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Prestressing shot-blasting formation technique for double-curved wallboard

A shot peening and prestressing technology, applied in the field of manufacturing, can solve the problems of limited forming ability and difficult final forming of large wing panels

Inactive Publication Date: 2007-10-03
XIAN AIRCRAFT IND GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, free shot peening has limited forming ability for large wing panels with double curvature and variable thickness, and it is difficult to form them finally.
[0003] In order to overcome the shortcomings of the existing free shot peening for the shot peening of large-scale wing panels with double curvature and variable thickness, the present invention discloses a prestressed shot peening technology for double curvature wall panels and the used forming prestressing fixtures and wall panels. Plate pre-bending clamping method

Method used

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  • Prestressing shot-blasting formation technique for double-curved wallboard
  • Prestressing shot-blasting formation technique for double-curved wallboard
  • Prestressing shot-blasting formation technique for double-curved wallboard

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Embodiment Construction

[0021] See the accompanying drawings: The theoretical shape shown in Figure 1 is a double-curvature structure, and its chord curvature is represented by several transverse rib lines 2 on the wall plate 1, and its span curvature line 3 is defined by the wall plate The central longitudinal line of is used as the representative curvature line. The technical problem solved by the present invention is to pre-bend and clamp the unfolded panel as shown in Figure 2 with a prestressing fixture, so that the pre-bending state of each rib line and spanwise curvature line on the panel conforms to Figure 1 The theoretical shape is shown, and then the wall panel parts are shaped by shot peening.

[0022] The prestressing fixture used in the present invention is shown in Figure 3, is formed a rigid framework by several columns 4 and beam 5 and beam guide rail 6, and the quantity of column 4 and the fixed position on beam guide rail 6 can be flexibly adjusted. The forming column is provided w...

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PUM

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Abstract

A pre-stressing and grit-blasting technique for shaping a double-curvature plate wall used as the thick jacket of large airplane features that a pre-stressing fixture unit is used to pre-bend a plate longitudinally and transversely and fix it for applying a pre-stress to it while the grits are blasted onto said plate for obtaining a needed shape.

Description

technical field [0001] The present invention relates to manufacturing technology, more specifically relates to the shot blasting forming technology of complex wing panel of large aircraft. Background technique [0002] The aerodynamic performance of an aircraft mainly depends on the wing airfoil. The complex hyperboloid shape is the mainstream of modern large aircraft design, which can increase the cruising speed of the aircraft, and has significant advantages such as low fuel consumption and excellent aerodynamic performance. However, complex airfoils also increase the difficulty of forming wing panels. For such wing panels whose thickness and curvature change in span and chord respectively, the preferred forming method is shot peening. Shot peening is a forming method that uses a high-speed metal shot flow to hit the surface of a metal plate, causing plastic deformation of the surface material on the sprayed surface, introducing residual stress, and gradually making the wo...

Claims

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Application Information

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IPC IPC(8): B24C1/00B24C3/32B24C9/00
Inventor 高国强乔明杰
Owner XIAN AIRCRAFT IND GROUP
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