一种局部双层曲面超塑成形 / 扩散连接零件成形方法

By employing a local double-layer curved surface superplastic forming/diffusion bonding method, the problems of large milling volume, uneven thickness, and multiple thermal cycles in parts have been solved, achieving efficient forming and quality control of parts while reducing processing difficulty and cost.

CN120421929BActive Publication Date: 2026-07-17AVIC XIAN AIRCRAFT IND GRP CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AVIC XIAN AIRCRAFT IND GRP CO LTD
Filing Date
2025-06-13
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies for processing locally double-layer curved surface superplastic forming/diffusion connection parts suffer from problems such as large milling volume, uneven thickness, poor positional accuracy, and high manufacturing costs, and require multiple thermal cycles and manual finishing.

Method used

The local double-layer curved surface superplastic forming/diffusion bonding method is adopted. Through CNC milling, pre-forming, anti-weld flux coating, gas circuit welding, diffusion bonding and superplastic forming, a one-time thermal cycle forming is achieved. The diffusion bonding area is controlled and formed by gas pressure and mechanical pressure.

Benefits of technology

This achieves uniform pressure on the surface of parts, reduces mold closing requirements, simplifies processing, improves product quality, and reduces manufacturing cycle and cost.

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Abstract

本发明属于热成形加工制造技术领域,具体涉及一种局部双层曲面超塑成形 / 扩散连接零件成形方法,所述方法包括以下步骤:步骤1:数控铣切下料,按照构件尺寸要求切割毛料获得板料,板料包括底板料和加强梗板料,加强梗板料在厚度铣切区铣切材料至0.3mm;步骤2:预成形,得到的预成形加强梗和预成形底板;步骤3:蒙皮止焊剂涂覆,酸洗去油,然后在所述预成形加强梗和预成形底板内侧除扩散焊接区外的所有区域涂覆止焊剂;步骤4:气路焊接;步骤5:扩散连接,采用气体压力加机械压力的方式;步骤6:超塑成形,采用气体压力加机械压力的方式;步骤7:降温取件。本发明提供的方法仅需一次热循环即可成形出零件,打磨简单,厚度均匀。
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