Method for rapidly generating corner side milling process path
Patent Information
- Authority / Receiving Office
- CN Β· China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
- Publication Date
- 2013-10-23
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Abstract
Description
technical field
[0001] The invention relates to the technical field of CAD / CAPP / CAM, in particular to a numerical control processing method, in particular to a method for quickly generating a machining track of corner side milling of an aircraft structural part. Background technique
[0002] Aircraft structural parts are the main load-bearing components of the aircraft, including frames, beams, wall panels and other structural types. Due to the high quality requirements and short processing cycle of aircraft structural parts, CNC machining is mainly carried out on high-end CNC machine tools. Through years of technological transformation, my country's aviation manufacturing enterprises have introduced and developed a large number of high-value, high-cost CNC machine tools and supporting equipment, but the overall utilization rate of equipment is less than 40%. One of the main reasons is the low efficiency of CNC programming. For large integral structural parts, the ratio of pr...