GH3128 Alloy Bar
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GH3128 Alloy Bar

GH3128 alloy comprehensive performance is better than the similar GH3128 and GH3536 nickel-based solidamalgamation of gold. Suitable for manufacturing of long-term work under 950 ℃ of aircraft engine combustor flame tube, afterburner shell, regulation and other high temperature parts, main products are cold rolled sheet, also can supply hot rolled plate, bar, forging, wire and tube.
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As a leading supplier and manufacturer in China, GNEE Steel provides cost-effective nickel-based alloy products.

Product Introduction

Nickel alloy GH3128 (GH128) is a nickel-based alloy that is solid solution strengthened with tungsten and molybdenum and grain boundary strengthened with boron, cerium and zirconium. It has high plasticity, high permanent creep strength, and good oxidation resistance, stamping and welding properties. Its comprehensive performance is superior to similar nickel-based solid solution alloys such as GH3044 and GH3536.

Chemical composition(mass fraction)(wt.%) of the GH3128

Elements Min.(≥) Max.(≤) Similar Remarks
C - 0.05    
Cr 19.0 22.00    
Mo 7.50 9.00    
Ni - Remainder    
W 7.50 9.00    
Al 0.40 0.80    
Ti 0.40 0.80    
Fe - 2.0    
Si - 0.80    
Mn - 0.50    
P - 0.013    
S - 0.013    
B - 0.005    
Ce - 0.05    
Zr - 0.06    

Mechanical properties of grade GH3128

Yield
Rp0.2 (MPa)
Tensile
Rm (MPa)
Impact
KV (J)
Elongation
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition HBW
353 (≥) 944 (≥) 43 13 24 Solution and Aging, Annealing, Ausaging, Q+T,etc 131

Physical properties of grade GH3128

Property Density
kg/dm3
Temperature T
°C/F
Specific heat
J / kgK
Thermal conductivity
W/mK
Electric resistance
µΩ·cm
725 (≥) 725 (≥) 13 43 22 Solution and Aging, Annealing, Ausaging, Q+T,etc
Temp.
°C/°F
Creep strain limit
(10000h)
(Rp1,0) N/mm2
Creep rupture strength
(10000h)
(Rp1,0) N/mm2
- - -
445 949 944 - - -

superalloy

superalloy gH3128 Bar Process performance and requirements

1. The furnace temperature during ingot forging is not higher than 700℃, and the final forging temperature is greater than 900℃.

2. The average grain size of the alloy is closely related to the degree of deformation of the forging and the final forging temperature.

3. The alloy can be welded by argon arc welding, spot welding, seam welding and other methods.

Package&delivery

SuperAlloys GH3128

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