Send Message
products
PRODUCTS DETAILS
Home > Products >
Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169

Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169

MOQ: 100KGS
Price: 15.7 USD/KG
Standard Packaging: Wooden Box Wooden Pallet
Delivery Period: 7 Days
Payment Method: L/C, T/T
Supply Capacity: 80000KGS
Detail Information
Place of Origin
China
Brand Name
TSING SHAN
Certification
ISO MTC SGS
Model Number
718 GH4169
Tolerance:
±1%
Special Use:
Compressor Disks,machine Manufacturing
Young'S Modulus:
205 GPa
Curie Point:
-319℉ (-195℃)
Standard:
ASTM, JIS, AISI, EN, GB
Executive Standard:
ASTM
Wire:
MIG
Hardness:
170 HB
Type:
Nickel Bar
Melting Point:
1350-1400°C
Elongation At Break:
45%
Surface Treatment:
Anodized,Brushed,Mill Finished,Polished
Delivery State:
Sosoloid
Packing:
Standard Export Packing
Highlight:

GH4169 Nickel Alloy Round Bar

,

UNS N07718 Nickel Alloy Round Bar

Product Description

Nickel Alloy 718 Round Bar 718 Nickel AlloyInconel 718 round Bar W. Nr. 2.4668 UNS N07718 GH4169 Black and Bright Bar

 

Nickel Alloy 718 (INCONEL® 718) | UNS# N07718

Nickel 718 (UNS# N07718), or Inconel 718 is a precipitation hardening nickel-chromium alloy that contains molybdenum, iron, columbium, and smaller traces of aluminum and titanium. Designed to exhibit significant yields, high strength, good ductility, and creep rupture properties up to 1300°F (704°C). These characteristics provide alloy 718 good formability, weldability, and cryogenic allowances compared to the metals other nickel based superalloys. The sluggish age hardening characteristics in alloy 718 also allow annealing and welding without the occurrence of spontaneous hardening during heating and cooling. This alloy is also non-magnetic, maintains significant corrosion and oxidation resistances and can be used in applications like jet engines, airframe components, and high temp bolts and fasteners.

Nickel Alloy 718 Inventory Size Range:

718 Nickel Alloy Round Bar Specifications:

Common Names:

  • ATI 718
  • Haynes 718
  • INCONEL® Alloy 718

Nickel Alloy 718 Applications:

  • Jet engines
  • Rotor Bolts
  • Gas turbine operations
 

DISCLAIMER: Alloy data sheets are for reference only, not for design purposes.

