Specification for alloy structural steel rods for aero-engine gears (English Version)
GJB 9451-2018 is a national military standard, led by the Metallurgical Industry Information Standards Research Institute and jointly formulated by seven units including Northeast Special Steel Group. The standard specifies the technical indicators of four special alloy steel bars, including 16Cr3NiWMoVNbE, in response to the extreme working conditions of aircraft engine gears.
Grade | Applicable diameter(mm) | Smelting process | Tensile strength(MPa) | Impact energy(J) |
---|---|---|---|---|
16Cr3NiWMoVNbE | ≤200 | Vacuum induction+Electroslag/Consumable | ≥1270 | ≥51 |
16Ni3CrMoE | ≤200 | Vacuum induction+Electroslag/Consumable | 1180-1380 | ≥30 |
The standard stipulates that 16Cr3NiWMoVNbE must adopt the vacuum induction + vacuum consumable dual process to ensure the purity of the material. The oxygen content must be controlled below 15ppm, and the sulfur and phosphorus content must be ≤0.010%.
Take 16CrNi4MoA as an example, after 920℃ normalizing + 650℃ tempering treatment:
Use the tower test method, the total length of each step hairline is ≤10mm, and the maximum length of a single hairline is ≤6mm. For key components, hairline-free steel may be required.
Diameter Range (mm) | Testing Standard | Allowable Defects |
---|---|---|
≤60 | GB/T 4162 AA Grade | ≤Φ1.2mm Flat Bottom Hole |
>60 | GB/T 4162 A Grade | ≤Φ1.5mm Flat Bottom Hole |
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