Tussah carbon fiber composite helmet based on multi-element coupling bionics and preparation method

A composite material and composite material layer technology, applied in the field of tussah carbon fiber composite helmet and preparation, can solve the problems of inability to absorb impact force, poor impact resistance, helmet damage, etc. Effect of small damage area

Pending Publication Date: 2022-07-01
ANHUI UNIVERSITY OF TECHNOLOGY
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a tussah carbon fiber composite helmet based on multi-component coupling bionics and a preparation method. The helmet will not be sunken after being subjected to external force, and the impact force can be effectively absorbed, and the damage area of ​​the helmet can be reduced to the greatest extent. , the advantage of ensuring the safety of the user's head solves the problem that the existing helmet has a single structure and poor impact resistance. After the helmet is subjected to an external force, it is easy to cause the helmet to sag, the damage area of ​​the helmet is large, and the helmet is damaged in severe cases , cannot effectively absorb the impact force, cannot guarantee the safety of the user's head, and there are certain safety hazards

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Tussah carbon fiber composite helmet based on multi-element coupling bionics and preparation method
  • Tussah carbon fiber composite helmet based on multi-element coupling bionics and preparation method
  • Tussah carbon fiber composite helmet based on multi-element coupling bionics and preparation method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0036] An tussah carbon fiber composite helmet based on multiple coupling bionics, including a helmet shell 1 and multiple bionic elements, the helmet shell 1 includes a reinforcement layer 2, and the inner wall of the reinforcement layer 2 is bonded with a tussah silk carbon fiber hybrid composite material layer 3, and a tussah silk carbon fiber The inner wall of the hybrid composite material layer 3 is bonded with a buffer layer 4;

[0037] There are four kinds of multi-element bionic elements: exponential stiffness gradient structure, cross-scale multi-level wave interface morphology, controllable pore (content, size and spatial distribution) structure, and soft-hard phase synergistic bionic structure.

[0038] The design of the exponential stiffness gradient structure includes: by laying up fabrics with different areal densities, a laminate structure with exponential stiffness gradient is obtained, and the outermost layer adopts an areal density of 260kg m -2 Carbon fiber ...

Embodiment 2

[0045] An tussah carbon fiber composite helmet based on multiple coupling bionics, including a helmet shell 1 and multiple bionic elements, the helmet shell 1 includes a reinforcement layer 2, and the inner wall of the reinforcement layer 2 is bonded with a tussah silk carbon fiber hybrid composite material layer 3, and a tussah silk carbon fiber The inner wall of the hybrid composite material layer 3 is bonded with a buffer layer 4;

[0046] There are four kinds of multi-element bionic elements: exponential stiffness gradient structure, cross-scale multi-level wave interface morphology, controllable pore (content, size and spatial distribution) structure, and soft-hard phase synergistic bionic structure.

[0047] The design of the exponential stiffness gradient structure includes: by laying up fabrics with different areal densities, a laminate structure with exponential stiffness gradient is obtained, and the outermost layer adopts an areal density of 260kg m -2 Carbon fiber ...

Embodiment 3

[0053] An tussah carbon fiber composite helmet based on multiple coupling bionics, including a helmet shell 1 and multiple bionic elements, the helmet shell 1 includes a reinforcement layer 2, and the inner wall of the reinforcement layer 2 is bonded with a tussah silk carbon fiber hybrid composite material layer 3, and a tussah silk carbon fiber The inner wall of the hybrid composite material layer 3 is bonded with a buffer layer 4;

[0054] There are four kinds of multi-element bionic elements: exponential stiffness gradient structure, cross-scale multi-level wave interface morphology, controllable pore (content, size and spatial distribution) structure, and soft-hard phase synergistic bionic structure.

[0055] The design of the exponential stiffness gradient structure includes: by laying up fabrics with different areal densities, a laminate structure with exponential stiffness gradient is obtained, and the outermost layer adopts an areal density of 260kg m -2 Carbon fiber ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

PropertyMeasurementUnit
densityaaaaaaaaaa
Login to view more

Abstract

The invention discloses a tussah silk carbon fiber composite helmet based on multi-element coupling bionics and a preparation method, the tussah silk carbon fiber composite helmet comprises a helmet shell and multi-element bionic elements, the helmet shell comprises a reinforcing layer, the inner wall of the reinforcing layer is bonded with a tussah silk carbon fiber hybrid composite layer, and the tussah silk carbon fiber hybrid composite layer is bonded with the reinforcing layer. A buffer layer is adhered to the inner wall of the tussah silk carbon fiber hybrid composite material layer, and finally the helmet shell which is wrapped by the reinforcing layer, the hybrid composite material layer and the buffer layer layer by layer is prepared. The multi-element bionic elements comprise an exponential stiffness gradient structure, a cross-scale multi-stage wave interface form, a controllable pore content, size and space distribution structure and a soft and hard collaborative bionic structure. The problems that after an existing helmet is subjected to external acting force, the helmet is prone to being sunken, the helmet is damaged when the external acting force is serious, impact force cannot be effectively absorbed, safety of the head of a user cannot be guaranteed, and certain potential safety hazards exist are solved.

Description

technical field [0001] The invention relates to the technical field of helmets, in particular to an tussah carbon fiber composite helmet based on multi-coupling bionics and a preparation method. Background technique [0002] Helmet is a device to protect the head. It is a hat worn by soldiers in training and combat. It is an indispensable tool in people's transportation. It is divided into military helmets, police helmets and civilian helmets. The shell, lining and suspension device are composed of three parts. The shell is made of special steel, FRP, reinforced plastic, leather, nylon and other materials to resist the damage of warheads, shrapnel and other strikes to the head. [0003] The existing helmet has a single structure and poor impact resistance. After the helmet is subjected to an external force, it is easy to cause a dent in the helmet, and the damage area of ​​the helmet is large. It can ensure the safety of the user's head, and there are certain safety hazards...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/34B29C70/54A42B3/04B29L31/48
CPCB29C70/345B29C70/54A42B3/0406B29L2031/4821
Inventor 杨康秦楠楠余浩天李皓曈张芷涵胡泽平戴威龙
Owner ANHUI UNIVERSITY OF TECHNOLOGY
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products