Magnesium alloy annular part and preparation method thereof
Through the processes of double-stage uniformization treatment, multi-directional forging, punching and reaming forging, ring rolling forming and aging treatment, the defects in the preparation of large-diameter VW93M magnesium alloy ring parts are solved, and high strength and heat resistance are improved, and lightweight equipment is suitable for aerospace.
Patent Information
- Application Number
- CN202411911991.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-24
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2044-12-24
AI Technical Summary
When preparing large-diameter VW93M magnesium alloy ring parts, defects such as segregation, thermal cracking and surface cold separation are present, and the plastic deformation ability of the magnesium alloy is poor, resulting in poor mechanical properties and heat resistance.
High-strength, heat-resistant magnesium alloy ring parts are prepared by using the processes of double-stage homogenization, multi-directional forging, punching and reaming forging, ring rolling forming and aging treatment. The specific steps include: double-stage homogenization treatment with low temperature first and high temperature, multi-directional forging to eliminate casting defects, improve shape through punching and reaming forging, improve wall thickness uniformity by ring rolling, and eliminate internal stress and unevenness through aging treatment.
The high strength and heat resistance of magnesium alloy ring parts have been achieved, and the room temperature mechanical properties and 250℃ mechanical properties have been significantly improved. It is suitable for lightweight equipment in the aerospace field.