Chemical Composition

  C Mn Fe P S Si Cu Ni Co Al Ti Cr Nb+Ta Mo
Inconel 600 ≤0.15 ≤1.0 6.0-10.0 ≤0.015 ≤0.015 ≤0.5 ≤0.5 ≥72.0 -- -- -- 14.0-17.0 -- --
Inconel 601 ≤0.1 ≤1.5 balance ≤0.02 ≤0.015 ≤0.5 ≤1.0 58.0-63.0 -- 1.0-1.7 -- 21.0-25.0 -- --
Inconel 625 ≤0.1 ≤0.5 ≤5.0 ≤0.015 ≤0.015 ≤0.5 -- ≥58.0 ≤1.0 ≤0.4 ≤0.4 20.0-23.0 3.15-4.15 8.0-10.0
Inconel 617 0.05-0.15 ≤1.0 -- ≤0.012 ≤0.015 ≤1.0 ≤0.5 ≥44.5 10.0-13.0 0.8-1.5 ≤0.6 20.0-24.0 -- 8.0-10.0
Inconel 690 ≤0.05 ≤0.5 7.0-11.0 -- ≤0.015 ≤0.5 ≤0.5 ≥58.0 -- -- -- 27.0-31.0 -- --
Inconel 718 ≤0.08 ≤0.35 balance ≤0.015 ≤0.015 ≤0.35 ≤0.3 50.0-55.0 ≤1.0 0.2-0.8 0.65-1.15 17.0-21.0   2.8-3.3
Inconel 725 ≤0.03 ≤0.35   ≤0.015 ≤0.010 ≤0.20   55.0-59.0       19.0-22.5   7.0-9.5
Inconel 750 ≤0.08 ≤1.0 5.0-9.0 -- ≤0.01 ≤0.5 ≤0.5 ≥70.0 ≤1.0 0.4-1.0 2.25-2.75 14.0-17.0 0.7-1.2 --
Inconel 20 ≤0.07 ≤2.0 balance ≤0.045 ≤0.035 ≤1.0 3.0-4.0 32.0-38.0 -- -- -- 19.0-21.0 8*C-1 2.0-3.0
Inconel 28 ≤0.02 ≤2.5 balance ≤0.02 ≤0.015 ≤1.0 0.6-1.4 30.0-34.0       26.0-28.0   3.0-4.0
Inconel 925 ≤0.03 ≤1.0 balance ≤0.03 ≤0.03 ≤0.5 1.5-3.0 42.0-46.0 -- 0.15-0.5 1.9-2.4 19.5-23.5 -- 2.5-3.5
Inconel 926 ≤0.02 ≤2.0 balance ≤0.03 ≤0.01 ≤0.5 0.5-1.5 24.0-26.0 -- -- -- 19.0-21.0 -- 6.0-7.0
Inconel 825 ≤0.05 ≤1.0 balance ≤0.02 ≤0.03 ≤0.5 1.5-3.0 38.0-46.0 -- ≤0.2 0.6-1.2 19.5-23.5 -- 2.5-3.5
Inconel 800 ≤0.1 ≤1.5 balance -- ≤0.015 ≤1.0 ≤0.75 30.0-35.0 -- 0.15-0.6 0.15-0.6 19.0-23.0 -- --
Inconel 800H 0.05-0.1 ≤1.5 balance   ≤0.015 ≤1.0 ≤0.75 30.0-35.0 -- 0.15-0.6 0.15-0.6 19.0-23.0 -- --
Inconel 800HT 0.06-0.1 ≤1.5 balance   ≤0.015 ≤1.0 ≤0.75 30.0-35.0   0.15-0.6 0.15-0.6 19.0-23.0    

 

PHYSICAL PROPERTIES
Density Electrical conductivity (% IACS) Thermal conductivity (BTU-in/hr-ft²-°F) Specific heat (BTU/lb-°F) Thermal expansion (1/°F) Thermal expansion Melting Point (°F)
0.296 1.38 77 0.104 7.22E-06 2300

 

 

 

MECHANICAL PROPERTIES
PROPERTY MINIMUM MAXIMUM
Yield Strength Range (Rp0.2 Offset) (ksi) 80 150
Tensile Strength Range (Rm) (ksi) 14 220
Elongation (AL=5 x Ø) 18% 27%
Brinell Hardness (H) 102 331
Modulus of Elasticity (ksi) (E): 29600
Machineability General Index: 12%

 

Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 0Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 1Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 2 

FAQ
Q1: What product information do I need to provide?

A1: You need to provide the grade, width, thickness, coating and the number of tons you need to purchase.
Q2: How long will it take to execute my order?
A2: Delivery time of stock products: 3-7 days after payment. Custom product delivery time: 20-45 days after payment.


Q3: Can I have a sample for testing?
A3: The cost of the samples is according to the value. The cost of the freight is necessary.

Q4: Do you have inspection for the products before packing?
A4: All products have to go through three checks in the whole manufacturing process,it includes production and Random Testing in warehouse and Before Shipping.and accept the third party inspection .

Q5: Can I get your best price?
A5: Price is different based on steel grade, size and quantity.Our goal is to provide you the best price with great quality
assured in a long run.Please leave your contact information for the includes production.we will get back to you with the best solutions as soon as we can.Please give those info, for price checking.If the required is sheet metal fabrication, please send drawing.

Q6:How to order?
A6: Buyer sends the inquiry --> Buyer gets the quotation-->Order confirmation-->Buyer send the deposit-->Seller prepares

Q7:what kind of payment does your company support?
A7: T/T, L/C at sight, are all accepted.

