A kind of manufacturing method of high-reinforced aluminum alloy panel
A manufacturing method and technology of aluminum alloy, applied in the direction of sheet/board, building components, etc., to achieve the effect of ensuring manufacturing efficiency and accuracy, ensuring the strength of parts, and ensuring manufacturing accuracy
Active Publication Date: 2018-01-02
JILIN UNIV
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Problems solved by technology
The mechanical removal after multi-point pressing can control the uniform release of residual stress by controlling the milling path, so as to ensure the manufacturing efficiency and precision of the aluminum alloy aircraft integral wall panel, and solve the problem that the existing aluminum alloy integral panel is simply formed by multi-point forming or brake pressure. Forming Disadvantages
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[0033] refer to Figure 1a , Figure 1b , Figure 1c , Figure 1d , Figure 4 ,in Figure 1a — Figure 1d It is a schematic structural diagram of the manufacturing process of high-reinforced aluminum alloy siding, a high-reinforced aluminum alloy siding, which is a double-curvature siding with I-shaped or T-shaped high-reinforced strips. The specific steps of the method are as follows:
[0034] Step 1. Predict the amount of springback according to the target shape, sheet thickness and material parameters of the high-reinforced aluminum alloy panel, obtain the surface data of the upper and lower multi-point molds through calculation, and automatically adjust the upper and lower multi-point molds 1 and 4 Profile;
[0035] The specific steps are as follows:
[0036] 11) Forming preparation process
[0037] According to the size and maximum thickness of the integral wall panel parts to be manufactured, in the case that there is a machining allowance around the sheet metal a...
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The invention relates to the field of metal molding, in particular to a high rib aluminum alloy wallboard manufacturing method. Firstly, upper and lower multipoint molds are adopted to oppositely press an aluminum alloy plane thick plate to mold a needed curved surface shape; and then, a high-speed milling method is used for milling a needed rib structure on the curved surface thick plate in a processing path parallel to the curved surface, so that a designed high rib aluminum alloy wallboard is obtained. The method applies the characteristic of quick and adjustable reconstruction of profile surfaces of the multipoint molds, uses one set of multipoint molds for molding double-curvature aluminum alloy thick plate parts with different geometric shapes, different thicknesses and different materials, and can control the rebound in molding of the aluminum alloy thick plate through multiple times of correction so as to improve the molding precision; and the high rib aluminum alloy wallboard manufacturing method can obtain high-precision high rib aluminum alloy wallboard parts without damaging fiber structures of the aluminum alloy plate materials, guarantees the strength requirements of the wallboard parts, solves the technical difficulties in large aircraft manufacturing, and can be popularized and applied to manufacturing of such other parts as spacecrafts and rockets.
Description
technical field [0001] The invention relates to the field of metal shaping processing, specifically a method for manufacturing high-reinforced aluminum alloy wall panels. Background technique [0002] With the rapid development of the aerospace industry, people's requirements for the performance of modern aircraft continue to increase. High-reinforced aluminum alloy integral wall panels have been widely used in the aerospace field due to their light weight, good rigidity, and long fatigue life. At present, the main methods of integral wall panel forming are: gate pressure forming, aging creep forming, shot blasting and so on. Aging creep forming has special requirements for materials, and requires large autoclave equipment, long manufacturing cycle and high production cost; shot peening is limited by deformation amount and wall plate structure, and is suitable for forming wall plates with low ribs ; Brake forming has strong adaptability to product dimensions and low proces...
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IPC IPC(8): B21C37/02F16S1/10
CPCB21C37/02F16S1/10
Inventor 刘纯国岳韬邓玉山赵勇蔡中义郑愿
Owner JILIN UNIV