A processing method of a semi-circular reference of a thin-walled sector structure part and a bushing
By using thermal calibration control and specialized fixture design, combined with reasonable cutting parameters and paths, the deformation and accuracy problems of the thin-walled semi-circular reference plane of the front sealing bushing of the aero-engine spindle during the machining process were solved, achieving efficient and high-precision machining results.
Patent Information
- Application Number
- CN202511414578.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2025-09-29
- Publication Date
- 2026-06-26
- Estimated Expiration
- 2045-09-29
AI Technical Summary
In the existing technology, the thin-walled semi-circular reference plane of the front sealing bushing of the aero-engine main shaft has the potential for deformation during the machining process. The clamping points and supports are not reasonable, and the effects of material springback and intermittent cutting cannot be effectively offset, resulting in low machining efficiency and difficulty in guaranteeing accuracy.
A thermal calibration process is adopted, and a special thermal calibration fixture and a finishing fixture are designed. The internal stress is released through thermal calibration, and the clamping rigidity is enhanced. Then, reasonable cutting parameters and combined tool paths are used for finishing to ensure the positioning and rigidity of the parts.
Effectively control part deformation, improve processing efficiency and precision, meet the manufacturing requirements of aero-engines for high-performance parts, and ensure high-quality forming of thin-walled semi-circular reference planes.