Long-cantilever large-scale integral blade-disc blade one-step milling method
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
- Publication Date
- 2015-04-01
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Abstract
Description
technical field
[0001] The invention belongs to the technical field of aero-engines, in particular to a one-time milling method for long-cantilever large-scale integral blisk blades. Background technique
[0002] Integral structure blisks are key parts used in international aero-engines. Integral blisk structures are used at all levels of the low-pressure compressor and high-pressure compressor of the engine. The five-coordinate numerical control milling method is widely used in the world, but for long cantilever large Blisk processing, the traditional butt milling process has been used in China at present, there are secondary clamping errors, and the processing vibration is large and the surface quality is poor. After butt milling, the tool marks are large, and subsequent manual polishing eliminates surface defects such as tool marks and vibration lines. The technical bottleneck problems such as overcutting of the front, rear edge and adjacent parts of the blade lead to ser...