GH2132 High-temperature Alloy Plate For Aircraft Blades
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GH2132 High-temperature Alloy Plate For Aircraft Blades

Grade: GH2132
Surface Treatment: Hot-rolled sheet (HR)
Form: Sheet, plate, coil
Hardness: Soft, hard, semi-hard
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As a leading supplier and manufacturer in China, GNEE Steel provides cost-effective nickel-based alloy products.

Product Introduction

GH2132 high-temperature alloy plate for aircraft blades description

GH2132 high-temperature alloy plate for aircraft blades

GNEE GH2132 high-temperature alloy plate for aircraft blades

 

GH2132 (also known as UNS S66286 or A-286) is a widely used iron-based precipitation-strengthened superalloy known for its excellent performance in high-temperature aerospace applications, particularly suitable for components such as turbine and compressor discs, rotor blades, and fasteners operating at temperatures up to approximately 650°C.

GH2132, also known as Inconel 713C, is a high-temperature alloy typically supplied in various forms, including plates and sheets. The properties of GH2132 plates and sheets are similar to those of the GH2132 tubing mentioned earlier, exhibiting excellent high-temperature strength, oxidation resistance, and creep resistance.

 

High-Temperature Strength: GH2132 plates and sheets maintain their strength and mechanical properties even at high temperatures, making them suitable for applications requiring resistance to thermal stress.

 

Oxidation Resistance: GH2132 possesses excellent oxidation and corrosion resistance, which is crucial in high-temperature environments where it is frequently exposed to gases and combustion products.

 

GH2132 Production Execution Standards

Standard Type Chemical Composition Bar Stock Forging Plate/Sheet Wire Pipe/Tube
National Standard (China) GB/T 14992 GB/T 14994
GB/T 14993
GB/T 14997
GB/T 14998
GB/T 14995
GB/T 14996
- GB/T 15062
Aviation Industry Standards - HB 5189 - - - -
Military Standards (China) - GJB 2611
GJB 3165
GJB 3020
GJB 3782
- GJB 2612
GJB 3167
-

 

Specification Of GH2132 high-temperature alloy plate for aircraft blades

 

Grade GH2132
Standard ASTM B463 / ASME SB463
Thickness 0.1mm To 100 mm
Size 1000 mm x 2000 mm, 1220 mm x 2440 mm, 1500 mm x 3000 mm, 2000 mm x 2000 mm, 2000 mm x 4000 mm
Finish Hot rolled plate (HR), Cold rolled sheet (CR), 2B, 2D, BA NO(8), SATIN (Met with Plastic Coated)
Form Sheets, Plates, Coils, Slatting Coils, Perforated Coils, Foils, Rolls, Plain Sheet, Shim Sheet, Strip, Flats, Blank (Circle), Ring (Flange)
Hardness Soft, Hard, Half Hard, Quarter Hard, Spring Hard etc.
Applications Off-Shore Oil Drilling Companies, Power Generation, Petrochemicals, Gas Processing, Specialty Chemicals, Pharmaceuticals, Pharmaceutical Equipment, Chemical Equipment, Sea Water Equipment, Heat Exchangers, Condensers, Pulp and Paper Industry

 

GH2132 high-temperature alloy plate for aircraft blades Specification

 

GH2132 - UNS S66286 High Temperature Alloy Chemical Composition

Cr Ni Mo Co Va Al Ti B C Fe Mn Si P S
Min 13.5 24 1 0.1 1.9 0.003
Max 16 27 1.5 1 0.5 0.35 2.35 0.01 0.08 Balance 2 1 0.025 0.025

 

GH2132 - UNS S66286 High Temperature Alloy Equivalent Grades

STANDARD WERKSTOFF NR. UNS GOST AFNOR JIS BS EN OR
GH2132/ A-286 1.4980 S66286

 

GH2132 - UNS S66286 High Temperature Alloy Mechanical Properties

Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
7.94 g/cm3 1430 °C (2600 °F) 550-1300Mpa 350-750Mpa2 25%

 

application Of GH2132 high-temperature alloy plate for aircraft blades

 

GH2132 High-Temperature Alloy Plate For Aircraft Blades

The GH2132 is specifically designed for high-temperature bearing components in aero engines, suitable for components operating at medium to high temperatures (below 650°C - 700°C):

Rotors and turbine blades

Turbine disks and compressor disks

Fasteners and structural components

Afterburner components

 

GH2132 high-temperature alloy plate for aircraft blades production process

  • Annealing process
    Gnee Steel
    Annealing process
  • Hot rolling process
    Gnee Steel
    Hot rolling process
  • Cold drawing process
    Gnee Steel
    Cold drawing process
  • Solution + aging process
    Gnee Steel
    Solution + aging process

Gnee Steel provides the following heat treatments for High-temperature GH2132 alloy tubing for aero engines: annealing, solution + aging. In addition, Gnee Steel also provides hot working and cold working, which are hot rolling and cold drawing.

 

GH2132 high-temperature alloy plate for aircraft blades Packaging 

 

1. Packaging is crucial, especially in international shipping, where goods undergo multiple stages to reach their final destination; therefore, we place great emphasis on packaging.

2. Gnee Steel employs various packaging methods depending on the product. For example, we use multiple packaging methods...

 

 

About Gnee Steel

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About Gnee Steel

Gnee Steel specializes in the production and sale of various nickel-based alloys, including Nickel 201, Nickel 202, Hastelloy C-276, Hastelloy C-22, Hastelloy B, Hastelloy C-4, Inconel Alloy 600, Inconel 625, Inconel 718, Inconel X-750, Incoloy Alloy 800, Incoloy 800H/HT, Incoloy 825, Monel Alloy 400, Monel K500, and high-temperature alloys. Gnee Steel's products are widely used in aerospace, chemical, electric power, automotive, and nuclear energy applications. We also offer customized alloy solutions tailored to customer needs. For alloy pricing inquiries or customized alloy solutions, please contact us for a quote at ss@gneesteel.com.

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