Brand	GH2696
Similar brands	GH696 GH696M
Technicalstandard	GJB 2611-1996 《Specification for cold rolled superalloy strip for aircraft》 GJB 3318—1998《Specification for cold rolled superalloy strip for aircraft》 HB 5463—1990 《Hot rolled and forged bars of GH696 alloy》 HB 5464—1990 《GH696 alloy cold-drawn bar》 HB 5465一1990《GH696 alloy cold rolled sheet》
Classification	Special alloy steel
Label	Iron-based superalloy
Explain	GH2696 is a Fe-Ni-Cr based precipitation hardening deformation superalloy, which is comprehensively strengthened with a small amount of titanium, aluminum, molybdenum and trace boron. It has high yield strength, endurance and creep strength below 650 ℃, as well as good high-temperature elastic property, gas corrosion resistance and processing plasticity. It is suitable for manufacturing turbine and compressor fasteners, discs and working blades, turbine shells, annular parts (including connecting rings) that work under 650 ℃ for a long time, as well as good machining and welding performance, and cylindrical spiral springs that work at 400-650 ℃. The short-term working temperature of the alloy can reach 750 ℃. It is widely used in manufacturing various high-temperature parts of aircraft engines and has long-term and reliable experience. This kind of alloy is used to manufacture various parts such as quick-action coil, fastener, spring, pipe joint, various engine devices, and supports.
Density	7.93g/cm³

Chemical composition:%

Note: The above information is for reference only. Some elements in different standards and specifications may be different.

The information of the above materials is rough description, and any deviation may be used for reference only

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Shanghai Timmco Special Alloy Co., Ltd