Double-layer spinning origami honeycomb interlayer energy-absorbing material and preparation method thereof

An energy-absorbing material and paper honeycomb technology, applied in the field of energy-absorbing sandwich structure and its preparation, can solve the problems of easy interference, difficult protection effect, high initial buckling load of regular hexagonal honeycomb structure, and achieve light weight, reduce quantity, The effect of reducing quality

Active Publication Date: 2021-05-04
ZHENGZHOU UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003]The traditional regular hexagonal honeycomb is a weight-reducing and energy-absorbing structure often used in contemporary lightweight design. In order to change the energy-absorbing performance of honeycomb sandwich panels, several This method was proposed in the literature (Gunes R(2016) Development of numerical realistic model for predicting low-velocity impact response of aluminum honeycomb sandwich structures. Journal of Sandwich Structures and Materials18(1):95-112. ; Tolga T(2018) Investigation of low velocity impact behaviors of honeycomb sandwich composites. Journal of Mechanical Science and Technology32(7):3161-3167. ;Giulia P(2018) Single and double-layer honeycomb sandwich panels under impact loading. International Journal of Impact291 Engineering:7) There are limited types of methods to change the energy absorption performance of honeycomb sandwich structures, and they are all proposed on the basis of changing their materials or geometric parameters, which have certain limitations in practical applications: (1) The initial buckling of traditional regular hexagonal honeycomb structures The load is high, and it requires a lot of energy to trigger its deformation and energy absorption mechanism, so it is difficult to achieve a protective effect when it collides with vulnerable protected objects such as the human body; (2) For the traditional regular hexagonal honeycomb structure, although it can Improve its energy absorption performance by increasing the side length of the core unit, but in environments with limited application space (such as helmets, protective gear, engine covers, etc.), the design size of the honeycomb structure is limited, so this method is difficult to meet Practical application requirements
[0004]The triangular orig

Method used

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  • Double-layer spinning origami honeycomb interlayer energy-absorbing material and preparation method thereof
  • Double-layer spinning origami honeycomb interlayer energy-absorbing material and preparation method thereof
  • Double-layer spinning origami honeycomb interlayer energy-absorbing material and preparation method thereof

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preparation example Construction

[0042] Embodiments of the present invention also provide a method for preparing a double-layer spin origami honeycomb sandwich energy-absorbing material, comprising the following steps:

[0043] Under normal temperature conditions, the preparation steps of the double-layer spin origami honeycomb sandwich energy-absorbing material are as follows:

[0044] 1) Prepare the metal skin according to the design size requirements, and the metal double-layer spin origami honeycomb core can be integrally formed by 3D printing; 2) Clean the surface of the metal skin to be bonded, and put Araldite 2015 two-component room temperature curing paste The paste glue is evenly mixed according to the ratio of 1:1 and spread evenly on the surface to be bonded of the skin, and then the metal skin and the metal core layer coated with the paste glue are placed according to the structural order; 3) Apply about 10~30N The constant pressure allows the product to achieve curing and bonding after 72 hours ...

Embodiment 1

[0050] Prepare the Al 2024-T3 aluminum alloy skin according to the design size length × width × height of 150mm × 100mm × 1mm. Using 3D printing integrated molding technology to obtain Al-3003-H19 aluminum alloy double-layer spin origami honeycomb core, the honeycomb core cell unit is larger than the regular hexagonal side length L c =10mm, the side length of the smaller regular hexagon is 1 / 2 L c =5mm, the cell wall thickness is 0.1mm, the total thickness of the core layer is 30mm, the angle between the normal projection of the small diameter end and the corresponding side of the large diameter end is 0°; the film adopts Araldite 2015 two-component Curing the paste glue at room temperature, mix the paste glue evenly according to the ratio of 1:1 and apply it evenly on the surface to be bonded of the skin, then place the metal skin and the metal core layer coated with the film in accordance with the structural order; apply With a constant pressure of about 20N, the adhesive...

Embodiment 2

[0052] According to the design size length × width × height of 150mm × 100mm × 1mm, the metal skin of 45 steel is prepared, and the aluminum alloy double-layer spin origami honeycomb core of Al-3003-H19 model is obtained by using 3D printing integrated molding technology, the honeycomb core The side length of the larger regular hexagon L c =10mm, the side length of the smaller regular hexagon is 1 / 2 L c =5mm, the cell wall thickness is 0.1mm, the total thickness of the core layer is 30mm, the angle between the normal projection of the small diameter end and the corresponding side of the large diameter end is 30°; the adhesive film is made of LJM-170 resin base Adhesive film: Clean the surface of the metal skin to be bonded, spread the LJM-170 resin-based paper-like adhesive film on the surface to be bonded of the skin, and ensure that there are no obvious air bubbles between the film and the skin, and then place the The metal skin and the metal core layer with the adhesive ...

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Abstract

The invention provides a double-layer spinning origami honeycomb interlayer energy-absorbing material which comprises a core layer and metal skins covering the upper end face and the lower end face of the core layer; the core layer is formed by origami honeycomb cell elements in an array mode, and each origami honeycomb cell element is composed of origami honeycomb unit cells which are symmetrically arranged up and down. The contact ends of the origami honeycomb unit cells and the metal skin are large-diameter ends, and the other ends are small-diameter ends; the large-diameter ends and the small-diameter ends are both in a regular hexagon shape, the side length of the large-diameter ends is twice that of the small-diameter ends, and the included angle between the normal projection of the small-diameter ends and the corresponding sides of the large-diameter ends is 0-30 degrees; and the large-diameter ends and the small-diameter ends of the origami honeycomb unit cells are open. The core layer deforms due to compression of external force, and kinetic energy of an external load is absorbed and converted into strain energy of the double-layer spinning origami honeycomb sandwich structure, so that the loaded process of a protected body is smoother, and the effects of energy absorption and vibration reduction are achieved.

Description

technical field [0001] The invention belongs to the technical field of protective energy-absorbing materials, and in particular relates to an energy-absorbing interlayer structure and a preparation method thereof, which are used as protective energy-absorbing materials. Background technique [0002] "Energy saving, environmental protection, and safety" have always been important themes in the development of the transportation industry. With the continuous emergence of energy shortages, environmental pollution, and traffic accidents, people's requirements for energy conservation, environmental protection, and traffic safety are also increasing. Lightweight energy-absorbing materials came into being. In recent years, with the increasing maturity of material preparation and molding technology, a variety of lightweight energy-absorbing materials with a sandwich structure as the design framework have emerged: honeycomb sandwich structure, foam sandwich structure, lattice sandwich...

Claims

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Application Information

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IPC IPC(8): B32B15/01B32B15/18B32B15/20B32B3/12B32B7/12B32B37/10B32B37/12B32B37/06
CPCB32B15/012B32B15/016B32B15/18B32B15/20B32B3/12B32B7/12B32B37/06B32B37/10B32B37/1284B32B37/1207B32B2037/1223B32B2250/40B32B2307/56B32B2307/718B32B2605/00B32B2605/12
Inventor 李成齐佳旗段玥晨铁瑛郑艳萍赵华东侯玉亮胡春幸
Owner ZHENGZHOU UNIV
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