Design method of airplane frame and rib type sheet metal part processing model

A technology of process model and sheet metal parts, which is applied in the field of process model design of aircraft frame and rib sheet metal parts, and can solve the problems of small number of single pieces of frame and rib parts, large size changes, and difficulty in parametric expression of structural features

Active Publication Date: 2013-03-20
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the number of single pieces of frame-rib parts is small, the variety is large, the size changes greatly, and the structural characteristics are difficult to parametrically express, which also brings difficulties to the determination of the springback correction intermediate state model of frame-rib parts, that is, the definition of the process model of frame-rib parts
[0007] In actual production, the process model design and forming mold design of rubber bladder hydroforming frame rib parts did not consider the springback prediction and compensation, and only carried out sinking deepening treatment in the sinking area to prevent interference; in papers and journals, Han Shengxia and Yan Hongyong In the research on the design technology of hydroforming dies, it is proposed to discretize the section of the part and use the discrete section to express the method of hydroforming parts. The information of curved parts is represented by the bending angle and bending radius contained in the two-dimensional section line. However, it is only limited to the research on linear flanged parts and various independent regular flanged expressions, and does not involve the research on flanged parts with variable cross-sections or the flanged expression when the curvature of the flange line changes, and the consideration of complete parts. Research on Process Model Design of Spring Compensation

Method used

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  • Design method of airplane frame and rib type sheet metal part processing model
  • Design method of airplane frame and rib type sheet metal part processing model
  • Design method of airplane frame and rib type sheet metal part processing model

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Embodiment Construction

[0052] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0053] by figure 1 Example Take the 20-rib part of the front flap as an example. The part consists of a flat web and two flanges with variable curvature, sagging and stringer notches. Combined with the accompanying drawings, the specific implementation process of the process model design method for aircraft frame rib parts is described.

[0054] 1. Example parts are figure 2 The 2 flange design reference surfaces shown and image 3 Flange outer surface shown by as design basis; use plane F WU and F WD intercept get Figure 4 Flange split reference plane shown borderline and projection line and in the normal plane and between, and intercept Get Flange Projection Segmentation Extended Reference Surface and common intercept plane F WU Get web extension inner surface The result is as Figure 5 Shown; the radius of the inn...

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Abstract

The invention belongs to the technical field of aircraft manufacturing, and relates to a design method of an airplane frame and rib type sheet metal part processing model. According to design model of a part, a part processing model which can be directly applied to mold working molded surface design is designed. The design method is applicable to a frame and rib flange part with a variable camber, a variable cross-section, subsidence and a purlin notch. The design method is based on a flange reference plane, and the flange springback and compensation are taken into account.

Description

technical field [0001] The invention belongs to the technical field of aircraft manufacturing, and in particular relates to a method for designing a process model of an aircraft frame and rib sheet metal part. Background technique [0002] Frame rib parts are the main parts of aircraft sheet metal parts. They are often used in wing ribs, fuselage bulkheads, etc., and are mostly overlapped with the skin. More than 50% of the amount. The web of the part is mostly flat or slightly curved, and there are flanges around it, and there are often sags and stringer notches on the flanges. As the complexity of the aircraft shape increases, the flange is generally a curved surface with variable curvature and variable cross-section characteristics. The part webs targeted by the present invention are planar. Part instances such as figure 1 shown. [0003] As an important part of the aircraft structure, frame rib parts directly affect the shape accuracy and structural bearing capacity...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 杨忆湄王俊彪刘闯雷湘衡谭浩
Owner NORTHWESTERN POLYTECHNICAL UNIV
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