 

products
PRODUCTS DETAILS
Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169
MOQ: 100KGS
Price: 15.7 USD/KG
Standard Packaging: Wooden Box Wooden Pallet
Delivery Period: 7 Days
Payment Method: L/C, T/T
Supply Capacity: 80000KGS
Detail Information
Place of Origin
China
Brand Name
TSING SHAN
Certification
ISO MTC SGS
Model Number
718 GH4169
Tolerance:
±1%
Special Use:
Compressor Disks,machine Manufacturing
Young'S Modulus:
205 GPa
Curie Point:
-319℉ (-195℃)
Standard:
ASTM, JIS, AISI, EN, GB
Executive Standard:
ASTM
Wire:
MIG
Hardness:
170 HB
Type:
Nickel Bar
Melting Point:
1350-1400°C
Elongation At Break:
45%
Surface Treatment:
Anodized,Brushed,Mill Finished,Polished
Delivery State:
Sosoloid
Packing:
Standard Export Packing
Minimum Order Quantity:
100KGS
Price:
15.7 USD/KG
Packaging Details:
Wooden Box Wooden Pallet
Delivery Time:
7 Days
Payment Terms:
L/C, T/T
Supply Ability:
80000KGS
Highlight

GH4169 Nickel Alloy Round Bar

,

UNS N07718 Nickel Alloy Round Bar

Product Description

Nickel Alloy 718 Round Bar 718 Nickel AlloyInconel 718 round Bar W. Nr. 2.4668 UNS N07718 GH4169 Black and Bright Bar

 

Nickel Alloy 718 (INCONEL® 718) | UNS# N07718

Nickel 718 (UNS# N07718), or Inconel 718 is a precipitation hardening nickel-chromium alloy that contains molybdenum, iron, columbium, and smaller traces of aluminum and titanium. Designed to exhibit significant yields, high strength, good ductility, and creep rupture properties up to 1300°F (704°C). These characteristics provide alloy 718 good formability, weldability, and cryogenic allowances compared to the metals other nickel based superalloys. The sluggish age hardening characteristics in alloy 718 also allow annealing and welding without the occurrence of spontaneous hardening during heating and cooling. This alloy is also non-magnetic, maintains significant corrosion and oxidation resistances and can be used in applications like jet engines, airframe components, and high temp bolts and fasteners.

Nickel Alloy 718 Inventory Size Range:

718 Nickel Alloy Round Bar Specifications:

Common Names:

  • ATI 718
  • Haynes 718
  • INCONEL® Alloy 718

Nickel Alloy 718 Applications:

  • Jet engines
  • Rotor Bolts
  • Gas turbine operations
 

DISCLAIMER: Alloy data sheets are for reference only, not for design purposes.

