Thin-wall component space envelope forming buckling deformation prediction method
A technology of thin-walled components and prediction methods, which is applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of component folding, rupture, scrapping, warping and deformation, and affecting component accuracy, so as to shorten the product development cycle, Improve design efficiency and efficiently predict the effect
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2021-06-25
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Abstract
Description
technical field
[0001] The invention relates to the field of thin-wall component manufacturing, and more specifically, to a method for predicting warpage deformation of thin-wall component space envelope forming. Background technique
[0002] Thin-walled components have the characteristics of light weight and large bearing capacity, and are widely used in aerospace fields such as wings, fuselages, and fuel storage tanks. At present, the main manufacturing method of thin-walled components is mechanical processing, but this method has problems such as poor performance, low processing efficiency, low material utilization rate, and high production cost.
[0003] The space envelope forming method of thin-walled components is a new forming method for thin-walled components, which has the advantages of small forming load, high forming efficiency and excellent component performance. However, thin-walled components are small in thickness and large in diameter, and are prone to warpi...
Examples
Embodiment Construction
[0056] In order to have a clearer understanding of the technical features, purposes and effects of the present invention, the specific implementation manners of the present invention will now be described in detail with reference to the accompanying drawings.
[0057] A method for predicting warping deformation of a thin-walled component space envelope forming according to the present invention comprises the following steps:
[0058] S1. Determine the principle of space envelope forming of thin-walled components. The initial state of space envelope forming of thin-walled members is as follows: figure 1 as shown, figure 1Among them, 1 is the enveloping mold, 2 is the blank, and 3 is the lower mold. The envelope mold rotates around its own axis and the central axis of the thin-walled member at a speed of n=4rad / s, and the lower mold drives the blank placed in the lower mold to approach the envelope mold at a feed speed of v=2mm / s. With the increase of the feed rate of the low...