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Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C

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Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C

China Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C supplier
Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C supplier Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C supplier

Large Image :  Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C

Product Details:

Place of Origin: China
Brand Name: XUNSHI
Certification: ISO9001
Model Number: GH4145

Payment & Shipping Terms:

Minimum Order Quantity: 50kg
Price: Negotiable
Packaging Details: Plywood case
Delivery Time: 30-35 days
Payment Terms: T/T
Supply Ability: 1000k per week
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Detailed Product Description
Equal Grades: Inconel X-750, NiCr15Fe7TiAl, 2.4669,UNS N07750 Melting Range: 1395°C~1425°C
Density: 8.25g/cm3 Forms Of Supply: Plate, Strip, Bar, Forging, Ring, Wire, Tube
Spec: GB/T 14992 Product Name: Nickel Cobalt Alloy

GH4145 Nickel Alloy Precipitation-hardened Superalloy up to 800°C Application

 

GH4145 is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures up to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. GH4145 also has excellent properties down to cryogenic termperatures.

Depending on the application and the properties desired, various heat treatments are employed. For service above 1100°F, particularly where loads are to be sustained for long times, optimum properties are achieved by solution treating (2100°F) plus stabilization treating (1550°F) plus precipitation treating (1300°F). For service below 1100°F, the alloy may be strengthened by precipitation treating after hot or cold working or by precipitation treating after equalizing or solution treating. A furnace-cooling treatment is also used to develop optimum properties for some applications.

 

Chemical compositin

Element C Cr Ni Co Al Ti Fe Nb Mn Si S P Cu
Weight(%) 0.08 max 14.00~17.00 70.00 min 1.00 max 0.40~1.00 2.25~2.75 5.00~9.00 0.70~1.20 1.00 max 0.50 max 0.010 max 0.015 max 0.50 max

 

Features

  •  Good creep rupture strength at high temperatures
  •  Not as strong as Nimonic 90
  •  Very good at cryogenic temperatures
  •  Age hardenable
  •  High temperature dynamic applications

Applications

  •  Nuclear reactors
  •  Gas turbines
  •  Rocket engines
  •  Pressure vessels
  •  Aircraft structures

 

 

Available Product Forms
Sheet, strip, plate, round bar, flat bar, forging stock, hexagon, wire, tube and extruded

Aircraft Structures Nickel Based Superalloys Precipitation Hardened GH4145 800°C 0

Contact Details
Suzhou Xunshi New Material Co., Ltd

Contact Person: Allen Sun

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