Chemical Composition

  C Mn Fe P S Si Cu Ni Co Al Ti Cr Nb+Ta Mo
Inconel 600 ≤0.15 ≤1.0 6.0-10.0 ≤0.015 ≤0.015 ≤0.5 ≤0.5 ≥72.0 -- -- -- 14.0-17.0 -- --
Inconel 601 ≤0.1 ≤1.5 balance ≤0.02 ≤0.015 ≤0.5 ≤1.0 58.0-63.0 -- 1.0-1.7 -- 21.0-25.0 -- --
Inconel 625 ≤0.1 ≤0.5 ≤5.0 ≤0.015 ≤0.015 ≤0.5 -- ≥58.0 ≤1.0 ≤0.4 ≤0.4 20.0-23.0 3.15-4.15 8.0-10.0
Inconel 617 0.05-0.15 ≤1.0 -- ≤0.012 ≤0.015 ≤1.0 ≤0.5 ≥44.5 10.0-13.0 0.8-1.5 ≤0.6 20.0-24.0 -- 8.0-10.0
Inconel 690 ≤0.05 ≤0.5 7.0-11.0 -- ≤0.015 ≤0.5 ≤0.5 ≥58.0 -- -- -- 27.0-31.0 -- --
Inconel 718 ≤0.08 ≤0.35 balance ≤0.015 ≤0.015 ≤0.35 ≤0.3 50.0-55.0 ≤1.0 0.2-0.8 0.65-1.15 17.0-21.0   2.8-3.3
Inconel 725 ≤0.03 ≤0.35   ≤0.015 ≤0.010 ≤0.20   55.0-59.0       19.0-22.5   7.0-9.5
Inconel 750 ≤0.08 ≤1.0 5.0-9.0 -- ≤0.01 ≤0.5 ≤0.5 ≥70.0 ≤1.0 0.4-1.0 2.25-2.75 14.0-17.0 0.7-1.2 --
Inconel 20 ≤0.07 ≤2.0 balance ≤0.045 ≤0.035 ≤1.0 3.0-4.0 32.0-38.0 -- -- -- 19.0-21.0 8*C-1 2.0-3.0
Inconel 28 ≤0.02 ≤2.5 balance ≤0.02 ≤0.015 ≤1.0 0.6-1.4 30.0-34.0       26.0-28.0   3.0-4.0
Inconel 925 ≤0.03 ≤1.0 balance ≤0.03 ≤0.03 ≤0.5 1.5-3.0 42.0-46.0 -- 0.15-0.5 1.9-2.4 19.5-23.5 -- 2.5-3.5
Inconel 926 ≤0.02 ≤2.0 balance ≤0.03 ≤0.01 ≤0.5 0.5-1.5 24.0-26.0 -- -- -- 19.0-21.0 -- 6.0-7.0
Inconel 825 ≤0.05 ≤1.0 balance ≤0.02 ≤0.03 ≤0.5 1.5-3.0 38.0-46.0 -- ≤0.2 0.6-1.2 19.5-23.5 -- 2.5-3.5
Inconel 800 ≤0.1 ≤1.5 balance -- ≤0.015 ≤1.0 ≤0.75 30.0-35.0 -- 0.15-0.6 0.15-0.6 19.0-23.0 -- --
Inconel 800H 0.05-0.1 ≤1.5 balance   ≤0.015 ≤1.0 ≤0.75 30.0-35.0 -- 0.15-0.6 0.15-0.6 19.0-23.0 -- --
Inconel 800HT 0.06-0.1 ≤1.5 balance   ≤0.015 ≤1.0 ≤0.75 30.0-35.0   0.15-0.6 0.15-0.6 19.0-23.0    

 

PHYSICAL PROPERTIES
Density Electrical conductivity (% IACS) Thermal conductivity (BTU-in/hr-ft²-°F) Specific heat (BTU/lb-°F) Thermal expansion (1/°F) Thermal expansion Melting Point (°F)
0.296 1.38 77 0.104 7.22E-06 2300

 

 

 

MECHANICAL PROPERTIES
PROPERTY MINIMUM MAXIMUM
Yield Strength Range (Rp0.2 Offset) (ksi) 80 150
Tensile Strength Range (Rm) (ksi) 14 220
Elongation (AL=5 x Ø) 18% 27%
Brinell Hardness (H) 102 331
Modulus of Elasticity (ksi) (E): 29600
Machineability General Index: 12%

 

Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 0Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 1Nickel Alloy 718 Round Bar 718 Nickel Alloy W. Nr. 2.4668 UNS N07718 GH4169 2 

FAQ
Q1: What product information do I need to provide?

A1: You need to provide the grade, width, thickness, coating and the number of tons you need to purchase.
Q2: How long will it take to execute my order?
A2: Delivery time of stock products: 3-7 days after payment. Custom product delivery time: 20-45 days after payment.


Q3: Can I have a sample for testing?
A3: The cost of the samples is according to the value. The cost of the freight is necessary.

Q4: Do you have inspection for the products before packing?
A4: All products have to go through three checks in the whole manufacturing process,it includes production and Random Testing in warehouse and Before Shipping.and accept the third party inspection .

Q5: Can I get your best price?
A5: Price is different based on steel grade, size and quantity.Our goal is to provide you the best price with great quality
assured in a long run.Please leave your contact information for the includes production.we will get back to you with the best solutions as soon as we can.Please give those info, for price checking.If the required is sheet metal fabrication, please send drawing.

Q6:How to order?
A6: Buyer sends the inquiry --> Buyer gets the quotation-->Order confirmation-->Buyer send the deposit-->Seller prepares

Q7:what kind of payment does your company support?
A7: T/T, L/C at sight, are all accepted.