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High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine

Product Details

Place of Origin: China

Brand Name: Victory

Certification: CE,ROHS,ISO 9001

Model Number: GH3128

Document: Product Brochure PDF

Payment & Shipping Terms

Minimum Order Quantity: 5 Kg

Price: Negotiable

Packaging Details: Spool package with Carton box, Coil package with polybag

Delivery Time: 5-21 days

Payment Terms: L/C, T/T, Western Union, MoneyGram

Supply Ability: 300 tons per month

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Product Details
Highlight:

High Temperature Alloy GH3128 Wire

,

Aircraft Engine High Temperature Alloy

,

High Plasticity GH3128 Wire

Product Name:
GH3128 Wire
Density:
8.81 G/cm³
Melting Point:
1340~1390℃
Tensile Strength:
690 MPa
Yield Strength:
270 MPa
Application:
Aerospace, Petrochemical, Heat Treatment Industry
Product Name:
GH3128 Wire
Density:
8.81 G/cm³
Melting Point:
1340~1390℃
Tensile Strength:
690 MPa
Yield Strength:
270 MPa
Application:
Aerospace, Petrochemical, Heat Treatment Industry
Product Description

Introduction:


GH3128 (GH128) is a nickel-based alloy solid solution reinforced with tungsten and molybdenum and grain boundaries reinforced with boron, cerium and zirconium. It has high plasticity, high lasting creep strength, good oxidation resistance and stamping, welding and other properties. . Its comprehensive performance is better than similar nickel-based solid solution alloys such as GH3044 and GH3536. It is suitable for manufacturing combustion chamber flame tubes, afterburner casings, regulator plates and other high-temperature parts of aeroengines that operate at 950°C for a long time. The main products are cold-rolled sheets, and hot-rolled plates, bars, etc. can also be supplied. Forgings, wire and tubing.

 

Parameter:


Chemical Composition ( % )
Brand C Si Mn S P Cr Co W Mo Ti Al Fe Ni other
Less than
GH3128 0.05 0.8 0.5 0.013 0.013 19~22 7.5~9 7.59 0.40.8 0.40.8 ≤2.0 rest B≤0.005
Ce≤0.05
Zr≤0.06

 

 

 

The minimum mechanical properties of the alloy at room temperature
Brand heat treatment tensile strength
RmN/mm²
Yield strength
Rp0.2N/mm2
Elongation
As%
Brinell hardness
HB
Rockwell hardness
HRC
GH3128 solid solution 750   40  

 

  • Thermal conductivity
θ/℃
100
200
300
400
500
600
700
800
900
950
λ/(W/(m·C))
11.30
12.56
14.24
15.49
16.75
18.42
19.68
21.35
23.02
23.86

 

 

  • Linear expansion coefficient
θ/℃
18~100
18~200
18~300
18~400
18~500
18~600
18~700 
18~800
18~900
18~1000
α/10-6C-1
11.25
11.86
12.68
12.80
13.37
13.68
14.46
15.19
15.66
15.29

 

 

Characteristic:


  • High temperature strength: GH3128 wire has excellent high temperature strength and can maintain high mechanical properties in high temperature environments.
  • Antioxidant properties: It exhibits good antioxidant properties and can resist oxidation and corrosion at high temperatures.
  • Creep resistance: GH3128 wire has good creep resistance and can withstand long-term continuous loading at high temperatures without deformation.
  • Anti-corrosion properties: It has good anti-corrosion properties in many corrosive media, including acidic, alkaline and chloride environments.

 

Specific application areas:


  1. Aeroengine combustion chamber flame tube, afterburner housing, regulator plate
  2. Structural parts of gas turbine combustion chamber
  3. Turbine engine combustion chamber parts
  4. Afterburner parts
High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine 0 High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine 1

 

contact us

email:victory@dlx-alloy.com

Oem service:
Welcome customized size
We are experience factory for OEM&ODM service

 

Process performance and requirements:


The alloy has a single-phase austenite structure in the solid solution state and contains a small amount of fine and evenly distributed TiN and M6C.

1. The furnace temperature for steel ingot forging should not be higher than 700°C, and the final forging temperature should be higher than 900°C.
2. The average grain size of the alloy is closely related to the deformation degree and final forging temperature of the forging.
3. Alloys can be welded by argon arc welding, spot welding, seam welding and other methods.