High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet

Product Details
Customization: Available
Application: Aviation, Electronics, Industrial, Medical, Chemical
Standard: JIS, GB, DIN, BS, ASTM, AISI
Still deciding? Get samples of US$ 0/Piece
Request Sample
Manufacturer/Factory, Trading Company
Gold Member Since 2024

Suppliers with verified business licenses

Audited Supplier

Audited by an independent third-party inspection agency

Fast Delivery
The supplier can deliver the goods within 15 days
Low MOQ
The MOQ for the supplier's products is 1
Customization from Samples
The supplier provides sample based customization services
R&D Capabilities
The supplier has 1 R&D engineers, you can check the Audit Report for more information
to see all verified strength labels (5)
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
  • High Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet
Find Similar Products

Basic Info.

Model NO.
GH3128
Sample
Free
Trade Terms
EXW, Fob, CIF, CFR
Surface
Mirror, Brushed, Mill Finished, Polished etc.
Transport Package
Standard Export Package
Specification
As Customer′s Request
Trademark
Mingson
Origin
China
HS Code
7506200000
Production Capacity
7000 Tons Per Year

Product Description

1.Product Name: High Temperature Alloy Plate/Sheet
2.Grade: GH3128
3.Thickness: 0.6mm-70mm, Length: 12000mm, Wide:≤2500mm
4.Features: High temperature alloy (GH3128), solid solution strengthened nickel-based alloy, it has good overall performance with high durable, also with high plasticity, high persistent creep strength, good oxidation resistance and stamping, welding and other performance.
5.Applications: 
  • aircraft engine combustion chamber flame cylinder, afterburner shell and regulating plate.
  • Structure of gas turbine combustion chamber.
  • Turbine engine combustion chamber components.
  • Afterburner parts.
6.Physical Properties
Density Melting Range
g/cm3 °C
8.81 1340-1390
7.Chemical Composition
% Ni Cr Mo W Fe Ti C Mn Si Al P S
MIN Balance 19 7.5 7.5 - 0.4 - - - 0.4 - -
MAX 22 9 9 2 0.8 0.05 0.5 0.8 0.8 0.013 0.013

 

High Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate SheetHigh Temperature Alloy Gh3128 Nickel-Based Alloy Plate Sheet




 

Send your message to this supplier

*From:
*To:
*Message:

Enter between 20 to 4,000 characters.

This is not what you are looking for? Post a Sourcing Request Now
Contact Supplier