. Nr. 2.4819,Hastelloy X / UNS N06002 / DIN W. Nr. 2.4665
 Haynes: Haynes 230/556/188
 Inconel 600/601/602CA/617/625/713/718/738/X-750,Carpenter 20
 Inconel 718 / UNS N07718 / DIN W. Nr. 2.4668,Inconel 601 / UNS N06601 / DIN W. Nr. 2.4851,
Inconel 625 / UNS N06625 / DIN W. Nr. 2.4856,Inconel 725 / UNS N07725,Inconel X-750 / UNS N07750 / DIN W. Nr. 2.4669,Inconel 600 / UNS N06600 / DIN W. Nr. 2.4816
 Incoloy: Incoloy 800/800H/800HT/825/925/926;
 GH: GH2132,GH3030,GH3039,GH3128,GH4180,GH3044
 Monel: Monel 400/K500/R405
 Nitronic: Nitronic 40/50/60;
 Nimonic: Nimonic 75/80A/90/A263 ;
 
 
Specification
Wire: 0.01-10mm
Strip: 0.05*5.0-5.0*250mm 
Bar: φ4-50mm;Length 2000-5000mm
Pipe: φ6-273mm;δ1-30mm;Length 1000-8000mm
Sheet: δ 0.8-36mm;Width 650-2000mm;Length 800-4500mm
 
 
Product 
Characteristics
1.According to the preparation process can be divided into deformation superalloys, 
casting superalloys and powder metallurgy superalloys.
2.According to the strengthening mode, there are solid solution strengthening type, precipitation 
strengthening type, oxide dispersion strengthening type and fiber strengthening type, etc..
StandardGB,AISI,ASTM,DIN,EN,SUS,UNS etc
InspectionISO,SGS,BV and so on.
 
Application
High temperature components such as turbine blades, guide vanes, turbine disks, 
high pressure compressor disks,machine manufacturing
and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines
 
 
Packaging
1. cases packed in wooden cases
2. paper packaging
3. plastic packing
4. foam packaging
Packaging according to customer requirements or products
Delivery7-25days orAccording to the product
 
Payment
L/C,D/A,D/P,T/T,Western Union,MoneyGram,According to customer requirements payments
for offline orders.

Properties of Inconlel 718

Inconel 718 is a nickel-based super alloy that is well suited for applications requiring high strength in temperature ranges from cryogenic up to 1400°F. Inconel 718 also exhibits excellent tensile and impact strength.
 

Chemical Composition of Inconel 718

Typical chemical analysis of Inconel 718.

ElementPercentage
Carbon0.08 max
Manganese0.35 max
Phosphorus0.015 max
Sulfur0.015 max
Silicon0.35 max
Chromium17-21
Nickel50-55
Molybdenum2.80-3.30
Columbium4.75-5.50
Titanium0.65-1.15
Aluminum0.20-0.80
Cobalt1.00 max
Boron0.006 max
Copper0.30 max
Tantalum0.05 max
IronBalance

Resistance to Corrosion and Oxidation of Inconel 718

Inconel 718 has good resistance to oxidation and corrosion at temperatures in the alloy's useful strength range in atmospheres encountered in jet engines and gas turbine operations.

Physical Properties of Inconel 718

Typical physical properties of Inconel 718 are summarized in the table below.

 Solution TreatedSolution Treated and Aged
Density0.296 lb/in3 (8.192 g/cm3)0.297 lb/in3 (8.22 g/cm3)
Specific Gravity8.198.22
Melting Range2500-2600°F1370-1430°C

Thermal Conductivity of Inconel 718

The thermal conductivity at various temperatures for Inconel 718 are given in the following table.

Temperature RangeCo-Efficients
°C°FW/m.KBtu.ft/ft2.hr.°F
0-100532-2126.511.2

Mechanical Properties

The room temperature strength of the Inconel 718 alloy is substantially increased by precipitation heat treatment as the following data indicate. These values are properties specified for sheet, strip and plate in AMS 5596 and AMS 5597.

 Yield Strength
Min
 (0.2% offset)
Ultimate Tensile Strength
Min
Elongation
(% in 2")
Sheet and strip80,000 psi (550 MPa)140,000 psi (965 MPa)30 (min)
Plate105,000 psi (725 MPa)150,000 psi (1,035 MPa)30 (min)

Solution trated plus precipitation heat treated.

Yield Strength
Min
 (0.2% offset)
Ultimate Tensile Strength
Min
Elongation
(% in 2")
150,000 (1,035 MPa)180,000 psi (1,240 MPa)12 (min)

 

Typical short time tensile properties of Inconel 718 as a function of temperature are shown here for material solution treated and aged as follows:

  • Solution Treatment: 1800°F (982°C) 1 hour
  • Precipitation Treatment: 1325°F (718°C) 8 hours, Furnace Cool at 100°F (55°C) per hour to 1150°F (621°C) 8 hours

Standards

United Performance Metals Inconel 718 is supplied to AMS 5596/5597 and has a UNS designation N07718.

Applications of Inconel 718

Inconel 718 is typically used for:

  • Jet engine
  • Gas turbine operations


Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine OperationsGh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
 

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations
 

Q1: Do you accept the trial order ?
A1: Yes,if we have the exactly size in stock.we can delivery even 1 piece/meter .

Q2: Can I have free sample before making orders?

A2: Yes,we can supply free sample as requirement,but buyer needs to pay the freight charges ,the freight fee will return to buyer after making order.

Q3: How do you control the quality ?
A3: MTC and PMI will be sent before shipment,any 3rd party inspection if need .

Q4: How about your delivery time ?
A4: Generally delivery time is 15 working days .

Q5: How can I quickly get the price list ?
A5: Directly click "chat now" or send us email with detail specifications,you will get the official price list in 1 hour .

Gh4169 Gh169 Nc19fenb Nicr19fe19nb5 Inconel 718 Nickel Alloy Plate for Gas Turbine Operations