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Placement layer theoretical thickness measuring and calculating method based on automatic tow placement technology

A technology of automatic laying and laying, which is applied in the field of theoretical thickness measurement of laying based on automatic laying technology, can solve problems such as large error and repeated trial and error, achieve accurate thickness, improve programming efficiency, and avoid actual laying. The effect of verification

Active Publication Date: 2020-12-11
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The traditional thickness measurement method is to use ultrasound and other means to measure the composite material after curing. There is no way to characterize the theoretical thickness before curing. It can only rely on the experience of programmers to avoid overlapping triangles and achieve the theoretical thickness as much as possible. This method There are problems such as large errors and repeated trial and error

Method used

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  • Placement layer theoretical thickness measuring and calculating method based on automatic tow placement technology
  • Placement layer theoretical thickness measuring and calculating method based on automatic tow placement technology
  • Placement layer theoretical thickness measuring and calculating method based on automatic tow placement technology

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Embodiment 1

[0030] A method for measuring and calculating the theoretical thickness of layers based on automatic wire laying technology, comprising the following steps:

[0031] Step S1: Extract the molded surface of the part to be formed, and represent the molded surface with a point cloud, such as figure 1 , get points P1, P2, P3...Pn;

[0032] Step S2: According to the theoretical trajectory of the laying program, extract the centerlines L1S1, L1S2, L1S3...L1Sn of each tow on the first laying layer L1, and extract all centerline;

[0033] Step S3: For any layer Ln, find the perpendicular line between any point Pn in the point cloud and any center line LnSn on the layer, and the length of the perpendicular line

[0034] Step S4: if figure 2 , according to the calculated distance between the Pn point and the center line, determine whether the Pn point falls in the prepreg coverage area, and judge each point of the point cloud in turn, filter out the points that fall in the prepreg ...

Embodiment 2

[0038] A method for measuring and calculating the theoretical thickness of layers based on automatic wire laying technology, comprising the following steps:

[0039] Step S1: Extract the molded surface of the part to be formed, and represent the molded surface with a point cloud, such as figure 1 , to obtain points P1, P2, P3...Pn; when using point cloud to express the molding surface, the ply thickness information is obtained after mathematical calculation for each point, where the distance between two adjacent points is not greater than the specified value; the specified value is determined according to the width of the automatic wire laying material and the gap between the belts;

[0040] Step S2: According to the theoretical trajectory of the laying program, extract the centerlines L1S1, L1S2, L1S3...L1Sn of each tow on the first laying layer L1, and extract all centerline;

[0041] Step S3: For any layer Ln, find the perpendicular line between any point Pn in the point ...

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Abstract

The invention discloses a placement layer theoretical thickness measuring and calculating method based on an automatic tow placement technology. The placement layer theoretical thickness measuring andcalculating method based on the automatic tow placement technology comprises the following steps that a die pasting surface of a part to be formed is extracted, and the die pasting surface is represented with point cloud; the center line of each tow on a first placement layer is extracted according to a theoretical track of a placement tow program, and all center lines are sequentially extractedon the subsequent placement layers; for any placement layer, a vertical line and a vertical line length of any point of the point cloud and any center line on the placement layers are solved; according to the calculated distances between the points and the center lines, whether the points fall in a prepreg coverage area or not is judged, all the points of the point cloud are judged in sequence, the points falling in the prepreg coverage area are screened out, the points falling outside the prepreg coverage area are removed, and the new point cloud is used for expressing the theoretical thickness of the placement layers; and all placement layers are analysed, the point cloud representing the theoretical thickness of each layer is superposed, repeated points are counted, coloring is carriedout according to a counting result, and the final theoretical thickness of the full placement layers is expressed according to the counting size corresponding to different chromatograms.

Description

technical field [0001] The invention relates to the field of automatic wire laying, in particular to a method for measuring and calculating the theoretical thickness of layers based on automatic wire laying technology. Background technique [0002] The full name of automatic fiber placement technology for composite materials is automatic tow placement technology ATP (Automated TowPlace-ment), also known as fiber placement technology (FiberPlacement). Automatic wire laying technology was proposed in the 1970s as a reform of winding and tape laying technology, aiming to overcome the "periodical, stable and non-overhead" aspects of winding technology and the fact that automatic tape laying must follow the "natural path". Limitation, for the manufacture of composite fuselage structures, the core technology is the design and development of multi-tow placement heads and the development of corresponding material systems. Boeing and Hercules began to develop automatic wire laying t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/38B29C70/54
CPCB29C70/382B29C70/54
Inventor 陈浩然聂海平罗辑谢林杉王大为
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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