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A fiber-dominated fiber laminated toughening structure and method for composite materials

A composite material fiber and toughening technology, which is applied in chemical instruments and methods, lamination, lamination devices, etc., can solve problems such as engineering application limitations, weak interlayer performance, and restrictions on application and promotion, and achieve strong synergistic deformation ability, Effect of optimized resistance to local damage

Active Publication Date: 2021-08-10
AEROSPACE RES INST OF MATERIAL & PROCESSING TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Composite laminated structures are limited by weak interlayer performance, easy delamination, and low impact damage tolerance, which restricts their application in two harsh service conditions of low-period multi-frequency repeated use and instantaneous high overload impact load. to promote
[0003] The existing resin-based composite laminated structure toughening technology mainly adopts two methods: one is to modify and toughen the resin matrix, which is the main improvement method for the interlayer toughening of thermosetting resin-based structural composite materials. The semi-interpenetrating cross-linked network of molecular chains between the structural phases is primary toughened, the thermoplastic resin and the epoxy matrix form a bicontinuous phase structure, and the micron-sized specific thermoplastic PA particles (thermoplastic particles) are introduced to form a progressive "three Step-by-step toughening”; one is to use stitching, Z-pin and other methods for interlayer toughening. Due to the complex manufacturing process, engineering applications are obviously limited

Method used

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  • A fiber-dominated fiber laminated toughening structure and method for composite materials
  • A fiber-dominated fiber laminated toughening structure and method for composite materials
  • A fiber-dominated fiber laminated toughening structure and method for composite materials

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0067] Embodiment 1: Composite fiber toughened laminate member;

[0068] Such as figure 1 , figure 2 and image 3 As shown, the size of the component is 1000mm×600mm, the thickness is 4.8mm, and the ply angle is [45 / 90 / -45 / 0] 8 , The raw material for molding is carbon fiber epoxy resin prepreg tape, and the thickness of a single layer is about 0.15mm.

[0069] The composite fiber laminated and toughened structure is a structure of equal thickness, including four ply units, which are respectively marked as the first ply unit, the second ply unit, the third ply unit, and the fourth ply unit. ply unit;

[0070] The first ply unit includes four angle plies, which are respectively 45° ply, 90° ply, -45° ply, and 0° ply;

[0071] The second ply unit includes four angle plies, which are 45° ply, 90° ply, -45° ply, and 0° ply;

[0072] The third ply unit includes four angle plies, which are 45° ply, 90° ply, -45° ply, and 0° ply;

[0073] The fourth ply unit includes four angl...

Embodiment 2

[0097] Example 2: 2.5-dimensional composite fiber-toughened laminate member

[0098] Such as figure 1 , figure 2 and Figure 4 As shown, the size of the component is 500mm×500mm, the thickness is 4mm, the layup angle is [60 / 90 / 0 / -60]5, the raw material for molding is glass fiber plain cloth, and the thickness of a single layer is about 0.2mm.

[0099] The fiber laminated and toughened structure of the composite material is an equal-thickness structure, including two ply units, and the two ply units are respectively marked as the first ply unit and the second ply unit;

[0100] The first ply unit includes four angle plies, which are 60° ply, 90° ply, 0° ply, and -60° ply;

[0101] The second ply unit includes four angle plies, which are 60° ply, 90° ply, 0° ply, and -60° ply;

[0102] 1) Select the prefabricated body laying mold and the glass fiber plain weave tape with a width of 50mm;

[0103] 2) Complete laying of 1 piece of glass fiber plain weave belt with 1 belt wid...

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Abstract

The invention relates to a fiber-dominated composite material fiber lamination toughening structure and method. The structure changes the way that the load transfer between the layers of the existing laminated structure only depends on the interlayer shear, and proposes a method based on the interlayer interface. The strong coupling interlayer mechanical load transfer mode of the fiber tow interweaving unit realizes a method for improving interlayer toughness of composite materials, and belongs to the technical field of structural composite material manufacturing. By introducing a cross-layer toughening tape layer between adjacent or similar layers of different angles, a form of interweaving structure is formed in two adjacent or multiple adjacent layers.

Description

technical field [0001] The invention relates to a fiber-dominated composite material fiber lamination toughening structure and method. The structure changes the way that the load transfer between the layers of the existing laminated structure only depends on the interlayer shear, and proposes a method based on the interlayer interface. The strong coupling interlayer mechanical load transfer mode of the fiber tow interweaving unit realizes a method for improving interlayer toughness of composite materials, and belongs to the technical field of structural composite material manufacturing. Background technique [0002] Composite laminated structures are limited by weak interlayer performance, easy delamination, and low impact damage tolerance, which restricts their application in two harsh service conditions of low-period multi-frequency repeated use and instantaneous high overload impact load. promote. [0003] The existing resin-based composite laminated structure toughening...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B32B3/06B32B5/02B32B5/26B32B33/00B32B37/02
Inventor 张建宝刘永佼孙建波陈亮耿东兵易凯沈登雄尚呈元
Owner AEROSPACE RES INST OF MATERIAL & PROCESSING TECH