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LJ
Product Description:
We can produce Steel sleeve for winding non-ferrous sheet and strip of various materials
and models according to customer needs.
Max length | 3000mm |
Max weight | 15000kg |
Application | Industrial Equipment and Mechinique Equipment |
Processing | Forging+machining+heating Treatment |
Design Support | Pro-E, UG,SolidWorks,AutoCad, PDF |
Heat treatment | N,N+T,Q+T or as customer's requirement |
Material:
GH3536 has good antioxidant and corrosion resistance, and has a medium -end and peristaltic intensity below
900 ° C. Cold, thermal processing formability and welding performance are good. The combustion room components and other high temperature components that are suitable for manufacturing aviation engines are used for a long time below 900 ° C. The short -term operating temperature reaches 1080 ° C. A alloys that can withstand certain stress and have antioxidant or corrosion capacity at 600 to 1200 ° C. According to the matrix elements, it can be divided into iron -based high -temperature alloys, nickel -based high -temperature alloys and cobalt -based high -temperature alloys. According to the preparation process, it can be divided into deformed high -temperature alloys, cast high temperature alloys and powder metallurgy and high temperature alloys. There are solid -soluble enhancement, precipitated reinforcement type, oxide diffuse enhancement, and fiber reinforcement type (see metal enhancement). High -temperature alloys are mainly used to make high -temperature components such as aviation, ships and industrial gas turbines, guided blades, turbine disks, high -pressure gas disks, and combustion rooms (Figure 1); it is also used to manufacture aerospace aircraft, rocket engines, nuclear reactors, and Energy conversion devices such as petrochemical equipment and coal conversion.
Chemical Composition(%)
C | Si | Mn | P | S | Cr | Ni | Mo |
0.05-0.15 | 1.00 | 1.00 | 0-0.25 | 0.015 | 20.5-23.00 | Bal | 8.00-10.00 |
W | Cu | Co | B | Nb | Al | Ti | Fe |
0.20-1.00 | ≦0.500 | 0.50-2.50 | ≦0.010 | - | ≦0.50 | ≦0.15 | 17.00-20.00 |
Mechanical Property
Yield Strength (Mpa) | Tensile Strength (Mpa) | Impact KV/Ku (J) | Elongation A(%) | Reduction Z(%) | As-Heat-Treated Conditin | Brinell Hardness (HBW) |
≧144 | ≧274 | 44 | 32 | 14 | Solution and Aging,Annealing, Ausaging,Q+T,etc | 233 |
Product Description:
We can produce Steel sleeve for winding non-ferrous sheet and strip of various materials
and models according to customer needs.
Max length | 3000mm |
Max weight | 15000kg |
Application | Industrial Equipment and Mechinique Equipment |
Processing | Forging+machining+heating Treatment |
Design Support | Pro-E, UG,SolidWorks,AutoCad, PDF |
Heat treatment | N,N+T,Q+T or as customer's requirement |
Material:
GH3536 has good antioxidant and corrosion resistance, and has a medium -end and peristaltic intensity below
900 ° C. Cold, thermal processing formability and welding performance are good. The combustion room components and other high temperature components that are suitable for manufacturing aviation engines are used for a long time below 900 ° C. The short -term operating temperature reaches 1080 ° C. A alloys that can withstand certain stress and have antioxidant or corrosion capacity at 600 to 1200 ° C. According to the matrix elements, it can be divided into iron -based high -temperature alloys, nickel -based high -temperature alloys and cobalt -based high -temperature alloys. According to the preparation process, it can be divided into deformed high -temperature alloys, cast high temperature alloys and powder metallurgy and high temperature alloys. There are solid -soluble enhancement, precipitated reinforcement type, oxide diffuse enhancement, and fiber reinforcement type (see metal enhancement). High -temperature alloys are mainly used to make high -temperature components such as aviation, ships and industrial gas turbines, guided blades, turbine disks, high -pressure gas disks, and combustion rooms (Figure 1); it is also used to manufacture aerospace aircraft, rocket engines, nuclear reactors, and Energy conversion devices such as petrochemical equipment and coal conversion.
Chemical Composition(%)
C | Si | Mn | P | S | Cr | Ni | Mo |
0.05-0.15 | 1.00 | 1.00 | 0-0.25 | 0.015 | 20.5-23.00 | Bal | 8.00-10.00 |
W | Cu | Co | B | Nb | Al | Ti | Fe |
0.20-1.00 | ≦0.500 | 0.50-2.50 | ≦0.010 | - | ≦0.50 | ≦0.15 | 17.00-20.00 |
Mechanical Property
Yield Strength (Mpa) | Tensile Strength (Mpa) | Impact KV/Ku (J) | Elongation A(%) | Reduction Z(%) | As-Heat-Treated Conditin | Brinell Hardness (HBW) |
≧144 | ≧274 | 44 | 32 | 14 | Solution and Aging,Annealing, Ausaging,Q+T,etc | 233 |
Inspection:
Inspection: