• Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
  • Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
  • Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
  • Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
  • Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
  • Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /

Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /

Application: Industrial
Standard: GB, ASTM
Purity: >99.5%
Alloy: Alloy
Powder: Not Powder
Transport Package: Wooden
Customization:
Gold Member Since 2016

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Manufacturer/Factory

Basic Info.

Model NO.
XD-89
Origin
Jiangsu Baoying
HS Code
7505120000
Production Capacity
500ton/Year

Product Description

GH2302 Overview
GH2302 is an iron-nickel-chromium-based age-hardening high-temperature alloy. When used for a long time at a working temperature below 700 °C, its structure and performance are stable, and it can reach 850 °C for a short time. Turbine parts, this alloy has good cold and hot formability and can be supplied in bar, sheet and casting.

GH2032 technical standard
GB/T 14992-1994 "Superalloy Grades"

GB/T 14993-1994 "Superalloy Hot-Rolled Bars for Rotating Parts"

GB/T 14995-1994 "Superalloy Hot Rolled Steel Plate"

GJB 1952-1994 "Specification for cold-rolled sheet of superalloy for aviation use"

YB/T5248-1993 "Casting Superalloy Master Alloy"

GH2302 Chemical composition

C: ≤0.08

Cr: 12.00-16.00

Ni38.00-42.00

Mo: 1.50-2.50

W3.50-4.50

Al: 1.80-2.30

Ti: 2.30-2.80

Fe: surplus

Si: ≤0.60

Mn: ≤0.60

P≤0.020

S:≤0.010

B:≤0.010

Zr≤0.050

Ce: ≤0.020


GH2302 Heat Treatment System
1180ºC±10ºC, 2h, air cooling 1050ºC±10ºC, 4h, air cooling+800ºC±10ºC, 16h, air cooling. Plate: 1100-1130ºC, air-cooled (when testing the performance, the sample must be aged, and its specification is: 800ºC±10ºC, 16h, air-cooled). Casting: 1100ºC, 3-5h, air cooling +800ºC, 16h, air cooling.

GH2302 Variety Specifications and Supply Status
Hot-rolled bars below d 55mm can be supplied without heat treatment: cold-rolled sheets with δ0.5-4mm and hot-rolled medium plates with δ4-14mm, delivered in solution treatment state. We can supply master alloys for castings, cast turbine rotor blades and guide vanes, and cast integral turbines.

GH2302 Melting and casting process
Vacuum induction melting plus electroslag or vacuum arc remelting process is adopted. The cast master alloy is melted by vacuum induction, and then remelted and poured by vacuum induction.

GH2302 application overview and special requirements
Manufacture of turbojet engine afterburner plate parts and components, as well as industrial gas turbine blades and other parts. It is difficult to contact welding the plate, and attention should be paid to the appropriate joining process.
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Company Profile
Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
Test Equipment :
Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
Company strength:
Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
Certificate:

 Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /Gh302/Jf-43 / K232 / K32 / Iron Nickel Chromium Base Superalloy / Gh2302 /
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Our products sales all over the world as well. From the following two websites you can also get more information about our company:
http://xingda-alloy.en.made-in-china.com
http://xingda-alloy.en.made-in-china.com
 
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