Turbine blade air film hole precision forming method
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- XI AN JIAOTONG UNIV
- Publication Date
- 2020-01-31
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the field of rapid casting based on light curing molding technology, and relates to a precision forming method for air film holes of turbine blades. Background technique
[0002] Hollow turbine blade high-efficiency film cooling technology is one of the core technologies in the development of heavy-duty gas turbines, and the film holes are developing in the direction of miniaturization, irregular structure and dense distribution. At present, the air film cooling holes of blades are realized by post-processing. After the blade casting blank is polished and trimmed to determine the process reference plane, laser drilling, electric spark drilling, electro-hydraulic beam drilling and other methods are used to realize the processing of gas film holes.
[0003] Laser drilling technology uses the high temperature at the laser focus point to instantly melt and vaporize the blade material, and the melted and vaporized substances are ej...