GH2132 High-temperature Alloy Plate For Aircraft Blades
Surface Treatment: Hot-rolled sheet (HR)
Form: Sheet, plate, coil
Hardness: Soft, hard, semi-hard
As a leading supplier and manufacturer in China, GNEE Steel provides cost-effective nickel-based alloy products.
- Send E-mail: ss@gneesteel.com
- Tel: +8615824687445
GH2132 high-temperature alloy plate for aircraft blades description

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

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
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

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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