Process method for enhancing the milling rigidity of aluminum alloy ultra-thin blade overall impeller
A technology of integral impeller and process method, applied in metal processing equipment, milling machine equipment, manufacturing tools, etc., can solve problems affecting the quality and performance stability of the impeller and impeller components, missing blades, undercutting and overcutting of blade surface contours, etc. , to achieve the effect of improving surface quality, reducing vibration and improving cutting efficiency
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2017-03-08
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to a process method for enhancing the milling rigidity of an integral impeller of an ultra-thin blade made of an aluminum alloy material. Background technique
[0002] With the development of computer integrated manufacturing technology, mechanical structure technology, material science and technology and other disciplines, more and more ultra-thin blade integral impellers have been applied in high-precision industrial equipment. The height and thickness of such ultra-thin blade integral impellers Ratio ≥ 15, the thinnest part of the leading and trailing edge of the blade δ min <0.5mm, the included angle α≤3° between the midline of the blade length direction and the midpoint of the normal sectional plane, and the structural feature of large distortion appears on the shape of the blade. During the entire cutting process, the material removal rate of such parts is as high as 95%, and the surface contour error is small, and the p...
Examples
Embodiment Construction
[0023] The present invention will be further described below according to the accompanying drawings.
[0024] A process method for enhancing the milling rigidity of an integral impeller of an aluminum alloy material ultra-thin blade, comprising the following steps:
[0025] Step 1: Layer the leaves.
[0026] The layering scheme is shown in Table 1.
[0027] Table 1: Leaf layering scheme. Where h is the blade height, a is the average thickness of the blade crown and the thickest part of the blade root, and ε is the ratio of the blade height to the average thickness.
[0028]
[0029] Step 2: Rough machining allowance is reserved.
[0030] Rough machining allowance is reserved for each layer respectively, and the reservation scheme is shown in Table 2.
[0031] Table 2: Reserved plan for the margin of each layer of the rough machining blade
[0032]
[0033] Step 3: Five-axis simultaneous finishing.
[0034] Five-axis simultaneous finishing of an ultra-thin blade mon...