Composite energy absorption structure based on degradable material and 3D printing process of composite energy absorption structure
A technology of degradable materials and energy-absorbing structures, applied in the field of 3D printing technology, can solve problems such as weak impact resistance, unsatisfactory miniaturization, customized design requirements and product requirements, and achieve the effect of high-efficiency cushioning performance
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0048] This embodiment provides a 3D printing method for a composite energy-absorbing structure based on degradable materials. For details of the composite energy-absorbing structure, see figure 1 As shown, it includes end plates 3 located on both sides, and a negative Poisson’s ratio-honeycomb energy-absorbing region made of degradable material between the two end plates 3, the negative Poisson’s ratio-honeycomb type energy-absorbing area The functional area is composed of honeycomb structure monomer layers and negative Poisson's ratio structure monomer layers arranged alternately in sequence, wherein the honeycomb structure monomer layer is composed of several honeycomb structure monomers 1 arranged side by side, and the negative Poisson's ratio The Poisson's ratio structural monomer layer is composed of several negative Poisson's ratio structural monomers 2 arranged side by side. The inside is bent such that two of the interior angles of the hexagon are greater than 180°). ...
Embodiment 2
[0062] Compared with Embodiment 1, most of them are the same, except that the printing process parameters of this embodiment are as follows:
[0063] Material: PLA;
[0064] Composite structure, the relationship between the size parameters of the two monomers is a=a` or c=c`, where the size range a=4mm, c=8mm, and the range of the angle between two adjacent side walls is α=115 degrees. Side width or wall thickness t is 1.3 mm.
[0065] Layer thickness: 0.2-0.4mm.
[0066] Wire diameter: 1.75mm.
[0067] Nozzle aperture: 0.4mm.
[0068] Printing speed: 40mm / s.
[0069] Printing temperature: 205-225°C, hot bed temperature: 60-70°C.
[0070] Compression and impact tests were carried out on this structure, and the stress-strain curve was obtained. The obtained platform stress range was 3.1-3.4MPa, and the specific energy absorption value Es range was 6.4-6.8KJ / m 3 .The range of stress is 33-38MPa, and the range of strain is 48-55%.
Embodiment 3
[0072] Compared with Example 1, most of them are the same, except that the composite energy-absorbing structure in this example is replaced by figure 2 structure, specifically:
[0073] Two adjacent rows of honeycomb structure monomers 1 of the same honeycomb structure monomer layer are stacked in the form of "side to side", and the same row of honeycomb structure monomers 1 is stacked "bottom to bottom". The forms are arranged side by side; at this time, there is a natural transition between the two layers of monomers, forming a zero-thickness zigzag section. The sides of the honeycomb structural monomer 1 and the negative Poisson's ratio structural monomer 2 are respectively facing the end plate 3, and the side of the honeycomb structural monomer 1 is facing the side of the negative Poisson's ratio structural monomer 2, At this time, b=b', t=t'.
[0074] When the end plate 3 is a honeycomb structure monomer layer, the honeycomb structure monomer layer continues for half a...
PUM
| Property | Measurement | Unit |
|---|---|---|
| diameter | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 


