Forming method of anti-icing array structure on surface of thermosetting resin-based composite material

A composite material and array structure technology, applied in the direction of climate sustainability, sustainable manufacturing/processing, household components, etc., can solve the problems of incomplete microstructure, complicated steps, difficult demoulding, etc., and achieve high structural consistency, Good superhydrophobic properties, the effect of complete microstructure

Pending Publication Date: 2020-11-10
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
View PDF8 Cites 5 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] In order to make up for the deficiencies of the prior art, the present invention provides a method for forming an anti-icing array structure on the surface of a thermosetting resin-based composite material to solve the problem of complex steps, difficult demoulding, micro Incomplete and unstable technical issues

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
  • Forming method of anti-icing array structure on surface of thermosetting resin-based composite material
  • Forming method of anti-icing array structure on surface of thermosetting resin-based composite material
  • Forming method of anti-icing array structure on surface of thermosetting resin-based composite material

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0039] refer to figure 1 , a method for forming an anti-icing array structure on a surface of a thermosetting resin-based composite material, comprising the following steps:

[0040](1) Prepare a transparent acrylic mold with an inner cavity size of 25×25×5mm, and a preform (H100 foam core material), clean and set aside.

[0041] (2) Prepare a 5×5×0.1mm anodized aluminum template with an inverted cone-shaped pit micro / nano array structure (for the structure, see figure 2 ), after cleaning, attach 70 pieces of anodized aluminum templates to the parts that need to build micro-nano structures in all the inner cavities of the mold.

[0042] (3) Place the H100 foam core material in a suitable position in the mold, and close the mold to form a closed mold.

[0043] (4) Mix bisphenol A epoxy resin LT5082, Cycracure UVI 6976 curing agent and low surface energy modifier FAS-17 in a ratio of 3:1:0.01 to obtain a liquid thermosetting resin mixture.

[0044] (5) Pour the mixed liquid ...

Embodiment 2

[0048] refer to figure 1 , a method for forming an anti-icing array structure on a surface of a thermosetting resin-based composite material, comprising the following steps:

[0049] (1) Prepare a cold-work steel mold with an inner cavity size of 70×70×10 mm, and clean it for later use.

[0050] (2) Prepare a 10×10×0.1mm anodized aluminum template with stepped pit micro / nano array structure (see Figure 4 ), after cleaning, stick 126 pieces of anodized aluminum templates on the parts that need to build micro-nano structures in all the inner cavities of the mold.

[0051] (3) Select SW220 high-strength glass fiber as the fiber cloth, cut the fiber cloth to a shape of 50×50×4mm, and wrap the H100 foam core material.

[0052] (4) Mix resin, curing agent and low surface energy modifier FAS-17 in a ratio of 3:1:0.01 to obtain a liquid thermosetting resin mixture.

[0053] (5) Place the preform wrapped in fiber cloth in a closed mold, and inject the mixed liquid thermosetting res...

Embodiment 3

[0059] refer to figure 1 , a method for forming an anti-icing array structure on a surface of a thermosetting resin-based composite material, comprising the following steps:

[0060] (1) Prepare a 304 stainless steel mold with an inner cavity size of 70×70×10 mm, and clean it for later use.

[0061] (2) Prepare a 10×10×0.1mm anodized aluminum template with an inverted cone-shaped pit micro / nano array structure, and after cleaning, attach 126 pieces of anodized aluminum template to all the inner cavities of the mold that need to build a micro-nano structure parts, to obtain a closed mold.

[0062] (3) Select SW220 high-strength glass fiber as the fiber cloth, cut the fiber cloth to a shape of 50×50×4mm, and wrap the H100 foam core material.

[0063] (4) Mix resin, curing agent and low surface energy modifier FAS-17 in a ratio of 3:1:0.03 to obtain a liquid thermosetting resin mixture.

[0064] (5) Place the preform wrapped in fiber cloth in a closed mold, and inject the mixe...

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
diameteraaaaaaaaaa
ice adhesion strengthaaaaaaaaaa
diameteraaaaaaaaaa
Login to view more

Abstract

The invention relates to a forming method of an anti-icing array structure on the surface of a thermosetting resin-based composite material. An anti-icing array on the surface of the thermosetting resin-based composite material is prepared by designing an anodic aluminum oxide template structure and adjusting forming parameters of the composite material. The forming method has the beneficial effects that the forming method of the anti-icing array structure on the surface of the thermosetting resin-based composite material is simple in manufacturing process, the manufactured composite materialis complete in surface micro-nano structure, stable in size and high in structural consistency, the super-hydrophobic characteristic is achieved on liquid water, the super-cooled liquid drop icing time can be remarkably prolonged, and supercooled liquid drops have enough time to be separated from the surface; the extremely low ice adhesion strength is achieved, and an ice coating can fall off fromthe surface under the action of natural wind or gravity; and the anti-icing array structure can be used for machine outer surfaces such as aircrafts and wind driven generator blades which are exposedin an extreme environment, and important significance on development of ice prevention and removal technologies of equipment such as wind driven generators, novel high-speed railway motor train unitsand airplanes, in particular to passive ice prevention and removal technologies is achieved.

Description

technical field [0001] The invention belongs to the field of composite material surface processing technology and surface modification technology, and in particular relates to a method for forming an anti-icing array structure on the surface of a thermosetting resin-based composite material. Background technique [0002] Thermosetting resin-based composite materials generally refer to continuous fiber / short fiber reinforced thermosetting resin-based composite materials, which have the characteristics of light weight, high strength and high stiffness, and have been widely used in the fields of national defense and people's livelihood. For example, the United States uses glass fiber reinforced epoxy resin composite materials to make rocket engine casings, high-pressure containers for fuel, and helicopter rotor blades. The domestic C919 aircraft skin uses a large number of epoxy resin composite laminates. [0003] Icing on the surface of aircraft such as high-altitude drones a...

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): B29C70/42B29C70/54B29C33/42B29C33/38
CPCB29C70/42B29C70/54B29C33/42B29C33/38B29L2031/085B29L2031/3076Y02P70/50
Inventor 刘森云郭奇灵陈圆圆魏龙涛杨升科赵献礼
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap