Quasi-zero-rigidity honeycomb core vibration reduction package and preparation method thereof

文档序号:608298 发布日期:2021-05-07 浏览:9次 中文

阅读说明:本技术 一种准零刚度蜂窝芯减振包装及其制备方法 (Quasi-zero-rigidity honeycomb core vibration reduction package and preparation method thereof ) 是由 刘彦琦 邓二杰 宋春芳 于 2021-02-09 设计创作,主要内容包括:本发明公开了一种准零刚度蜂窝芯减振包装及其制备方法,涉及食品、果蔬、酒水、精密仪器等运输缓冲包装结构设计领域。该减振包装的外部结构包括但不限于箱、圆柱、垫或其他形式,可依据具体情况改变;内部核心结构为准零刚度蜂窝芯,由负刚度双曲梁和正刚度圆锥曲线壁并联组成的胞元线性阵列构成。本发明基于正负刚度并联的原理,获得了整体结构的准零刚度特性,从而在保证原承载能力的情况下实现低频宽带减振,解决了传统减振包装以塑性变形方式吸收能量后不能重复使用、承载力低、低频减振效果差等问题。此外,本发明的结构通过3D打印技术或切割技术进行一体化制备,避免了现有的准零刚度减振器加工繁杂、安装困难等问题。(The invention discloses a quasi-zero-rigidity honeycomb core vibration reduction package and a preparation method thereof, and relates to the field of design of transportation buffer package structures of foods, fruits and vegetables, drinks, precision instruments and the like. The external structure of the shock absorbing package includes, but is not limited to, a box, cylinder, pad or other form, which may vary from case to case; the internal core structure is a quasi-zero rigidity honeycomb core and is formed by a cell linear array formed by connecting a negative rigidity double-curved beam and a positive rigidity conical curve wall in parallel. The invention obtains the quasi-zero stiffness characteristic of the whole structure based on the principle of positive and negative stiffness parallel connection, thereby realizing low-frequency broadband vibration reduction under the condition of ensuring the original bearing capacity, and solving the problems that the traditional vibration reduction package can not be reused after absorbing energy in a plastic deformation mode, has low bearing capacity, poor low-frequency vibration reduction effect and the like. In addition, the structure of the invention is integrally prepared by a 3D printing technology or a cutting technology, so that the problems of complex processing, difficult installation and the like of the existing quasi-zero stiffness damper are solved.)

1. A quasi-zero rigidity honeycomb core vibration damping package and a preparation method thereof are characterized in that: the honeycomb core is formed by a cell linear array formed by connecting a negative-rigidity double-curved beam and a positive-rigidity conic curve wall in parallel, and the whole structure has a quasi-zero rigidity characteristic based on the positive-negative rigidity parallel principle, so that low-frequency broadband vibration reduction is realized under the condition of ensuring the original bearing capacity, and the honeycomb core is integrally prepared by a 3D printing technology or a cutting technology.

2. A quasi-zero stiffness honeycomb core vibration dampening package according to claim 1 wherein: the honeycomb core cell element is composed of a double-curved beam, a conical curve wall and a pressing plate, and the upper part and the lower part of the honeycomb core cell element are in an axial symmetry structure.

3. A quasi-zero stiffness honeycomb core vibration dampening package according to claim 2 wherein: the double-curved beam provides positive stiffness for a mechanism providing negative stiffness and a conical curve wall in the orthogonal direction with the double-curved beam, and the cell element has a quasi-zero stiffness characteristic based on the positive and negative stiffness parallel principle, so that the whole structure can realize high static and low dynamic.

4. The method for preparing a quasi-zero stiffness honeycomb core vibration damping package according to claim 1, wherein the method comprises the following steps: the conical curve wall is tangent to the lower end of the hyperbolic beam, so that the honeycomb core is integrally formed through a 3D printing technology or a cutting technology.

5. The method for preparing a quasi-zero stiffness honeycomb core vibration damping package according to claim 4, wherein the method comprises the following steps: the honeycomb core is prepared from a viscoelastic nylon-based material by a 3D printing technology or a superelastic metal material by a cutting technology.

Technical Field

The invention relates to the field of transportation buffer packaging structure design of foods, fruits and vegetables, drinks, precision instruments and the like, in particular to a quasi-zero-rigidity honeycomb core vibration reduction package and a preparation method thereof.

Background

The vibration is widely existed in nature, a large amount of product breakage and buffer packaging function failure phenomena occur particularly in the transportation process, and the economic loss caused by product breakage due to improper packaging protection reaches hundreds to hundreds of billions yuan every year. In china, the protection research of product vibration and impact environment is comparatively weak in the transportation, and common transportation cushion packaging includes corrugated carton, honeycomb cardboard, paper pulp molding, air cushion film, foamed plastic, plastics turnover case etc. and most absorb the energy through taking place plastic deformation, but reuse to traditional cushion packaging is relatively poor at the damping effect of low frequency transportation, easily causes direct influence to external packing, loses the cushioning effect.

The traditional linear vibration absorber cannot reduce the natural frequency of the traditional linear vibration absorber to a low enough value, so that the expected vibration absorbing target is difficult to achieve, and the traditional linear vibration absorber mainly has the defects of poor low-frequency vibration absorbing performance, lack of adjustability and controllability and the like. Research shows that low-frequency vibration reduction can be realized by reasonably designing a nonlinear vibration damper, and particularly the development of the research is promoted by proposing the related principle of the quasi-zero stiffness vibration damper. Most of the existing quasi-zero stiffness vibration absorbers are based on spring mechanisms, and have the problems of difficulty in processing, difficulty in mounting, difficulty in implementation and the like during application, so that the application range of the quasi-zero stiffness vibration absorbers is limited.

Disclosure of Invention

Aiming at the problems in the existing transportation buffer package, the invention provides a quasi-zero-rigidity honeycomb core vibration reduction package, and the vibration reduction package is integrally prepared by a 3D printing technology or a cutting technology (including water cutting or laser cutting and the like), so that the vibration reduction package not only shows a certain degree of reusability, but also effectively improves the vibration reduction effect of the package at low frequency in the transportation process; the diversity of the external structure and the integrated preparation of the internal continuous structure of the shock absorber enable the shock absorber to be easier to process and apply and have wider application range compared with the existing quasi-zero rigidity shock absorber.

In order to achieve the purpose, the invention provides the following technical scheme: a quasi-zero rigidity honeycomb core vibration attenuation package is characterized in that an internal core structure is a honeycomb core formed by a cell linear array formed by connecting negative rigidity doubly-curved beams and positive rigidity conic curve walls in parallel, and the honeycomb core is integrally prepared through a 3D printing technology or a cutting technology; external structures include, but are not limited to, boxes, cylinders, pads, or other forms.

Specifically, the honeycomb core cell element consists of a double-curved beam, a conical curve wall and a pressing plate, and the upper part and the lower part of the honeycomb core cell element are in an axisymmetric structure.

Preferably, the double-curved beam provides positive stiffness for a mechanism providing negative stiffness and a conical curve wall in the orthogonal direction with the double-curved beam, and the cell element has a quasi-zero stiffness characteristic based on the positive and negative stiffness parallel principle, so that the overall structure can realize high static and low dynamic.

Specifically, the conical curve wall is tangent to the lower end of the hyperbolic beam, so that the honeycomb core is integrally formed through a 3D printing technology or a cutting technology.

Preferably, the honeycomb core is made of a nylon-based material with viscoelasticity by a 3D printing technology or a metal material with super elasticity by a cutting technology.

The working principle is as follows: when the single-curved-beam-type spring energy-saving loading and unloading device is used, when the single-curved beam generates nonlinear large deformation under the action of external load, an elastic buckling step phenomenon occurs, in the process of 'kick', the rigidity is subjected to a negative-value stage, namely, a negative rigidity effect is shown, and energy dissipation in the loading and unloading process is realized. But the single curved beam is easy to twist under the action of load, so that the negative stiffness effect is prevented from being shown, and the energy absorbed by the structure is reduced; when the double-curved beam is adopted, the double-curved beam is beneficial to limiting the jump of the curved beam between the first-order buckling mode and the third-order buckling mode, the occurrence of the asymmetric buckling mode is avoided, the negative rigidity behavior is promoted to be shown, the energy absorption capacity of the honeycomb core is improved, and therefore the double-curved beam is selected as a mechanism for providing the negative rigidity. The conical curve wall comprises an elliptical wall, a hyperbolic wall, a parabolic wall and the like, not only shows excellent stability, but also has higher static bearing capacity, and shows a positive rigidity characteristic under the action of vertical load, so that the conical curve wall is selected as a mechanism for providing positive rigidity. When external load acts, based on the principle that positive rigidity and negative rigidity are connected in parallel, positive rigidity generated by the conical curve wall and negative rigidity generated by buckling of the hyperbolic beam are offset, so that the cell element has the quasi-zero rigidity characteristic, the whole structure can realize high static and low dynamic, and low-frequency broadband vibration reduction is realized under the condition that the original bearing capacity is ensured. In addition, the nylon base material with viscoelasticity is integrally prepared by a 3D printing technology or a metal material with super elasticity is integrally prepared by a cutting technology, and the viscoelasticity, the super elasticity and the mechanical superstructure design of the material allow the honeycomb core to be reusable after multiple loading and unloading cycles.

Has the advantages that: the external structure of the quasi-zero-rigidity honeycomb core vibration damping package provided by the invention comprises but is not limited to a box, a cylinder, a pad or other forms, can be changed according to specific conditions, realizes multidirectional buffering vibration damping, and reduces the direct influence of vibration or impact on the external package in the transportation process. The internal core structure of the packaging bag is a quasi-zero-rigidity honeycomb core, so that the vibration reduction effect of the packaging bag in low-frequency transportation is improved, and the mechanical damage to the contents is reduced. The honeycomb core is integrally prepared by adopting a viscoelastic nylon-based material through a 3D printing technology or a superelastic metal material through a cutting technology, so that the problems that the traditional transportation buffer package cannot be reused after absorbing energy through plastic deformation, the bearing capacity is low and the like are solved, and the problem of three difficulties of the existing quasi-zero stiffness shock absorber is avoided.

Drawings

Fig. 1 is a front view of a package of an embodiment of the present invention.

Figure 2 is an internal cross-sectional view of a quasi-zero stiffness honeycomb core shock absorbing package.

Fig. 3 is a schematic view of the structure of a honeycomb core.

Fig. 4 is a schematic diagram of the cell structure.

In the figure: 2-1, side wall; 2-2, a bottom plate; 4-1, an upper pressing plate; 4-2, a hyperbolic beam; 4-3, reinforcing walls; 4-4, circular wall; 4-5, and a lower pressing plate.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail with reference to the accompanying drawings and embodiments; it should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

The example relates to a hyperbolic beam-circular wall quasi-zero rigidity honeycomb core vibration-damping packaging box, namely the external part of the box-type structure is shown in figure 1. The nylon-based material with viscoelasticity is integrally prepared by a 3D printing technology, and when alternating load is applied to the viscoelasticity material, the stress and strain are asynchronous, so that a hysteresis effect is shown, and the structure generates energy loss and has reusability.

Specifically, referring to fig. 2, an internal cross-sectional view of a quasi-zero stiffness honeycomb core shock-absorbing packing case is shown; the side wall 2-1 and the bottom plate 2-2 are honeycomb cores and are formed by linear arrays of cells, which are shown in fig. 3; the cell element is composed of a hyperbolic beam 4-2, a circular wall 4-4 and a pressing plate 4-1, and is in an axisymmetric structure from top to bottom, as shown in figure 4. Here, a circular wall 4-4 is selected as a mechanism for providing positive rigidity, and a hyperbolic beam 4-2 is selected as a mechanism for providing negative rigidity; when an external load acts, based on the principle that positive rigidity and negative rigidity are connected in parallel, positive rigidity generated by the circular wall 4-4 is gradually offset with negative rigidity generated by the hyperbolic beam 4-2, so that the cell element has the characteristic of quasi-zero rigidity, and further the whole structure realizes high static and low dynamic, thereby realizing low-frequency broadband vibration reduction under the condition of ensuring the original bearing capacity, and effectively improving the vibration reduction effect of the bottom plate 2-2 in the vertical direction under low frequency; the side wall 2-1 of the packing box is also of a quasi-zero rigidity honeycomb core structure, so that impact and mutual collision in the transverse direction are avoided, and the multi-direction vibration reduction effect of the packing box is improved. The structure is gradually restored to the original shape by virtue of the viscoelasticity and the mechanical superstructure design of the material in the unloading process, and meanwhile, the reusability is shown to a certain degree.

Specifically, referring to fig. 4, a schematic diagram of a cell structure is shown, which includes: an upper pressing plate 4-1, a hyperbolic beam 4-2, a reinforcing wall 4-3, a circular wall 4-4 and a lower pressing plate 4-5. The single curved beam is a prefabricated stress-free curved beam, the shape of the single curved beam is similar to that of a cosine beam, two concentric single curved beams are coupled at the center of the top to form a double curved beam 4-2, the curved beam is forced to jump between a first buckling mode and a third buckling mode, the occurrence of asymmetric buckling modes is limited, and the occurrence of a negative stiffness effect is promoted; the left end and the right end of the upper double-curved beam and the lower double-curved beam are respectively tangent to the horizontal direction and fixed by the reinforcing walls 4-3, so that the phenomenon that the transverse expansion of the beams prevents the negative stiffness effect is avoided; in addition, the circular outer wall 4-4 is tangent to the lower end of the hyperbolic beam 4-2, so that an internal continuous structure can be integrally prepared through a 3D printing technology, and the method is simple, convenient and quick.

The hyperbolic beam is used as a mechanism for providing negative rigidity and mainly plays a role in energy consumption; the conic curved wall is used as a mechanism for providing positive rigidity and mainly plays a bearing role.

The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms, and different external structures can be prepared or the structural parameters of the honeycomb core cells can be optimized according to actual requirements, so that the quasi-zero stiffness honeycomb core vibration damping package can meet the requirements of bearing capacity, energy consumption and vibration damping under different applications.

Any equivalent embodiments that may be changed or modified into equivalent variations by those skilled in the art can be applied to other fields without departing from the technical scope of the present invention, and any simple modification, equivalent variation and modification made to the above embodiments according to the technical spirit of the present invention still belong to the protection scope of the technical scope of the present invention.

6页详细技术资料下载
上一篇:一种医用注射器针头装配设备
下一篇:一种用于茶叶包装箱中的缓冲衬垫

网友询问留言

已有0条留言

还没有人留言评论。精彩留言会获得点赞!

精彩留言,会给你点赞!