Discretized stepped multilayer structure superplastic forming / diffusion bonding method
CN117124020BActive Publication Date: 2026-08-28SHENYANG AIRCRAFT CORP
Patent Information
- Application Number
- CN202310935343.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2023-07-28
- Publication Date
- 2026-08-28
- Estimated Expiration
- 2043-07-28
AI Technical Summary
Technical Problem
[0009]针对上述提出的传统SPF/DB制造过程中容易出现缺陷的问题,提出一种离散化梯度多层结构超塑成形/扩散连接方法
Benefits of technology
[0020]1.通过激光焊封焊方式替代传统氩弧焊密封口袋,密封效果好、效率高,大幅度减缓了板料的焊接变形;
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Figure CN117124020B_ABST
Abstract
The application discloses a discrete stepped multilayer structure superplastic forming / diffusion bonding method, and belongs to the field of metal sheet plastic forming. A split surface of a reinforcing block is reasonably designed according to the feature structure of a discrete reinforcing area of a part, and a milling and laser positioning welding process is adopted to realize assembly of the stepped multilayer structure of the reinforcing area before SPF / DB forming. The thickness specification of an outer skin is reasonably designed, the rigidity of the outer skin during SPF / DB forming is improved, and process compensation is performed on collapse and depression of the outer skin during forming. Finally, the precision of the part is improved through overall milling of the part after SPF / DB forming. Laser welding is adopted to replace argon arc welding to realize sealing between the inner skin and the outer skin. During diffusion bonding, an internal suction and external pressure mode is adopted, the inner and outer pressure difference is adjusted, the outer surface of the upper skin is adhered to a die, beneficial friction between the two is utilized, the elongation deformation amount of the outer skin is controlled, and depression defects caused in the superplastic process due to deformation growth of the outer skin in the diffusion process are inhibited.
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Citation Information
Patent Citations
Variable-thickness titanium alloy skin integrated forming method
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