Chen Jianxin (left) and Yan Qi (right), First Class Experts from Xi'an Aerospace Power Control Co., Ltd., AVIC Engine Group
Part Structure and Material
The part is made from TC4 titanium alloy, known for its high strength, hardness, toughness, and elongation. However, it has poor thermal conductivity, significant surface work hardening, and challenging cutting properties. The induction wheel is part of the impeller fuel pump and is located at the front end of the impeller. Its inner surface is a rotating body, finished through turning, while the outer surface features evenly distributed blades, completed via milling. At both ends, there are face grooves and radial square holes, making it a classic example of turn-milling composite machining (see Figure 1).
Figure 1: Three-dimensional model of the induction wheel
2. Equipment Selection
The S191 Linear Turn-Milling Machining Center was selected for this task. This seven-axis CNC machine combines the advantages of a five-axis machining center with a two-spindle turning center. It allows for five-axis linkage processing on both the front and back parts. The Y and Z axes are driven by linear motors in a horizontal plane, and the rear spindle can be rotated vertically or horizontally, enabling high-precision machining in both orientations (see Figure 2).
Figure 2
3. Machining Process
Through detailed process analysis, it was found that the part has a large machining allowance, and the blade thickness is only 2mm. Large-margin machining can cause significant deformation. Therefore, stress relief steps and angular orientation must be considered during the process. Since the device features a dual-spindle function with an extended process head at the small outer circumference, the positioning hole is also placed here, ensuring no error occurs due to secondary clamping. Based on the principle of completing multiple processing tasks under one clamping, the process route was determined as follows: rough turning and boring, drilling the positioning hole and deburring, rough milling, stabilization, grinding, fine turning, final milling, square hole milling, cone surface turning, groove milling, and final inspection. Roughing operations were performed on a lathe and CNC machine. From a cost and precision perspective, roughing could not be done on this equipment. Finishing, including fine turning, deburring, cone surface turning, and groove milling, was alternately performed by the dual-spindle of the turn-milling machining center, with positioning done in one setup. By utilizing turn-milling composite technology, the process was optimized, fully leveraging the machine tool’s capabilities, shortening the process route, improving reliability, increasing efficiency, reducing costs, and ensuring high-quality results. Advanced material technologies and modern manufacturing methods form the foundation of aerospace innovation. To enhance processing quality and productivity, it is essential to research and apply efficient and diverse composite machining techniques.Low Type Heavy-duty Industrial Caster
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