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Automatic tape-laying forming method for composite material with hollowed-out structure

A composite material and hollow structure technology, which is applied in the field of automatic tape laying and forming of composite materials, can solve the problems of restricting the shape of laying products, increasing the workload of cutting knives, and wrinkles on the surface of prepreg tape, so as to reduce post-processing work Quantity, improve molding efficiency, reduce the effect of product quality

Inactive Publication Date: 2012-01-11
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in existing applications, tape laying products have relatively large limitations in shape, and more products have regular shapes and regular boundaries, and are rarely used in the molding of products with hollow structures. Among them, the more typical hollow structures are only For products with a small number of holes
If it is necessary to lay and form a product with a large number of hollow structures, the cutting workload of the cutter will be greatly increased, resulting in a decrease in the efficiency of laying and forming, especially when the one-step tape laying method is adopted
Moreover, when using the one-step tape laying method, when laying the end part of the prepreg tape with a small angle, the press shoe or roller will press to the leading edge of the next prepreg tape, and the leading edge of the prepreg tape needs to be torn off from the mold surface, and the Affect product quality and molding efficiency
In addition, when the angle between a certain section of the predetermined line trajectory and the fiber direction in the predetermined broken line trajectory is small, the movement of the cutter will cause the fibers to shift and pile up, which will cause wrinkles on the surface of the prepreg tape and affect the surface quality of the product. It also limits the shape of the laying product

Method used

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  • Automatic tape-laying forming method for composite material with hollowed-out structure
  • Automatic tape-laying forming method for composite material with hollowed-out structure
  • Automatic tape-laying forming method for composite material with hollowed-out structure

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Experimental program
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specific Embodiment approach 1

[0029] Specific implementation mode one: combine figure 1 , 2 , 3, 4, 5, 6, 7, and 8 describe this embodiment. When forming a composite material with a hollow structure, the shape of the prepreg tape is first designed according to the shape and size to be formed, the width of the prepreg tape and the direction of the layup, and then the trajectory of the double cutter 5 is obtained. use as figure 1 The pre-cutting unit shown, performs pre-cutting of prepreg tape. The prepreg tape 3 to be cut is led out from the unwinding roll 1 by the guide roller 2, and after the backing paper 4 is peeled off, the prepreg tape 3 is cut into a predetermined shape by double cutters 5. In order to ensure efficiency and realize continuous production, the cutting depth of the double cutter 5 needs to be strictly controlled, so that the backing paper can not be cut while cutting the prepreg. After the prepreg is cut, add a new backing paper 8 (one layer can be replaced by a film), and then comp...

specific Embodiment approach 2

[0035] Specific implementation mode two: combination Figure 5 , 6 , 7 describe this embodiment. Compared with the first embodiment, the forming principle of this embodiment is the same, but there are differences in the pre-cutting and laying methods of the prepreg tape, that is, the winding method of the single-layer backing paper. Such as Figure 5 As shown, after the prepreg tape is pre-cut, a layer of new backing paper 8 is added below, and a special backing film 16 is used to replace the top. Backing paper. When laying the prepreg tape, if Figure 6 As shown, a paving head paper motor 13 can be omitted, and its schematic diagram is as follows Figure 7 .

specific Embodiment approach 3

[0036] Specific implementation mode three: combination Figure 8 , 9 , 10, and 11 describe this embodiment. When it comes to the laying and molding of composite materials with a large number of grid-like structures, the automatic tape-laying of -45° ply grid-like materials is taken as an example. The pre-cut prepreg tape shape should be designed in advance considering the mesh size and prepreg tape width. Pre-cut prepreg tape into Figure 9 After laying the shape shown, the molding effect is as follows Figure 9 , where the arrow points to the laying direction of the prepreg tape, black represents the prepreg tape, and white represents the formed grid shape. If the prepreg tape is precut into Figure 10The shape shown, the molding effect is as follows Figure 11 shown.

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Abstract

The invention relates to an automatic tape-laying forming method for a composite material with a hollowed-out structure, belonging to the field of laying and forming of composite materials. The invention is characterized by comprising the following processes: (1) designing the shape of a prepreg tape according to the shape and dimension of a product, the bandwidth of the prepreg tape and the direction of tape laying so as to further obtain a predetermined fold line path of a cutting knife; (2) precutting the prepreg tape, rolling up strip coils, wherein, the method of double layer back lining paper rolling or single layer back lining paper rolling can be employed to roll up the strip coils, and when one part of predetermined linear path of the predetermined fold line path is related to low-angle cutting, carrying out cutting by using the method of notching fold line cutting; (3) laying the cut prepreg tape on the surface of a die with the head of a laying tape so as to complete automatic tape-laying forming of the composite material with a hollowed-out structure. The invention enables basic functions of a tape-laying machine to be realized and fabrication difficulty of composite materials with a hollowed-out structure to be overcome.

Description

technical field [0001] The invention relates to a composite material automatic tape-laying forming method with a hollow structure, and belongs to the field of composite material laying and forming. Background technique [0002] With the development of the aerospace industry, advanced composite materials are more and more used in the manufacture of large components of aerospace vehicles, and automatic tape laying technology is widely used in the field of aerospace as an automatic forming technology for advanced composite materials. The traditional manual lay-up molding method improves the processing efficiency, improves the working environment and reduces the manufacturing cost. However, in existing applications, tape-laying products have relatively large limitations in shape, and more products have regular shapes and regular boundaries, and are rarely used in the molding of products with hollow structures. Among them, the more typical hollow structures are only A product wi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/38B29C70/54B29B13/00
Inventor 文立伟李俊斐王显峰齐俊伟还大军李勇
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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