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A kind of composite material lattice structure and preparation method

A composite material and lattice structure technology, applied in the field of composite material lattice structure and preparation, composite material lattice structure preparation technology field, can solve the problem of inability to prepare curved composite material lattice structure, low strength of lattice core fiber rods, The fiber turning angle is too large to achieve the effect of high reliability of product quality, low porosity of finished products, and reduced impact on mechanical properties

Active Publication Date: 2019-09-27
HARBIN ENG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The metal mold of the above method (1) is complex to process, difficult to close the mold, and is only suitable for flat plate structures, and cannot prepare curved surface composite material lattice structures
The above method (2) and method (3) use the method of bonding to connect the lattice core and the panel, the strength of the bonding is low, and the nodes are prone to damage
The lattice core fiber of the above method (4) is directly interspersed between the panels, the lattice core fiber is not subjected to external pressure during curing, and the strength of the lattice core fiber rod is low
The above method (5) uses the molten core forming technology, which effectively solves the problem of forming molds, and is very suitable for preparing composite lattice structures with complex shapes. interspersed fiber protrusion

Method used

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  • A kind of composite material lattice structure and preparation method
  • A kind of composite material lattice structure and preparation method
  • A kind of composite material lattice structure and preparation method

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preparation example Construction

[0058] A kind of preparation method of composite material lattice structure of the present invention, concrete preparation steps:

[0059] Step 1: Preparation of low melting point alloy core mold;

[0060] combine image 3 and Figure 4 As shown, the present invention adopts a fusible alloy core molding technology, and the used fusible alloy core 4 is cast from a low-melting point alloy, which contains through holes 5 .

[0061] The low-melting-point alloy is Wood's alloy, whose melting point is higher than the forming temperature and lower than the Martin heat-resistant temperature of the material. The present invention adopts Wood's alloy with a melting point of 60-70 degrees Celsius, and the alloy composition: 38-50% bismuth, 25-31% of lead, 12.5-15% of tin, and 12.5-16% of cadmium.

[0062] The hole 5 is a through hole or a square hole, the diameter of which is the same as that of the rod of the lattice core 3, and the axis coincides with the axis of the lattice core. ...

Embodiment

[0095] In order to prove the mechanical performance advantage of the composite material lattice structure prepared in the present invention, adopt ABAQUS finite element software to carry out numerical simulation, Figure 17 The finite element model shown shows a 100mm x 100mm plate domain with two lattice core members at an angle of 45 degrees, hinged around the plate.

[0096] Composite lattice structures generally fail at nodes. In order to accurately simulate the failure behavior at nodes, Surface-based Cohesive Behavior is used to simulate the delamination behavior between fibers. The finite element model of each bundle of fiber rods is established, and the C3D8R three-dimensional solid reduced integration element is used for simulation. The material is carbon fiber, the thickness of the panel is 4mm, and the section of the trapezoidal fiber rod is 2mm×2mm. In order to discuss the influence of triangular fibers on the structural force, the failure modes of no triangular f...

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Abstract

The invention provides a composite lattice structure and a preparation method. The composite lattice structure is composed of an upper face plate, a lower face plate and a lattice core arranged between the upper face plate and the lower face plate. The lattice core is formed in the manner that lattice core triangular fibers and trapezoidal fibers are interlaced. Foam interlayers are arranged in the upper face plate and the lower face plate. A specific injection manner is applied to the composite lattice structure for VARTM formation. The preparation method of the composite lattice structure comprises the seven steps of (1) preparing a fusible alloy mold core; (2) inserting the triangular fibers; (3) laying fibers on the bottom layers of the upper face plate and the lower face plate; (4) inserting the trapezoidal fibers; (5) arranging the face plate interlayers and laying surface fibers of the face plates; (6) conducting VARTM (vacuum assisted resin transfer molding) formation; (7) heating and melting the fusible alloy mold core. The composite lattice structure and the preparation method effectively solve the connection problem between a composite lattice core and the face plates, integrated formation is achieved, the quality is reliable, the technology is simple, and the node strength is high.

Description

technical field [0001] The invention relates to a lattice structure of a composite material and a preparation method thereof, in particular to a preparation process of a lattice structure of a composite material, and belongs to the fields of engineering material preparation and structure design. Background technique [0002] In 2001, Professor Evans of Princeton University, Professor Hutchinson of Harvard University, Professor Ashby of Cambridge University, and Professor Gibson of MIT first proposed the concept of lattice sandwich structure. The lattice structure not only has the advantages of high specific strength and specific stiffness, but also has multifunctional potentials such as energy storage, braking, and pre-embedding. Although some achievements have been made in the preparation method of lattice structure of composite materials, there are still many problems, which have been the focus of research at home and abroad. [0003] The current composite material lattic...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C70/34B29C70/54B29C70/08B29C70/10B32B5/18B32B33/00B32B3/26B32B3/08
Inventor 张建华官成宇薛启超高硕颀周恩惟佟丽莉杨思远林佳悦
Owner HARBIN ENG UNIV
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